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poi oi6 - oo18 $ NEW MILLENNIUM .......................... BUILDING SYSTEMS November 8, 2019 APPROVED To: StNorth rth HolStar Industries, RECEIVED North Star Industries, Inc. MAR 2 3 2020 Project: TIGARD HIGH SCHOOL—Phase 2 CITY OFTIGARD OFFICE COP'sr Tigard, OR BUILDING DIVISION NMBS Job#5618-0007 Re: Final Joist Design CalculationsREVISION This letter is to certify that the steel joists and bridging supplied by New Millennium Building Systems,LLC for the above-mentioned project have been designed and manufactured in accordance with the current Steel Joist Institute standards and specifications, as well as with the specified design and loading information provided on the contract documents. New Millennium Building Systems, LLC is a fully approved member company of the Steel Joist Institute. Respectfully,� ii'r.�"�if-<�0— f/----z ��D PROFS Hamed Zargar ��\� *G I N E E '/, Design Engineer 'r 72501PE II—II-19 OREGON y/S MONtC's4 Exp. 12-31-20 ®REVIEWED REJECTED ❑n REVISE MAKE AND RRECTIONS NOTED NDR RESUBMIT THIS REVIEW DOES NOT RELIEVE CONTRACTOR FROM COMPLIANCE WITH THE REQUIREMENTS OF THE DRAWINGS AND SPECIFICATIONS. THIS REVIEW IS ONLY FOR GENERAL CONFORMANCE WITH THE DESIGN CONCEPT OF THE PROJECT AND GENERAL COMPLIANCE WITH THE INFORMATION GIVEN IN THE CONTRACT DOCUMENTS. CONTRACTOR IS RESPONSIBLE FOR CONFIRMING AND CORRELATING ALL QUANTITIES AND DIMENSIONS, SELECTING FABRICATION PROCESSES AND TECHNIQUES OF CONSTRUCTION,COORDINATING THEIR WORK WITH ALL OTHER TRADES,AND PERFORMING THEIR WORK IN A SAFE AND SATISFACTORY MANNER. 03/02/2020 DAA DATE CATENA CONSULTING ENGINEERS BY 8200 Woolery Way I Fallon,Nevada 89406 I Phone:775-428-0600 I Fax:775-867-2169 I www.newmill.com FLEXIBLE to the FINISH NEW MILLENNIUM BUILDING SYSTEMS JOIST CALCULATION DEFINITION SHEET Load Types: (Figure 1) Uniform Uniform line load applied to TC or BC Net Uplift Uniform line load applied to TC(not concurrent w/uniform dead or live loading) Gross Uplift Uniform line load applied to TC(concurrently w/factored dead loads per Code requirements) Axial Compressive/Tensile (+/-)forces applied to TC or BC Concentrated Load Vertical load applied at given location , Conc @ any pp Vertical load applied at any panel point(local panel bending not applied to chords) Conc anywhere Vertical load applied at any location along chord (local panel bending applied to chords) Conc w/bending Vertical load applied at given location (local panel bending applied to chords) Category: (Figure 1) DL Dead Load LL Live Load TL Total Load (DL+ LL) IP Inward Pressure WL Wind Load SM Seismic Load CL Collateral Load SL Snow Load (1), (2), (3),etc. Individual Separate Design Load Cases Position: (Figure 1) TC Top Chord BC Bottom Chord Load Combinations: (Figure 2) All shown load combinations are ran for each Load Case(1,2,3,etc.) Loads Load Type Category Loadt Load2 Position Direction Loc/Begin Sp/End Uniform(pif) DL(1) 96.47 96.47 TC + 0-0 30-5 518 Uniform(pit) LL(1) 234.22 234.22 TC + 0-0 30-5 5/8 Net Uplift(pit) WL(1) 87.00 67.00 TC - 0-0 30-5 5/8 Uniform(plt) TL(2) 319.00 319.00 TC + 0-0 30-5 5/8 Axial(Ibs) SM(2) 300.00 0.00 IC + 0-0 0-0 Cone Load(bs) DL(2) 1,700.00 0.00 TC + 13-01/4 13-0 114 Conti... .alb) DL(2) 1,70000 0.00 TC + 26.61/4 26-61/4 Figure 1 LoadComb+tidons (Example only) Case 1:DL Case 6a:DL+CL+0.85(1L)+WL+AX Case 2a:LL Case 6b:DL+CL+0.85(TL)-WL-AX Case 2b:SL Case 6c:0LaCL+0.85(TL)+WL+AX+IP Case 3a:DL+CL+TL+LL Case 641:DL+CL+0.85(TL)+WL-AX 4P Case 3b:DL+CL+TL+SL Case 6e:DL•CL.0.85(TL)+SM+AX Case 3c:DL+CL+TL+LL+FEM Case 6f:DL+CL-0.85(TL)+SM-AY Case 3d:OL+CL+TL+SL+FEM Case 7a:DLCL.0,85(TL)+0.75(WL+AX+LLI Case 3e:DL+CL+TL+LL Case 76:DL.CL+0,85(TLN0.75(WL-AX+LLI Case 3f:DL+CL+TL+SL Case 7c:DL+0L+0,85(TL)+0.75(WL+AX+LL+1P) Case 4a:DL+WLaAX Case 7d:OL+CL+0.85(TL)+0.75(WL-AX.LL+IP) Case 4b:OL+WL-AX Case 7e:0L+CL+0.85(1L)+0.75(SM+AX+LL) Case 4c:DL+W L+AX+IP Case 71:DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4d:0L+WL-AX+IP Casa as:DL.CL+0.851TL)+0.75(WL+AX+SL) Case 4e:DL+SM+AX Case ab:DL,CL+0.85(TL)+0.75(WL-AX+SL) Case 41:DL+SM-AX Case Sr.0L+CL+0.85(TL)+0,75(11L+AX+SL+IP) Case 58:0.6(DL)+WL+AX Case ad:DL+CL.0.a5(TL)+0.75(WL•AX-SL.P) Case 5b:0,6(DL)+WL-AX Case 8e:OL.CL.0,a5(TL).0,75(WL+AX+SL+8M) Casa 5c:0.6(DLi+WL+AX+lP Case 81:OL+CL+0.85(TL)+0.75(WL-AX+SL+SMI Casa 5d:0.6(13L)+WL-AX+IP Case 9a:1,2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Figure 2 Case 5e:0.6(DL)+WL+AX+SM Case 96:1.2(OL)+05(LL).0.8(TL)+SM-AX+FEM Case 51:0.6(DL)+W L-AX+SM 8200 Woolery Way I Fallon,Nevada 89406 I Phone:775-428-0600 I Fax:775-867-2169 I www.newmill.com r1LEXIBLL to the FINISH Interior Dimensions: - TC PANEL 1 V2 { BC PANEL - Left End Dimensions: OVERALL LENGTH BASELENG TH TCX FIRST DIAGONAL - { TC PANEL -� W2 V 1S W3 W4 V2 BC PANEL FIRST HALF BCX Right End Dimensions: FIRST DIAGONAL 1 F TCX TC PANEL V2 4 W3 1S 2 v U I BCX FIRST HALF BC PANEL Notes&Abbreviations: TCX-Top Chord Extension BCX-Bottom Chord Extension BPL-Base Plate Length V1S-First Vertical Web Member V2-Standard Vertical Web Member W2-First Diagonal Web Member All vertical and diagonal web members are ordered numerically progressive toward interior 8200 Woolery Way j Fallon,Nevada 89406 I Phone:775-428-0600 I Fax:775-867-2169 www.newmill.com FLEXIBLE to the FINISH STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:01:01 AM NEW NI I L L E N N I U NI Location: Joist Description: Mark: 91_I11_O1NC SYSTEMS TIGARD,OR Long Span 48LH550/370 J22 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 56-4 56-0 48.00 46.16 7 Special Parallel Chords Variable Left End Right End BC Panel 8-1 7-11 ,I�,,„bk„"k°,.]_i,I,.,., , ,.,,, ,..,.1ny7,�„�„��,�,y,,��,„,,„,,,,� �,�, ��������„��,y ,,,���,7,1, „r,�,,,,,t TC Panel 4-0 4-0j,77 �� �\ /� �� / \ i \ i / �, / A� / i j/ First Half 0-10 0-10 � ,,,/ First Diag. 8-11 8-9 Depth 48.00 48.00 J Loads Load Type Category Load1 Load2 Position Direction LocBegin Sp/End Reference Uniform(plf) LL (1) 370.00 370.00 TC + 0-0 56-4 L-BL Uniform(plf) DL(1) 180.00 180.00 TC + 0-0 56-4 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM (1) 3,500.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp (Ibs) SM(1) 400.00 0.00 TC + Uniform(plf) DL(1) 120.00 120.00 BC + 0-0 56-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) IP (1) 84.00 84.00 TC + 0-0 56-4 L-BL Conc @ any pp(Ibs) WL (1) 400.00 0.00 TC + Uniform(plf) SM (1) 30.00 30.00 TC + 0-0 56-4 L-BL Uniform(plf) DL(1) 38.00 38.00 TC + 0-0 56-4 L-BL Conc Load(Ibs) SM(1) 2,800.00 0.00 TC + 1-9 1/2 7-9 1/2 L-OAL Conc Load(lbs) WL(1) 2,400.00 0.00 TC + 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 4-11 1/2 4-11 1/2 L-OAL Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 9-1 1/2 9-1 1/2 L-OAL Conc w/bending(Ibs) CL(1) 500.00 0.00 TC + 28-9 1/2 28-9 1/2 L-OAL Conc Load(lbs) LL(1) 4,000.00 0.00 TC + 30-3 31-4 L-OAL Conc Load(Ibs) LL(1) 1.00 0.00 TC + 30-3 30-3 L-OAL Conc Load(Ibs) LL(1) 1.00 0.00 TC + 31-4 31-4 L-OAL Conc Load(Ibs) WL(1) 2,400.00 0.00 TC + 49-9 1/2 55-9 1/2 L-OAL Conc Load (Ibs) SM (1) 2,800.00 0.00 TC + 49-9 1/2 55-9 1/2 L-OAL Conc @ any pp(Ibs) SM(2) 400.00 0.00 TC - Gross Uplift(plf) WL(2) 54.00 54.00 TC - 0-0 56-4 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc Load(Ibs) WL(2) 2,400.00 0.00 TC - 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) SM (2) 2,800.00 0.00 TC - 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) LL(2) 4,000.00 0.00 TC - 30-3 31-4 L-OAL Conc Load(Ibs) SM(2) 2,800.00 0.00 TC - 49-9 1/2 55-9 1/2 L-OAL Conc Load(Ibs) WL(2) 2,400.00 0.00 TC - 49-9 1/2 55-9 1/2 L-OAL Stress Analysis Summary InL Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 52.00 73.00 27,343.22 22,894.37 6,835.80 92,484.00 91,749.76 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 9,194.90 57,876.93 0.00 0.00 60,120.21 10,999.58 105.62 0-2 Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:01:01 AM NEW MILLENNIUM Location: Joist Description: Mark: BUILCIING SN' TEnes TIGARD,OR Long Span 48LH550/370 J22 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. V1S 8,286.07 51,363.94 0.00 0.00 4,723.14 11,500.58 67.32 4-0 W3 8,286.07 51,363.94 51,086.21 9,068.48 3,899.10 19,940.45 47.23 8-1 W4 11,619.86 70,003.26 51,086.21 9,068.48 23,133.82 4,225.60 69.53 8-11 V2 11,619.86 70,003.26 51,086.21 9,068.48 1,896.45 4,347.62 46.16 13-3 W5 11,619.86 70,003.26 73,906.16 13,270.38 3,319.84 15,891.82 58.54 13-3 W6 14,826.13 84,418.86 73,906.16 13,270.38 13,654.70 3,165.75 58.54 16-3 V3 14,826.13 84,418.86 73,906.16 13,270.38 1,896.45 4,018.18 46.16 19-3 W7 14,826.13 84,418.86 86,062.59 16,287.11 2,970.90 10,498.13 58.54 19-3 W8 17,653.33 92,484.00 86,062.59 16,287.11 8,669.21 2,551.50 58.54 22-3 V4 17,653.33 92,484.00 86,062.59 16,287.11 1,896.45 4,477.03 46.16 25-3 W9 17,653.33 92,484.00 91,749.76 19,243.05 9,862.30 9,739.85 66.59 25-3 W9 18,633.63 92,391.52 91,749.76 19,243.05 2,118.74 7,637.51 51.57 29-3 V5 18,633.63 92,391.52 91,749.76 19,243.05 2,174.02 2,703.73 46.16 31-2 W8 18,633.63 92,391.52 84,889.03 17,101.58 8,761.07 2,844.50 59.16 31-2 W7 15,514.85 81,723.59 84,889.03 17,101.58 2,970.90 10,498.13 58.54 34-3 V6 15,514.85 81,723.59 84,889.03 17,101.58 2,174.98 2,325.24 46.16 37-3 W6 15,514.85 81,723.59 70,146.77 13,833.36 13,654.70 3,165.75 58.54 37-3 W5 12,057.09 64,807.21 70,146.77 13,833.36 3,319.84 15,891.82 58.54 40-3 V7 12,057.09 64,807.21 70,146.77 13,833.36 2,174.98 2,626.47 46.16 43-3 W4 12,057.09 64,807.21 44,084.04 9,324.08 23,133.82 4,225.60 69.53 43-3 W3 8,498.66 44,654.66 44,084.04 9,324.08 3,899.10 19,940.45 47.23 47-7 V1S 8,498.66 44,654.66 0.00 0.00 4,640.69 6,893.93 65.87 52-4 W2 9,338.80 47,706.37 0.00 0.00 49,089.00 11,279.79 103.82 48-5 STRESS ANALYSIS - PAGE 2 0 Job Number. Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:01:01 AM NEW MILLENNIUM Location: Joist Description: Mark: aLIILoING SYSTEMS TIGARD,OR Long Span 48LH550/370 J22 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 2.0930 1.0824 0.6899 1.8930 0.9905 2.4522 0.9871 3531 =3 1/2 X 3 1/2 X .313 BC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 3,880.84 825.59 1,238.38 26-9 3/4 23-9 1/2 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.00 59.00 52.00 57.00 46.00 1.1250 Min Weld Len 2X: Bending Load 588.00 588.00 588.00 588.00 588.00 0.9965 Axial Load 57,876.93 51,363.94 92,484.00 44,654.66 47,706.37 Max Load Fillers TC: fa 13,826.31 12,270.41 22,093.65 10,667.62 11,396.65 108,701.86 Maximum K L/r 66.68 85.52 52.18 82.62 66.68 Max Load no Fillers TC: Fcr 35,808.61 29,113.36 40,549.95 30,155.83 35,808.61 97,493.13 TC OAU Fa 21,485.17 17,468.02 24,329.97 18,093.50 21,485.17 354.99Ryy: 54.99 F'e 158,473.86 96,331.71 258,742.78 103,210.43 158,473.86 BC GAL/Ryy: Cm 0.9564 0.9363 0.9428 0.9483 0.9640 397.16 Panel Point Moment 13,382.47 13,606.80 12,863.95 13,006.97 12,582.66 BC Stress: Mid Panel Moment 5,680.78 7,826.49 6,575.97 7,105.31 5,477.60 0.95 Panel Point fb 6,847.59 6,962.37 6,582.27 6,655.45 6,438.34 BC 123.585822 Mid Panel fb 1,147.30 1,580.65 1,328.09 1,435.00 1,106.26 TC Shear Stress: Fillers 0 0 0 0 0 13,620.19 Panel Point Stress 20,673.90 19,232.78 28,675.91 17,323.07 17,834.99 BC Shear Stress: Mid Panel Stress 0.6821 0.7589 0.9519 0.6390 0.5668 17,708.68 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 60,120.21 96,902.01 10,999.58 56,749.00 14.41 x 0.281 2 3028=3 X 3 X.281 V1S 4,723.14 28,769.10 11,500.58 12,902.79 5.16 x 0.150 2 A28B= 1.7350 x 0.150 W3 3,899.10 31,392.15 19,940.45 21,739.21 8.50 x 0.158 2 A30B= 1.7970 x 0.158 W4 23,133.82 24,373.24 4,225.60 4,397.44 8.31 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V2 1,896.45 14,381.54 4,347.62 5,250.81 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 3,319.84 31,392.15 15,891.82 17,851.42 6.77 x 0.158 2 A30B= 1.7970 x 0.158 W6 13,654.70 14,381.54 3,165.75 3,648.09 6.13 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V3 1,896.45 10,742.43 4,018.18 4,052.10 2.10 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 2,970.90 28,624.38 10,498.13 10,875.72 3.77 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W8 8,669.21 10,742.43 2,551.50 2,788.78 4.53 x 0.129 1 C22BB = 1.125 x 1.110 x.129 V4 1,896.45 14,381.54 4,477.03 5,250.81 2.01 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W9 9,862.30 28,597.25 9,739.85 10,361.07 3.54 x 0.188 1 A40B=2.3750 x 0.218 W9 2,118.74 28,624.38 7,637.51 8,076.09 2.74 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V5 2,174.02 8,984.69 2,703.73 3,238.38 2.00 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 8,761.07 14,381.54 2,844.50 3,586.82 3.93 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 2,970.90 28,624.38 10,498.13 10,875.72 3.77 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 V6 2,174.98 7,826.93 2,325.24 2,665.16 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 13,654.70 14,381.54 3,165.75 3,648.09 6.13 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 3,319.84 31,392.15 15,891.82 17,851.42 6.77 x 0.158 2 A30B= 1.7970 x 0.158 Continued on Next Page... STRESS ANALYSIS - PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:01:01 AM NEW MILLENNIUM Location: Joist Description: Mark: BLELOINM SYSTEMS TIGARD,OR Long Span 48LH550/370 J22 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 2,174.98 7,826.93 2,626.47 2,665.16 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W4 23,133.82 24,373.24 4,225.60 4,397.44 8.31 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 3,899.10 31,392.15 19,940.45 21,739.21 8.50 x 0.158 2 A30B= 1.7970 x 0.158 V1S 4,640.69 21,490.90 6,893.93 7,780.38 3.60 x 0.129 2 A22B= 1.5000 x 0.129 W2 49,089.00 79,023.08 11,279.79 45,608.89 14.56 x 0.227 2 3022=3 x 3 x.227 STRESS ANALYSIS - PAGE 3 l/� Job Number: Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:01:01 AM NEW MI L L E N NI UM Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 48LH550/370 J22 TCX Design TCX Left TCX Right TCX Length 0-7 1/2 TCX Length 0-9 TCX Type S TCX Type S TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-8 1/8 Clear Bearing 0-8 3/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 550.00 Total Load 550.00 Reqd TL Def L/80 0.09 Reqd TL Def L/80 0.11 Live Load 370.00 Live Load 370.00 Reqd LL Def L/120 0.06 Reqd LL Def L/120 0.08 Section Modulus 1.9543 Section Modulus 1.9543 Reqd SM 0.0689 Reqd SM 0.0924 Mom of Inertia 4.9044 Mom of Inertia 4.9044 Reqd MI 0.0137 Reqd MI 0.0212 Seat Type:T-Plate 1" Seat Type:T-Plate 1" Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0/� Job Number: Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/3/2019 8:57:58 AM NEW MILLENNIUM Location: Joist Description: Mark: 0UILOING SYSTEMS TIGARD,OR Long Span 48LH550/370 J24 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 56-4 56-0 48.00 L46.31 7 Special Parallel Chords Variable Left End Right End BC Panel 8-1 7-11 TC Panel 4-0 4-0 ��\ I 1 V / vv / � i ,V / ./ 1� / First Half 0-10 0-10 First Diag. 8-11 8-9 Depth 48.00 48.00 Loads Load Type Category Load1 Load2 Position Direction LoclBegin Sp/End Reference Uniform(plf) LL(1) 370.00 370.00 TC + 0-0 56-4 L-BL Uniform(plf) DL(1) 180.00 180.00 TC + 0-0 56-4 L-BL Uniform(plf) SM (1) 30.00 30.00 TC + 0-0 56-4 L-BL Uniform(plf) DL(1) 120.00 120.00 BC + 0-0 56-4 L-BL Uniform (plf) DL(1) 26.00 26.00 TC + 0-0 56-4 L-BL Uniform (plf) IP(1) 84.00 84.00 TC + 0-0 56-4 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM(1) 3,500.00 0.00 TC + 0-0 0-0 L-BL Cone Load(Ibs) SM (1) 2,800.00 0.00 TC + 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) WL(1) 2,400.00 0.00 TC + 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) CL(1) 500.00 0.00 TC + 28-9 1/2 28-9 1/2 L-OAL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc Load (Ibs) WL (1) 2,400.00 0.00 TC + 49-9 1/2 55-9 1/2 L-OAL Conc Load (Ibs) SM (1) 2,800.00 0.00 TC + 49-9 1/2 55-9 1/2 L-OAL Gross Uplift(plf) WL(2) 54.00 54.00 TC - 0-0 56-4 L-BL Conc Load(Ibs) WL(2) 2,400.00 0.00 TC - 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) SM (2) 2,800.00 0.00 TC - 1-9 1/2 7-9 1/2 L-OAL Cone @ any pp(Ibs) SM(2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc Load(Ibs) SM(2) 2,800.00 0.00 TC - 49-9 1/2 55-9 1/2 L-OAL Conc Load (Ibs) WL(2) 2,400.00 0.00 TC - 49-9 1/2 55-9 1/2 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 52.00 72.00 20,253.84 20,256.69 5,064.17 76,370.90 72,760.77 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 8,222.58 43,202.32 0.00 0.00 43,830.01 . 10,179.22 105.69 0-2 V1S 7,068.81 39,994.77 0.00 0.00 4,714.68 6,903.87 67.42 4-0 W3 7,068.81 39,994.77 38,847.16 7,698.88 3,045.35 15,987.39 47.38 8-1 W4 8,959.24 56,639.92 38,847.16 7,698.88 18,500.21 2,353.28 69.63 8-11 W5 8,959.24 56,639.92 59,264.14 9,677.88 1,666.00 12,105.75 58.66 13-3 W6 10,270.59 69,613.94 59,264.14 9,677.88 10,029.18 1,460.81 58.66 16-3 •Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/3/2019 8:57:58 AM NEW MI L L E N N I UM Location: Joist Description: Mark: BIJILDIWO BVSTFM5 TIGARD,OR Long Span 48LH550!370 J24 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W7 10,270.59 69,613.94 69,129.63 10,737.38 1,302.05 6,999.95 58.66 19-3 W8 11,078.24 76,370.90 69,129.63 10,737.38 6,414.21 1,302.05 58.66 22-3 W9 11,078.24 76,370.90 72,760.77 11,284.53 1,302.05 6,414.21 58.66 25-3 W9 11,062.60 76,271.63 72,760.77 11,284.53 1,302.05 6,414.21 58.66 28-3 W8 11,062.60 76,271.63 68,948.38 10,714.75 6,414.21 1,302.05 58.66 31-3 W7 10,240.97 69,350.69 68,948.38 10,714.75 1,302.05 6,999.95 58.66 34-3 W6 10,240.97 69,350.69 58,918.88 9,641.26 10,029.18 1,460.81 58.66 37-3 W5 8,915.62 56,212.65 58,918.88 9,641.26 1,666.00 12,105.75 58.66 40-3 W4 8,915.62 56,212.65 38,301.45 7,645.16 18,500.21 2,353.28 69.63 43-3 W3 7,002.41 39,427.34 38,301.45 7,645.16 3,045.35 15,987.39 47.38 47-7 V1S 7,002.41 39,427.34 0.00 0.00 4,632.71 6,697.14 65.98 52-4 W2 8,049.48 42,416.46 0.00 0.00 43,090.39 9,969.20 103.89 48-5 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 617.64 2,568.17 46.31 STRESS ANALYSIS - PAGE 2 �, Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/3/2019 8:57:58 AM NEW MILLENNIUM Location: Joist Description: Mark: RI Ill 1-11ti1-, SYSTEMS TIGARD,OR Long Span 48LH550/370 J24 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028= 3 X 3 X.281 BC 1.3105 0.9336 0.5937 1.6798 0.8340 1.1423 0.9229 3022= 3 x 3 x.227 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 3,101.51 659.80 989.69 23-115/8 27-101/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.00 59.00 52.00 57.00 46.00 1.1250 Min Weld Len 2X: Bending Load 576.00 576.00 576.00 576.00 576.00 0.8229 Axial Load 43,202.32 39,994.77 76,370.90 39,427.34 42,416.46 Max Load Fillers TC fa 13,441.92 12,443.92 23,761.95 12,267.37 13,197.41 87,990.42 Maximum K L/r 77.87 99.88 45.71 96.50 77.87 Max Load no Fillers TC: Fcr 32,092.32 24,108.93 42,916.72 25,309.95 32,092.32 80,841.32 OALFa 19,255.39 14,465.36 25,750.03 15,185.97 19,255.39 3 97.16 T7..16 y: Fe 115,985.59 70,504.31 336,660.53 75,538.79 115,985.59 BC oA1Ryy: Cm 0.9421 0.9118, 0.9527 0.9188 0.9431 400.04 Panel Point Moment 13,099.30 13,332.00 5,184.00 12,745.41 12,312.16 BC Stress: Mid Panel Moment 5,540.06 7,670.35 2,592.00 6,965.22 5,332.66 0.93 Panel Point fb 10,201.86 10,383.10 4,037.35 9,926.25 9,588.83 BC 121.272734 Mid Panel fb 1,715.89 2,375.69 802.81 2,157.30 1,651.65 TC Shear Stress: Fillers 0 0 0 0 0 12,935.85 Panel Point Stress 23,643.78 22,827.02 27,799.30 22,193.63 22,786.24 BC Shear Stress: Mid Panel Stress 0.7575 0.9513 0.9485 0.8884 0.7424 15,979.43 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 43,830.01 96,902.01 10,179.22 56,709.61 11.65 x 0.281 2 3028=3 X 3 X.281 W3 3,045.35 25,965.15 15,987.39 16,761.72 7.58 x 0.142 2 A26B = 1.6560 x 0.142 W4 18,500.21 18,714.09 2,353.28 3,490.12 7.08 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W5 1,666.00 25,965.15 12,105.75 13,275.54 5.74 x 0.142 2 A26B = 1.6560 x 0.142 W6 10,029.18 10,742.43 1,460.81 2,779.11 5.24 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 1,302.05 28,624.38 6,999.95 10,845.76 2.51 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 W8 6,414.21 7,826.93 1,302.05 1,853.56 4.23 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 1,302.05 28,624.38 6,414.21 6,631.75 2.30 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W9 1,302.05 28,624.38 6,414.21 6,631.75 2.30 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W8 6,414.21 7,826.93 1,302.05 1,853.56 4.23 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,302.05 28,624.38 6,999.95 10,845.76 2.51 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 W6 10,029.18 10,742.43 1,460.81 2,779.11 5.24 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W5 1,666.00 25,965.15 12,105.75 13,275.54 5.74 x 0.142 2 A26B= 1.6560 x 0.142 W4 18,500.21 18,714.09 2,353.28 3,490.12 7.08 x 0.176 1 C34AA= 1.125 x 1.549 x .176 W3 3,045.35 25,965.15 15,987.39 16,761.72 7.58 x 0.142 2 A26B= 1.6560 x 0.142 W2 43,090.39 86,681.16 9,969.20 50,896.02 11.67 x 0.250 2 3025= 3 x 3 x.250 V1 4,714.68 21,490.90 6,903.87 7,426.99 3.60 x 0.129 2 A22B= 1.5000 x 0.129 V2 617.64 7,826.93 2,568.17 2,652.48 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/3/2019 8:57:58 AM NEW MILLENNIUM Location: Joist Description: Mark: SUILon is SYSTEMS TIGARD,OR Long Span 48LH550/370 J24 TCX Design TCX Left TCX Right TCX Length 0-7 1/2 TCX Length 0-9 TCX Type S TCX Type S TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-8 1/8 Clear Bearing 0-8 1/4 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 550.00 Total Load 550.00 Reqd TL Def L/80 0.09 Reqd TL Def L/80 0.11 Live Load 370.00 Live Load 370.00 Reqd LL Def L/120 0.06 Reqd LL Def L/120 0.08 Section Modulus 1.2840 Section Modulus 1.2840 Reqd SM 0.0689 Reqd SM 0.0924 Mom of Inertia 2.7560 Mom of Inertia 2.7560 Reqd MI 0.0137 Reqd MI 0.0212 Seat Type'T-Plate 1" Seat Type'T-Plate 1" Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+A)(+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 �/� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 8:43:28 AM NEW MILLENNIUM Location: Joist Description: Mark: aUlt_oING SYSTEMS TIGARD,OR Long Span 48LH550/370 J26 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 56-4 56-0 48.00 46.18 7 Special Parallel Chords Variable Left End Right End BC Panel 8-1 7-11 milli 1r TC Panel 4-0 4-0 i 1 /\.� /\ j\ / v �`� First Half 0-10 0-10 ����ih101i1111(1111➢1111Uillllllll11�1if1'IIIIIIIIIIIIIIIILI I111111111I1I1i�1,11111111111111111��1i�((II 1111I(ll�ftlWt 1111111111I � First Diag. 8-11 8-9 Depth 48.00 48.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference ! Uniform(plf) LL(1) 370.00 370.00 TC + 0-0 56-4 L-BL Uniform(plf) DL(1) 180.00 180.00 TC + 0-0 56-4 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Conc @ any pp (Ibs) WL(1) 400.00 0.00 TC + Axial(Ibs) SM (1) 450.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 36.00 36.00 TC + 0-0 56-4 L-BL Uniform(plf) SM (1) 30.00 30.00 IC + 0-0 56-4 L-BL Uniform(plf) IP (1) 84.00 84.00 TC + 0-0 56-4 L-BL Axial (Ibs) SM (1) 3,500.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(Ibs) SM(1) 400.00 0.00 TC + Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Uniform(plf) DL(1) 120.00 120.00 BC + 0-0 56-4 L-BL Axial(Ibs) WL(1) 450.00 0.00 TC + 0-0 0-0 L-BL Conc Load(Ibs) WL(1) 2,400.00 0.00 TC + 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) SM(1) 2,800.00 0.00 TC + 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) LL(1) 4,000.00 0.00 TC + 30-3 31-4 L-OAL Conc Load(Ibs) SM (1) 2,800.00 0.00 TC + 49-9 1/2 55-9 1/2 L-OAL Conc Load(Ibs) WL(1) 2,400.00 0.00 TC + 49-9 1/2 55-9 1/2 L-OAL Gross Uplift(plf) WL(2) 54.00 54.00 TC - 0-0 56-4 L-BL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc Load (Ibs) SM (2) 2,800.00 0.00 TC - 1-9 1/2 7-9 1/2 L-OAL Conc Load (Ibs) WL(2) 2,400.00 0.00 TC - 1-9 1/2 7-9 1/2 L-OAL Conc Load (Ibs) LL(2) 4,000.00 0.00 TC - 30-3 31-4 L-OAL Conc Load (Ibs) WL(2) 2,400.00 0.00 TC - 49-9 1/2 55-9 1/2 L-OAL Conc Load(Ibs) SM (2) 2,800.00 0.00 TC - 49-9 1/2 55-9 1/2 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 52.00 73.00 22,003.49 22,216.58 5,554.14 87,482.96 85,065.57 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 9,499.40 46,909.86 0.00 0.00 47,892.73 11,675.73 105.63 0-2 Continued on Next Page... STRESS ANALYSIS - PAGE 1 �' Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 8:43:28 AM NEW MILLENNIUM Location: Joist Description: Mark: aLIIL�ING SYSTEMS TIGARD,OR Long Span 48LH550/370 J26 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. V1S 8,590.97 43,646.45 0.00 0.00 5,305.26 7,417.82 67.33 4-0 W3 8,590.97 43,646.45 42,504.49 9,405.51 4,052.50 17,724.84 47.25 8-1 W4 12,124.67 62,354.82 42,504.49 9,405.51 21,689.46 4,605.76 69.54 8-11 V2 12,124.67 62,354.82 42,504.49 9,405.51 1,896.45 4,297.82 46.18 13-3 W5 12,124.67 62,354.82 65,797.68 13,891.40 3,590.99 14,687.23 58.55 13-3 W6 15,563.40 77,613.95 65,797.68 13,891.40 12,458.10 3,436.93 58.55 16-3 V3 15,563.40 77,613.95 65,797.68 13,891.40 1,896.45 3,972.77 46.18 19-3 W7 15,563.40 77,613.95 78,487.25 17,140.67 3,201.35 9,309.68 58.55 19-3 W8 18,623.22 86,544.16 78,487.25 17,140.67 7,042.61 2,780.33 58.55 22-3 V4 18,623.22 86,544.16 78,487.25 17,140.67 1,896.45 4,298.35 46.18 25-3 W9 18,623.22 86,544.16 85,065.57 20,283.70 2,851.63 8,011.34 66.61 25-3 W9 19,599.84 87,482.96 85,065.57 20,283.70 2,118.68 6,204.98 51.59 29-3 V5 19,599.84 87,482.96 85,065.57 20,283.70 2,174.98 2,666.66 46.18 31-2 W8 19,599.84 87,482.96 79,413.05 17,948.28 7,124.25 3,077.40 59.17 31-2 W7 16,245.32 78,056.88 79,413.05 17,948.28 3,201.35 9,309.68 58.55 34-3 V6 16,245.32 78,056.88 79,413.05 17,948.28 2,174.98 2,597.25 46.18 37-3 W6 16,245.32 78,056.88 66,141.34 14,447.63 12,458.10 3,436.93 58.55 37-3 W5 12,555.22 62,387.04 66,141.34 14,447.63 3,590.99 14,687.23 58.55 40-3 V7 12,555.22 62,387.04 66,141.34 14,447.63 2,174.98 2,904.54 46.18 43-3 W4 12,555.22 62,387.04 42,240.07 9,654.51 21,689.46 4,605.76 69.54 43-3 W3 8,796.97 43,326.22 42,240.07 9,654.51 4,052.50 17,724.84 47.25 47-7 V1S 8,796.97 43,326.22 0.00 0.00 5,210.38 7,198.44 65.89 52-4 W2 9,636.74 46,367.83 0.00 0.00 47,555.97 11,947.32 103.83 48-5 STRESS ANALYSIS - PAGE 2 0 Job Number. Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 8:43:28 AM NEW MILLENNIUM Location: Joist Description: Mark: ELM.OING SYSTEMS TIGARD,OR Long Span 48LH550/370 J26 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.9266 1.0861 0.6914 1.8874 0.9811 2.2726 0.9552 3528 =3 1/2 x 3 1/2 x.287 BC 1.4375 0.9304 0.5924 1.6850 0.8424 1.2442 0.9613 3025 =3 x 3 x.250 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 3,517.81 748.36 1,122.53 26-8 7/8 21-9 7/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.00 59.00 52.00 57.00 46.00 1.1250 Min Weld Len 2X: Bending Load 586.00 586.00 586.00 586.00 586.00 0.9325 Axial Load 46,909.86 43,646.45 87,482.96 43,326.22 46,367.83 Max Load Fillers TC: fa 12,174.26 11,327.33 22,460.34 11,244.22 12,033.59 98,173.06 Maximum K L/r 66.53 85.33 52.07 82.44 66.53 Max Load no Fillers TC: Fcr 35,058.03 28,719.75 39,519.82 29,709.86 35,058.03 88,393.87 TC OAU Fa 21,034.82 17,231.85 23,711.89 17,825.92 21,034.82 356.04 Ryy: 56.04 Fe 159,559.14 96,991.42 260,514.80 103,917.25 159,559.14 BC DAURyy: Cm 0.9619 0.9416 0.9422 0.9459 0.9623 398.81 Panel Point Moment 13,335.28 13,561.00 9,376.00 12,963.37 12,537.58 BC Stress: Mid Panel Moment 5,657.33 7,800.47 4,688.00 7,081.96 5,453.44 0'99 BC Panel Point fb 7,390.26 7,515.36 5,196.08 7,184.16 6,948.19 123.22 23.2275 Mid Panel fb 1,221.16 1,683.76 1,011.92 1,528.67 1,177.15 TC Shear Stress: Fillers 0 0 0 0 0 11,889.93 Panel Point Stress 19,564.53 18,842.68 27,656.41 18,428.38 18,981.78 BC Shear Stress: Mid Panel Stress 0.6205 0.7184 0.9818 0.6855 0.6123 15,926.92 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 47,892.73 57,194.49 11,675.73 24,521.94 14.79 x 0.218 2 A40B=2.3750 x 0.218 V1S 5,305.26 21,490.90 7,417.82 7,447.58 3.87 x 0.129 2 A22B= 1.5000 x 0.129 W3 4,052.50 28,769.10 17,724.84 19,380.86 7.96 x 0.150 2 A28B= 1.7350 x 0.150 W4 21,689.46 28,624.38 4,605.76 5,035.72 7.79 x 0.188 1 C40BA= 1.125 x 2.014 x .218 V2 1,896.45 14,381.54 4,297.82 5,247.39 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W5 3,590.99 28,769.10 14,687.23 15,684.06 6.59 x 0.150 2 A28B= 1.7350 x 0.150 W6 12,458.10 14,381.54 3,436.93 3,646.46 5.59 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V3 1,896.45 10,742.43 3,972.77 4,049.60 2.07 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W7 3,201.35 28,624.38 9,309.68 10,871.78 3.34 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 W8 7,042.61 10,742.43 2,780.33 2,787.50 3.68 x 0.129 1 C22BB= 1.125 x 1.110 x.129 V4 1,896.45 14,381.54 4,298.35 5,247.39 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W9 2,851.63 28,624.38 8,011.34 9,008.45 2.88 x 0.188 1 CW40BA= 1.5 x 1.926 x .218 W9 2,118.68 24,373.24 6,204.98 7,044.36 2.23 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V5 2,174.98 8,984.69 2,666.66 3,236.21 2.00 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 7,124.25 14,381.54 3,077.40 3,585.25 3.20 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 3,201.35 28,624.38 9,309.68 10,871.78 3.34 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 V6 2,174.98 7,826.93 2,597.25 2,663.49 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 12,458.10 14,381.54 3,436.93 3,646.46 5.59 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 3,590.99 28,769.10 14,687.23 15,684.06 6.59 x 0.150 2 A28B= 1.7350 x 0.150 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 �/� Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 8:43:28 AM NEW MI L L E N N I U M Location: Joist Description: Mark: aLJILOINn wsTFM.S TIGARD,OR Long Span 48LH550/370 J26 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 2,174.98 8,984.69 2,904.54 3,236.21 2.00 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W4 21,689.46 28,624.38 4,605.76 5,035.72 7.79 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W3 4,052.50 28,769.10 17,724.84 19,380.86 7.96 x 0.150 2 A28B= 1.7350 x 0.150 V1S 5,210.38 21,490.90 7,198.44 7,776.96 3.76 x 0.129 2 A22B= 1.5000 x 0.129 W2 47,555.97 48,746.47 11,947.32 19,129.23 16.09 x 0.199 2 A38B=2.2190 x 0.199 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 8:43:28 AM NEW MILLENNIUM Location: Joist Description: Mark: 9LJILOING SYSTEMS TIGARD,OR Long Span 48LH550/370 J26 TCX Design TCX Left TCX Right TCX Length 0-7 1/2 TCX Length 0-9 TCX Type S •TCX Type S TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-9 7/8 Clear Bearing 0-10 1/8 BPL Material:2024=2 x 2 x.248 BPL Material: 2024=2 x 2 x.248 Total Load 550.00 Total Load 550.00 Reqd TL Def L/80 0.09 Reqd TL Def L/80 0.11 Live Load 370.00 Live Load 370.00 Reqd LL Def L/120 0.06 Reqd LL Def L/120 0.08 Section Modulus 1.8044 Section Modulus 1.8044 Reqd SM 0.0689 Reqd SM 0.0924 Mom of Inertia 4.5452 Mom of Inertia 4.5452 Reqd MI 0.0137 Reqd MI 0.0212 Seat Type:T-Plate 1" Seat Type:T-Plate 1" I Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 4 Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:07:55 AM NEW MILLENNIUM Location: Joist Description: Mark: B1"-=""° '' TE^^s TIGARD,OR Long Span 24LH344/230 J27 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-8 32-4 24.00 22.83 L7 @t 4-0 Parallel Chords Variable Left End Right End BC Panel 3-4 3-4 , TC Panel 2-2 2-2 _-,, / ; First Half 1-0 1-0 �� First Diag. 4-4 4-4 Depth 24.00 24.00 - - J Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) LL(1) 230.00 230.00 TC + 0-0 32-8 L-BL Uniform(plf) DL(1) 114.00 114.00 IC + 0-0 32-8 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform(plf) DL(1) 14.00 14.00 TC + 0-0 32-8 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM (1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Uniform(plf) DL(1) 76.00 76.00 BC + 0-0 32-8 L-BL Uniform (plf) IP(1) 54.00 54.00 TC + 0-0 32-8 L-BL Uniform (plf) SM (1) 19.00 19.00 TC + 0-0 32-8 L-BL Additional Shear(Ibs) LL(1) 600.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Conc Load(Ibs) CL(1) 200.00 0.00 TC + 22-11 22-11 L-OAL Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-8 L-BL Axial(Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp (Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp (Ibs) SM(2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 6,908.25 6,922.73 1,730.68 32,097.96 32,534.51 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,734.19 12,879.72 0.00 0.00 13,868.92 2,305.30 44.33 0-2 V1S 1,345.54 12,444.03 0.00 0.00 1,221.83 1,633.22 26.78 2-2 W3 1,345.54 12,444.03 15,367.40 4,363.47 835.77 7,097.15 25.79 3-4 W4 1,939.81 20,467.26 15,367.40 4,363.47 8,032.94 982.73 33.12 4-4 W5 1,939.81 20,467.26 24,570.44 5,414.82 907.76 6,608.08 33.12 6-4 W6 2,845.87 27,956.60 24,570.44 5,414.82 5,569.18 907.76 33.12 8-4 W7 2,845.87 27,956.60 30,306.13 6,213.84 907.76 4,089.18 33.12 10-4 W8 3,518.74 31,938.64 30,306.13 6,213.84 3,041.94 907.76 33.12 12-4 W9 3,518.74 31,938.64 32,534.51 6,760.55 907.76 2,511.18 33.12 14-4 W9 3,518.74 32,097.96 32,534.51 6,760.55 907.76 2,511.18 33.12 16-4 W8 3,518.74 32,097.96 30,616.02 6,213.84 3,041.94 907.76 33.12 18-4 W7 2,845.87 28,215.55 30,616.02 6,213.84 907.76 4,089.18 33.12 20-4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 l/� Job Number. Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:07:55 AM NEW MI L L E N N I U M Location: Joist Description: Mark: eLJILOING SVSTFMS TIGARD,OR Long Span 24LH344/230 J27 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W6 2,845.87 28,215.55 24,778.46 5,414.82 5,569.18 907.76 33.12 22-4 W5 1,920.68 20,624.33 24,778.46 5,414.82 907.76 6,608.08 33.12 24-4 W4 1,920.68 20,624.33 15,473.53 4,363.47 8,032.94 982.73 33.12 26-4 W3 1,052.01 12,524.68 15,473.53 4,363.47 835.77 7,097.15 25.79 28-4 V1S 1,052.01 12,524.68 0.00 0.00 1,221.83 1,633.22 26.78 30-6 W2 1,090.34 12,960.37 0.00 0.00 13,868.92 2,305.30 44.33 29-4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 470.15 1,473.74 22.83 STRESS ANALYSIS - PAGE 2 0 Job Number: Job Name: - Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:07:55 AM N E W MI L L EN N I UM Location: Joist Description: Mark: ALJILMING SYSTEMS TIGARD,OR Long Span 24LH344/230 J27 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.7132 0.6446 0.3831 1.3432 0.6159 0.2963 1.0000 A36B=2.0780 x 0.188 BC 0.5550 0.5933 0.3554 1.2664 0.5563 0.1954 0.9834 A32B= 1.9060 x 0.158 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 326.28 360.61 540.91 17-11 3/4 17-7 7/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 24.00 26.00 24.00 1.1250 Min Weld Len 2X: Bending Load 358.00 358.00 358.00 358.00 358.00 0.5000 Axial Load 12,879.72 12,444.03 32,097.96 12,524.68 12,960.37 Max Load Fillers TC: fa 3,917.90 8,724.08 22,502.78 8,780.63 3,942.44 38,988.17 Maximum K Ur 62.65 67.87 46.99 67.87 62.65 Max Load no Fillers TC: Fcr 37,527.17 35,703.41 42,546.99 35,703.41 37,527.17 35,648.12 TC OAL/ Fa 22,516.30 21,422.04 25,528.20 21,422.04 22,516.30 288.8788.87Ryy: Fe 835,768.25 175,926.64 367,056.81 175,926.64 835,768.25 BC oAL/Ryy: Cm 0.9977 0.9752 0.9589 0.9750 0.9976 306.38 Panel Point Moment 16,569.29 1,779.84 1,432.00 1,786.04 1,786.04 BC Stress: Mid Panel Moment 12,769.69 1,165.14 716.00 857.21 1,313.95 0.98 Panel Point fb 4,752.66 4,391.35 3,533.12 4,406.63 512.30 BC 135.050591 Mid Panel fb 3,662.80 1,210.95 744.15 890.92 454.85 TC Shear Stress: Fillers 0 0 0 0 0 12,741.60 Panel Point Stress 8,670.57 13,115.42 26,035.90 13,187.26 4,454.74 BC Shear Stress: Mid Panel Stress 0.2098 0.4454 0.9050 0.4380 0.1028 16,009.63 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 13,868.92 14,381.54 2,305.30 6,295.69 6.23 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 835.77 14,381.54 7,097.15 8,715.59 3.19 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 8,032.94 8,984.69 982.73 4,646.67 4.58 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 907.76 14,381.54 6,608.08 7,422.65 2.97 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 5,569.18 5,758.64 907.76 2,486.66 4.17 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 907.76 8,984.69 4,089.18 4,646.67 2.33 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 3,041.94 4,802.89 907.76 1,917.58 2.66 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 907.76 7,826.93 2,511.18 3,837.04 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 907.76 7,826.93 2,511.18 3,837.04 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W8 3,041.94 4,802.89 907.76 1,917.58 2.66 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W7 907.76 8,984.69 4,089.18 4,646.67 2.33 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W6 5,569.18 5,758.64 907.76 2,486.66 4.17 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 907.76 14,381.54 6,608.08 7,422.65 2.97 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 8,032.94 8,984.69 982.73 4,646.67 4.58 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W3 835.77 14,381.54 7,097.15 8,715.59 3.19 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W2 13,868.92 14,381.54 2,305.30 6,295.69 6.23 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V1 1,221.83 4,802.89 1,633.22 2,583.71 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 470.15 4,802.89 1,473.74 3,000.33 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS -PAGE 3 Job Number Job Name: Date Run. 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/201911:07:55 AM N E W M I L L E N N I U M Location: Joist Description: Mark: aUILOING SYSTEMS TIGARD,OR Long Span 24LH344/230 J27 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-5 1/8 BPL Length 2-9 1/8 Clear Bearing 0-10 3/8 Clear Bearing 0-10 3/8 BPL Material:2024=2 x 2 x.248 BPL Material: 2024=2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def L/80 0.00 Live Load 230.00 Live Load 230.00 Reqd LL Def L/160 0.20 Reqd LL Def L/120 0.00 Section Modulus 2.8888 Section Modulus 2.8888 Reqd SM 0.5523 Reqd SM 0.0000 Mom of Inertia 5.5292 Morn of Inertia 5.5292 Reqd MI 0.5828 Reqd MI 0.0000 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c:DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS -PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:59:50 PM NEW MILLENNIUM Location: Joist Description: Mark: aLELTEN° SYSTEMS TIGARD,OR Long Span 24LH344/230 J29 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-7 1/2 32-3 1/2 24.00 22.48 7 Special Parallel Chords Variable Left End Right End BC Panel 3-4 3-2 7/8 TC Panel 2-2 2-1 � z /,,, ,,,\ v , First Half 1-0 5/8 1-0 - First Diag. 4-4 5/8 4-2 7/8 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 230.00 230.00 TC + 0-0 32-7 1/2 L-BL Uniform (plf) DL(1) 114.00 114.00 TC + 0-0 32-7 1/2 L-BL Uniform (plf) DL(1) 22.00 22.00 TC + 0-0 32-7 1/2 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Additional Shear(Ibs) LL(1) 600.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 76.00 76.00 BC + 0-0 32-7 1/2 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM (1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) SM (1) 19.00 19.00 TC + 0-0 32-7 1/2 L-BL Uniform (plf) IP(1) 54.00 54.00 TC + 0-0 32-7 1/2 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc w/bending(Ibs) CL(1) 3,000.00 0.00 TC + 8-3 8-3 L-OAL Conc Load (Ibs) LL(1) 4,000.00 0.00 TC + 18-3 1/2 19-4 1/2 L-OAL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM(1) 400.00 0.00 TC + Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-7 1/2 L-BL Axial(Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc Load (Ibs) LL(2) 4,000.00 0.00 TC - 18-3 1/2 19-4 1/2 L-OAL Conc @ any pp(Ibs) SM(2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL (2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 33.50 57.50 11,520.07 9,445.19 2,880.02 51,081.32 50,721.09 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 4,476.79 19,866.94 0.00 0.00 23,005.19 5,401.93 44.15 0-2 V1S 4,046.75 19,408.38 0.00 0.00 3,274.42 4,148.33 26.48 2-2 W3 4,046.75 19,408.38 24,782.71 7,223.10 2,425.46 12,463.00 25.78 3-4 W4 7,236.54 32,928.43 24,782.71 7,223.10 13,007.03 3,049.23 32.88 4-4 5/8 V2 7,236.54 32,928.43 24,782.71 7,223.10 2,084.29 5,342.85 22.48 6-4 5/8 W5 7,236.54 32,928.43 38,307.63 11,146.74 3,049.23 10,352.64 32.88 6-4 5/8 W6 11,417.01 43,257.23 38,307.63 11,146.74 9,281.75 3,049.23 32.88 8-4 5/8 V3 11,417.01 43,257.23 38,307.63 11,146.74 2,084.29 3,578.02 22.48 10-45/8 W7 11,417.01 43,257.23 47,068.46 14,878.17 3,049.23 7,766.13 32.88 10-4 5/8 W8 16,424.88 51,081.32 47,068.46 14,878.17 6,136.88 3,741.06 40.34 12-4 5/8 *Continued on Next Page... STRESS ANALYSIS -PAGE 1 0 Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:59:50 PM NEW MILLENNIUM Location: Joist Descnption: Mark: aLJILMI r. SYSTEMS TIGARD, OR Long Span 24LH344/230 J29 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. V4 16,424.88 51,081.32 47,068.46 14,878.17 2,084.29 3,751.68 22.48 15-21/8 W9 16,424.88 51,081.32 50,721.09 17,495.83 4,734.26 3,114.54 33.62 15-21/8 W9 15,350.94 48,864.49 50,721.09 17,495.83 2,429.02 4,351.97 26.22 17-31/8 V5 15,350.94 48,864.49 50,721.09 17,495.83 1,439.74 2,041.36 22.48 18-4 5/8 W8 15,350.94 48,864.49 44,660.72 14,588.29 6,695.24 3,046.27 32.88 18-4 5/8 W7 10,988.81 39,675.29 44,660.72 14,588.29 3,049.23 7,766.13 32.88 20-4 5/8 V6 10,988.81 39,675.29 44,660.72 14,588.29 1,439.74 2,040.90 22.48 22-4 5/8 W6 10,988.81 39,675.29 33,583.60 10,695.45 9,281.75 3,049.23 32.88 22-4 5/8 W5 6,626.69 27,102.82 33,583.60 10,695.45 3,049.23 10,352.64 32.88 24-4 5/8 V7 6,626.69 27,102.82 33,583.60 10,695.45 1,439.74 2,040.45 22.48 26-4 5/8 W4 6,626.69 27,102.82 19,738.54 6,610.40 13,007.03 3,049.23 32.88 26-4 5/8 W3 3,355.10 15,669.17 19,738.54 6,610.40 2,405.87 10,015.52 25.48 28-4 5/8 V1S 3,355.10 15,669.17 0.00 0.00 3,274.42 4,148.33 26.41 30-61/2 W2 3,357.50 16,107.93 0.00 0.00 18,626.94 4,243.72 43.18 29-4 5/8 STRESS ANALYSIS - PAGE 2 ,, Job Number. Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:59:50 PM NEW MI L L E N N I LJ M Location: Joist Description: Mark: BUILoINIM SYSTEMS TIGARD,OR Long Span 24LH344/230 J29 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 1.1207 0.8991 0.5436 1.6512 _ 0.8225 0.9058 0.9280 A44A=2.8750 x.209 BC 0.9485 0.7361 0.4403 1.4631 0.7019 0.5140 1.0000 A40B=2.3750 x 0.218 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 521.85 579.00 868.49 22-1 1/4 16-6 7/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.63 33.50 25.88 23.00 1.1250 Min Weld Len 2X: Bending Load 366.00 366.00 366.00 366.00 366.00 0.5504 Axial Load 19,866.94 19,408.38 51,081.32 15,669.17 16,107.93 Max Load Fillers TC: fa 4,842.76 8,659.04 22,789.92 6,990.80 3,926.46 57,369.77 Maximum K Ur 44.15 48.98 46.22 47.60 42.31 Max Load no Fillers TC: For 40,650.88 39,429.20 40,138.28 39,787.30 41,091.95 52,935.76 Fa 24,390.53 23,657.52 24,082.97 23,872.38 24,655.17 TCOAURyy: 234.68 Fe 839,250.44 326,388.25 366,523.31 345,583.53 913,815.19 BC OAL'1?yy. Cm 0.9971 0.9867 0.9583 0.9899 0.9979 264.85 _Panel Point Moment 16,569.39 6,801.65 2,852.39 1,807.31 1,807.31 BC Stress: Mid Panel Moment 12,300.11 3,878.85 1,426.19 865.38 1,130.57 0.89 Panel Point fb 4,139.48 7,706.11 3,231.69 2,047.65 451.52 13 .59: 30.5928 Mid Panel fb 3,072.90 4,394.65 647.52 392.90 288.65 TC Shear Stress: Fillers 0 0 0 0 0 12,697.88 Panel Point Stress 8,982.24 16,365.16 26,021.60 9,038.44 4,377.98 BC Shear Stress: Mid Panel Stress 0.2104 0.5109 0.9684 0.3057 0.0900 15,469.89 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 23,005.19 24,373.24 5,401.93 10,063.55 8.26 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1S 3,274.42 7,826.93 4,148.33 4,501.38 2.74 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W3 2,425.46 24,373.24 12,463.00 14,149.32 4.48 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 13,007.03 14,381.54 3,049.23 7,464.43 5.84 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 2,084.29 8,984.69 5,342.85 5,872.90 3.05 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 3,049.23 24,373.24 10,352.64 11,995.81 3.72 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 9,281.75 10,742.43 3,049.23 5,736.06 4.85 x 0.129 1 C22BB= 1.125 x 1.110 x.129 V3 2,084.29 5,758.64 3,578.02 3,731.49 2.68 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 3,049.23 16,730.22 7,766.13 8,341.56 3.31 x 0.158 1 C32BA= 1.125 x 1.520 x .158 W8 6,136.88 8,984.69 3,741.06 3,853.18 3.50 x 0.118 1 C18BB= 1.125 x 1.035 x .118 V4 2,084.29 7,826.93 3,751.68 4,936.88 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 4,734.26 7,826.93 3,114.54 3,789.69 3.13 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 2,429.02 7,826.93 4,351.97 4,528.80 2.87 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V5 1,439.74 4,802.89 2,041.36 3,025.15 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W8 6,695.24 7,826.93 3,046.27 3,860.25 4.42 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 3,049.23 16,730.22 7,766.13 8,341.56 3.31 x 0.158 1 C32BA= 1.125 x 1.520 x.158 V6 1,439.74 4,802.89 2,040.90 3,025.15 2.00 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W6 9,281.75 10,742.43 3,049.23 5,736.06 4.85 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W5 3,049.23 24,373.24 10,352.64 11,995.81 3.72 x 0.188 1 C38BA= 1.125 x 1.845 x.199 Continued on Next Page... STRESS ANALYSIS -PAGE 2 ' Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:59:50 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILOING SYSTEMS TIGARD, OR Long Span 24LH344/230 J29 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 1,439.74 4,802.89 2,040.45 3,025.15 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W4 13,007.03 14,381.54 3,049.23 7,464.43 5.84 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W3 2,405.87 18,714.09 10,015.52 11,311.50 3.83 x 0.176 1 C34AA= 1.125 x 1.549 x .176 V1 S 3,274.42 7,826.93 4,148.33 4,508.29 2.74 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W2 18,626.94 18,714.09 4,243.72 8,295.31 7.13 x 0.176 1 C34AA= 1.125 x 1.549 x.176 STRESS ANALYSIS - PAGE 3 G� Job Number Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:59:50 PM NEW MILLENNIUM Location: Joist Description: Mark: AUIL CIING SYSTEMS TIGARD, OR Long Span 24LH344/230 J29 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 1/2 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-3 1/8 BPL Length 2-6 5/8 Clear Bearing 0-9 3/4 Clear Bearing 0-9 7/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024 =2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def L/80 0.01 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L/120 0.00 Section Modulus 3.9167 Section Modulus 3.9167 Reqd SM 0.5523 Reqd SM 0.0030 Mom of Inertia 6.9287 Mom of Inertia 6.9287 Reqd MI 0.5845 Reqd MI 0.0002 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f:DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+A)(+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:06:57 AM NEW NI I L L E N N I U NI Location: Joist Description: Mark: 6LELO1NG SYSTEMS TIGARD,OR Long Span 24LH344/230 J30 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-7 1/2 32-3 1/2 24.00 22.87 7 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-4 3-3 1/2 TC Panel 2-2 2-2 - �., i �, First Half 1-0 1-0 ! i ' Mill ; 11111111iaJJ1L • LI1Ifi diJI11ll1Lattllfll ! I !-7 First Diag. 4-4 4-3 1/2 Depth 24.00 24.00 !' Loads Load Type Category Load1 Load2 Position L Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 230.00 230.00 TC + 0-0 32-7 1/2 L-BL Uniform(plf) DL(1) 114.00 114.00 TC + 0-0 32-7 1/2 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform(plf) DL(1) 13.00 13.00 TC + 0-0 32-7 1/2 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM(1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) DL(1) 76.00 76.00 BC + 0-0 32-7 1/2 L-BL Uniform (plf) IP(1) 54.00 54.00 TC + 0-0 32-7 1/2 L-BL Uniform(plf) SM (1) 19.00 19.00 TC + 0-0 32-7 1/2 L-BL Additional Shear(Ibs) LL(1) 600.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp (Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-7 1/2 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 6,807.81 6,776.53 1,701.95 31,194.25 31,696.47 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,730.66 12,696.30 0.00 0.00 13,564.03 2,301.75 44.35 0-2 V1S 1,342.68 12,262.64 0.00 0.00 1,222.89 1,628.71 26.81 2-2 W3 1,342.68 12,262.64 15,129.94 4,359.74 835.46 6,977.62 25.82 3-4 W4 1,935.42 20,121.13 15,129.94 4,359.74 7,878.63 982.74 33.15 4-4 W5 1,935.42 20,121.13 24,119.46 5,407.96 906.79 6,457.96 33.15 6-4 W6 2,837.61 27,404.10 24,119.46 5,407.96 5,422.91 906.79 33.15 8-4 W7 2,837.61 27,404.10 29,656.02 6,204.29 906.79 3,947.15 33.15 10-4 W8 3,508.00 31,194.25 29,656.02 6,204.29 2,912.10 906.79 33.15 12-4 W9 3,508.00 31,194.25 31,696.47 6,744.36 906.79 2,467.25 33.15 14-4 W9 3,502.31 31,173.43 31,696.47 6,744.36 906.79 2,467.25 33.15 16-4 W8 3,502.31 31,173.43 29,617.65 6,197.29 2,912.10 906.79 33.15 18-4 W7 2,829.30 27,348.19 29,617.65 6,197.29 906.79 3,947.15 33.15 20-4 W6 2,829.30 27,348.19 24,045.99 5,398.34 5,422.91 906.79 33.15 22-4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number. Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:06:57 AM NEW M I L L E N N I U M Location: Joist Description: Mark: aLIILoING SYSTEMS TIGARD,OR Long Span 24LH344/230 J30 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W5 1,904.40 20,030.12 24,045.99 5,398.34 906.79 6,457.96 33.15 24-4 W4 1,904.40 20,030.12 15,021.39 4,347.50 7,878.63 982.74 33.15 26-4 W3 1,036.57 12,149.04 15,021.39 4,347.50 835.46 6,977.62 25.82 28-4 V1S 1,036.57 12,149.04 0.00 0.00 699.58 1,604.25 26.56 30-51/2 W2 1,073.10 12,563.03 0.00 0.00 13,438.13 1,635.07 43.92 29-4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 470.11 1,458.87 22.87 STRESS ANALYSIS - PAGE 2 ' Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:06:57 AM NEW MILLENNIUM Location: Joist Description: Mark: ELELoItiG SYSTEMS TIGARD, OR Long Span 24LH344/230 J30 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.6209 0.6011 0.3559 1.2877 0.5763 0.2243 1.0000 A34A= 1.9380 x 0.176 BC 0.5550 0.5933 0.3554 1.2664 0.5563 0.1954 0.9834 A32B = 1.9060 x 0.158 Axial and Bending Analysis K. Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Brldg BC: 0.75 50,000.00 30,000.00 307.32 340.98 511.46 17-2 7/8 17-8 1/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 24.00 25.50 24.00 1.1250 Min Weld Len 2X.' Bending Load 357.00 357.00 357.00 357.00 357.00 0.5000 Axial Load 12,696.30 12,262.64 31,194.25 12,149.04 12,563.03 Max Load Fillers TC: fa 4,091.88 9,874.89 25,120.19 9,783.41 4,048.93 33,342.73 Maximum K L/r 67.43 73.05 33.72 71.65 67.43 Max Load no Fillers TC: Fcr 35,856.57 33,845.36 46,011.85 34,352.20 35,856.57 30,057.71 TC Fa 21,513.95 20,307.22 27,607.11 20,611.32 21,513.95 300.93 yy 00.93 F'e 831,498.50 152,983.48 319,187.78 159,041.66 831,498.50 BCOAL/Ryy: Cm 0.9975 0.9677 0.9473 0.9692 0.9976 305.98 Panel Point Moment 16,569.29 1,735.29 1,428.00 1,697.49 1,697.50 BC Stress: Mid Panel Moment 12,796.22 1,110.77 714.00 816.25 1,278.38 0.95 BC L Panel Point fb 4,865.39 5,267.37 4,334.61 5,152.65 498.45 135: 5.0 591 Mid Panel fb 3,757.47 1,426.97 917.25 1,048.60 486.38 TC Shear Stress: Fillers 0 0 4 0 0 14,484.04 Panel Point Stress 8,957.27 15,142.26 29,454.80 14,936.06 4,547.38 BC shear Stress: Mid Panel Stress 0.2211 0.5321 0.9396 0.5082 0.1104 15,674.60 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 13,564.03 15,057.20 2,301.75 6,985.86 5.78 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W3 835.46 14,381.54 6,977.62 8,709.24 3.13 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 7,878.63 10,742.43 982.74 5,701.05 4.11 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 906.79 14,381.54 6,457.96 7,417.94 2.90 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 5,422.91 7,826.93 906.79 3,834.42 3.58 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W7 906.79 8,984.69 3,947.15 4,643.62 2.25 x 0.118 1 C18BB = 1.125 x 1.035 x .118 W8 2,912.10 4,802.89 906.79 1,914.86 2.55 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W9 906.79 5,758.64 2,467.25 2,483.45 2.00 x 0.090 1 C12BB = 1.125 x 0.799 x.090 W9 906.79 5,758.64 2,467.25 2,483.45 2.00 x 0.090 1 C12BB = 1.125 x 0.799 x.090 W8 2,912.10 4,802.89 906.79 1,914.86 2.55 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W7 906.79 8,984.69 3,947.15 4,643.62 2.25 x 0.118 1 C18BB = 1.125 x 1.035 x.118 W6 5,422.91 7,826.93 906.79 3,834.42 3.58 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W5 906.79 14,381.54 6,457.96 7,417.94 2.90 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W4 7,878.63 10,742.43 982.74 5,701.05 4.11 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 835.46 14,381.54 6,977.62 8,709.24 3.13 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W2 13,438.13 15,057.20 1,635.07 7,055.49 5.73 x 0.158 1 C32BA= 1.125 x 1.520 x.158 V1 1,222.89 4,802.89 1,628.71 2,580.04 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 470.11 4,802.89 1,458.87 2,997.55 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:06:57 AM NEW MILLENNIUM Location: Joist Description: Mark: A, I-311,1r. SYSTEMS TIGARD,OR Long Span 24LH344/230 J30 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 1/2 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-5 1/8 BPL Length 2-9 3/8 Clear Bearing 0-10 1/4 Clear Bearing 0-10 BPL Material:2024=2 x 2 x.248 BPL Material:2024 =2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def L/80 0.01 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L/120 0.00 Section Modulus 2.6283 Section Modulus 2.6283 Reqd SM 0.5523 Reqd SM 0.0030 Mom of Inertia 5.1921 Mom of Inertia 5.1921 Reqd MI 0.5845 Reqd MI 0.0002 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c:DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:14:02 AM NEW MI L L E N N I UM Location: Joist Description: Mark: SUILoiN❑ SYSTEMS TIGARD,OR Long Span 24LH344/230 J31 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-7 1/2 32-3 1/2 - 24.00 22.48 7 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-4 3-3 1/2 TC Panel 2-2 2-2 First Half 1-0 1-0 First Diag. 4-4 4-3 1/2 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 230.00 230.00 TC + 0-0 32-7 1/2 L-BL Uniform (plf) DL(1) 114.00 114.00 TC + 0-0 32-7 1/2 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) DL(1) 21.00 21.00 TC + 0-0 32-7 1/2 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM (1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) DL(1) 76.00 76.00 BC + 0-0 32-7 1/2 L-BL Uniform (plf) IP(1) 54.00 54.00 TC + 0-0 32-7 1/2 L-BL Uniform (plf) SM(1) 19.00 19.00 TC + 0-0 32-7 1/2 L-BL Additional Shear(Ibs) LL(1) 600.00 0.00 TC + 0-0 0-0 L-BL Conc w/bending (lbs) CL(1) 3,000.00 0.00 TC + 8-3 8-3 L-OAL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 18-11 1/2 18-11 1/2 L-OAL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-7 1/2 L-BL Axial(Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM(2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear. Max TC Comp.: Max BC Tension 24.00 48.00 10,935.68 8,906.99 2,733.92 48,477.26 49,996.31 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,760.82 19,843.97 0.00 0.00 21,830.76 2,331.27 44.15 0-2 V1S 1,366.09 19,392.37 0.00 0.00 1,244.13 1,691.63 26.48 2-2 W3 1,366.09 19,392.37 24,500.40 4,383.44 838.63 11,655.48 25.48 3-4 W4 1,969.16 32,741.01 24,500.40 4,383.44 12,283.53 991.76 32.88 4-4 V2 1,969.16 32,741.01 24,500.40 4,383.44 466.45 3,358.64 22.48 6-4 W5 1,969.16 32,741.01 37,952.20 5,449.94 915.11 9,513.87 32.88 6-4 W6 2,887.08 42,420.16 37,952.20 5,449.94 8,445.91 915.11 32.88 8-4 V3 2,887.08 42,420.16 37,952.20 5,449.94 469.01 1,531.88 22.48 10-4 W7 2,887.08 42,420.16 45,820.31 6,260.15 915.11 6,933.21 32.88 10-4 W8 3,569.15 48,477.26 45,820.31 6,260.15 5,865.25 915.11 32.88 12-4 V4 3,569.15 48,477.26 45,820.31 6,260.15 470.28 1,623.79 22.48 14-4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:14:02 AM NEW MILLENNIUM Location: Joist Description: Mark: aLIILoING SYSTEMS TIGARD,OR Long Span 24LH3441230 J31 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W9 3,569.15 48,477.26 49,996.31 6,809.63 915.11 4,352.55 32.88 14-4 W9 3,563.36 47,318.40 49,996.31 6,809.63 915.11 4,352.55 32.88 16-4 V5 3,563.36 47,318.40 49,996.31 6,809.63 470.28 1,555.51 22.48 18-4 W8 3,563.36 47,318.40 43,572.67 6,253.03 5,865.25 915.11 32.88 18-4 W7 2,878.62 39,083.73 43,572.67 6,253.03 915.11 6,933.21 32.88 20-4 V6 2,878.62 39,083.73 43,572.67 6,253.03 468.99 1,515.21 22.48 22-4 W6 2,878.62 39,083.73 33,526.97 5,440.15 8,445.91 915.11 32.88 22-4 W5 1,937.60 27,227.00 33,526.97 5,440.15 915.11 9,513.87 32.88 24-4 V7 1,937.60 27,227.00 33,526.97 5,440.15 466.42 1,456.07 22.48 26-4 W4 1,937.60 27,227.00 19,899.78 4,370.99 12,283.53 991.76 32.88 26-4 W3 1,054.64 15,852.96 19,899.78 4,370.99 838.63 11,655.48 25.48 28-4 V1S 1,054.64 15,852.96 0.00 0.00 702.76 1,649.16 26.22 30-51/2 W2 1,091.81 16,284.08 0.00 0.00 17,737.90 1,655.90 43.72 29-4 STRESS ANALYSIS - PAGE 2 l/� Job Number: Job Name: Date Run: �/� 5618 OOD7 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:14:02 AM NEW MILLENNIUM Location: Joist Description: Mark: BUILo,tiG S`eSTFMS TIGARD,OR Long Span 24LH344/230 J31 Chord Properties Chord _ Area Rx Rz Ryy Y lx Q Material TC 1.1207 0.8991 0.5436 1.6512 0.8225 0.9058 0.9280 A44A=2.8750 x.209 BC 0.9485 0.7361 0.4403 1.4631 0.7019 0.5140 1.0000 A40B=2.3750 x 0.218 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 521.85 579.00 868.49 22-1 1/4 26-6 7/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 24.00 25.50 24.00 1.1250 Bendin Load 365.00 365.00 365.00 365.00 365.00 0..5WeldLen2X: 9 0.5000 Axial Load 19,843.97 19,392.37 48,477.26 15,852.96 16,284.08 Max Load Fillers TC: fa 4,837.16 8,651.90 14,607.39 7,072.79 3,969.40 51,951.30 Maximum K Lir 44.15 47.83 33.11 46.91 44.15 Max Load no Fillers TC: Fcr 40,650.88 39,728.11 43,072.44 39,963.70 40,650.88 49,854.73 Fa 24,390.53 23,836.86 25,843.46 23,978.22 24,390.53 234.68 2 yy. 4.68 F'e 839,250.44 342,268.59 714,116.00 355,822.47 839,250.44 BCOAL/Ryy: Cm 0.9971 0.9874 0.9863 0.9901 0.9976 264.85 Panel Point Moment 16,569.39 6,526.34 12,006.88 1,796.54 1,796.55 BC Stress: Mid Panel Moment 12,300.63 3,720.19 8,640.16 812.47 1,288.09 0.88 Panel Point fb 4,139.48 7,394.19 13,603.51 2,035.44 448.83 BC 109.010166 Mid Panel fb 3,073.03 4,214.89 3,922.79 368.88 328.87 TC Shear Stress: Fillers 0 0 0 0 0 12,049.64 Panel Point Stress 8,976.64 16,046.09 28,210.90 9,108.24 4,418.23 BC Shear Stress: Mid Panel Stress 0.2103 0.5017 0.6931 0.3070 0.0933 14,680.14 Web Design Member Web Tension Allow Tension Web Comp Allow Camp Weld Qty Material W2 21,830.76 24,373.24 2,331.27 10,063.55 7.84 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1S 1,244.13 4,802.89 1,691.63 2,616.26 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W3 838.63 24,373.24 11,655.48 14,243.97 4.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 12,283.53 14,381.54 991.76 7,464.43 5.51 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 466.45 5,758.64 3,358.64 3,731.49 2.51 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 915.11 18,714.09 9,513.87 9,600.97 3.64 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 8,445.91 8,984.69 915.11 4,673.73 4.82 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V3 469.01 4,802.89 1,531.88 3,025.15 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W7 915.11 14,381.54 6,933.21 7,464.43 3.11 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 5,865.25 7,826.93 915.11 3,860.25 3.87 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V4 470.28_ 4,802.89 1,623.79 3,025.15 2.00 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W9 915.11 8,984.69 4,352.55 4,673.73 2.48 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W9 915.11 8,984.69 4,352.55 4,673.73 2.48 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V5 470.28 4,802.89 1,555.51 3,025.15 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W8 5,865.25 7,826.93 915.11 3,860.25 3.87 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 915.11 14,381.54 6,933.21 7,464.43 3.11 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V6 468.99 4,802.89 1,515.21 3,025.15 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W6 8,445.91 8,984.69 915.11 4,673.73 4.82 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 915.11 18,714.09 9,513.87 9,600.97 3.64 x 0.176 1 C34AA= 1.125 x 1.549 x.176 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 0 Job Number: Job Name. Date Run: 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:14:02 AM NEW M I L L EN N I UM Location: Joist Description: Mark: BUILaING SYSTEM= TIGARD,OR Long Span 24LH344/230 J31 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 466.42 4,802.89 1,456.07 3,025.15 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W4 12,283.53 14,381.54 991.76 7,464.43 5.51 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 838.63 24,373.24 11,655.48 14,243.97 4.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1S 702.76 4,802.89 1,649.16 2,644.64_ 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W2 17,737.90 18,714.09 1,655.90 8,193.16 6.79 x 0.176 1 C34AA= 1.125 x 1.549 x.176 STRESS ANALYSIS - PAGE 3 11 Job Number: Job Name. Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:14:02 AM NEW MILLENNIUM Location: Joist Description: Mark: a�11_oING SYSTEMS TIGARD, OR Long Span 24LH344/230 J31 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 1/2 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-5 BPL Length 2-9 3/8 Clear Bearing 0-9 7/8 Clear Bearing 0-10 1/8 BPL Material:2024=2 x 2 x.248 BPL Material: 2024=2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def U80 0.01 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def U120 0.00 Section Modulus 3.9167 Section Modulus 3.9167 Reqd SM 0.5523 Reqd SM 0.0030 Mom of Inertia 6.9287 Mom of Inertia 6.9287 Reqd MI 0.5845 Reqd MI 0.0002 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)*0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 //1♦ Job Number: Job Name: Date Run: �J 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:01:07 PM NEW MILLENNIUM Location: Joist Description: Mark: aIJILo,NG SYSTEMS TIGARD,OR Long Span 24LH344/230 J32 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-8 32-4 24.00 22.35 �7 Special Parallel Chords Variable Left End Right End BC Panel 3-4 3-4 ;,, , TC Panel 2-2 2-2 ce - First Half 1-0 1-0 ' u,.,..: ,., 'r� �� �... '. ... ,. ... ,..m. First Diag. 4-4 4-4 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction i Loc/Begin I Sp/End Reference i Uniform(pif) DL(1) 114.00 114.00 TC + 0-0 32-8 L-BL Uniform(plf) , _ LL (1) 230.00 230.00 TC + 0-0 32-8 L-BL Uniform(plf) SM (1) 19.00 19.00 TC + 0-0 32-8 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 22.00 22.00 TC + 0-0 32-8 L-BL Uniform (pif) DL(1) 76.00 76.00 BC + 0-0 32-8 L-BL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Additional Shear(Ibs) LL (1) 600.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) LL (1) 85.00 85.00 TC + 0-0 32-8 L-BL Axial(Ibs) _ SM (1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp(Ibs) _ WL(1) 400.00 0.00 TC + Uniform (plf) IP(1) 54.00 54.00 TC + 0-0 32-8 L-BL Conc Load(Ibs) LL (1) 4,000.00 0.00 TC + 18-3 1/2 19-4 1/2 L-OAL Uniform(plf) LL (1) 0.00 466.00 TC + 21-9 7/8 33-3 7/8 L-OAL Conc Load(Ibs) CL(1) 2,000.00 0.00 TC + 33-10 33-10 L-OAL Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-8 L-BL Axial(Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Conc Load(Ibs) LL(2) 4,000.00 0.00 TC - 18-3 1/2 19-4 1/2 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 33.50 57.50 10,970.70 15,055.21 3,763.80 57,129.46 58,166.34 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 4,500.65 18,126.93 0.00 0.00 27,783.95 5,427.78 44.09 0-2 V1S 4,068.29 17,588.41 0.00 0.00 3,282.27 6,871.37 26.38 2-2 W3 4,068.29 17,588.41 22,085.24 7,198.01 2,405.12 12,337.25 25.37 3-4 W4 7,220.27 31,100.23 22,085.24 7,198.01 13,560.19 3,061.59 32.80 4-4 V2 7,220.27 31,100.23 22,085.24 7,198.01 2,086.73 3,711.13 22.35 6-4 W5 7,220.27 31,100.23 38,861.27 11,146.01 3,061.59 11,676.51 32.80 6-4 W6 11,422.92 45,653.95 38,861.27 11,146.01 10,353.12 3,061.59 32.80 8-4 V3 11,422.92 45,653.95 38,861.27 11,146.01 2,086.73 3,762.43 22.35 10-4 Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:01:07 PM NEW MILLENNIUM Location: Joist Description: Mark: PI III rIING GvsTFMG TIGARD,OR Long Span 24LH344/230 J32 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W7 11,422.92 45,653.95 51,119.57 14,900.77 3,061.59 8,539.58 32.80 10-4 W8 16,457.34 57,129.46 51,119.57 14,900.77 8,539.29 3,759.39 40.27 12-4 V4 16,457.34 57,129.46 51,119.57 14,900.77 2,086.73 3,991.40 22.35 15-11/2 W9 16,457.34 57,129.46 58,166.34 17,665.62 2,416.92 5,646.50 33.54 15-11/2 W9 15,533.87 56,888.32 58,166.34 17,665.62 2,906.19 4,396.86 26.12 17-21/2 V5 15,533.87 56,888.32 58,166.34 17,665.62 1,437.30 2,038.92 22.35 18-4 W8 15,533.87 56,888.32 53,548.02 14,744.89 5,522.13 3,051.71 32.80 18-4 W7 11,147.84 49,098.08 53,548.02 14,744.89 3,061.59 8,539.58 32.80 20-4 V6 11,147.84 49,098.08 53,548.02 14,744.89 1,437.30 2,038.46 22.35 22-4 W6 11,147.84 49,098.08 43,070.87 10,834.25 10,353.12 3,061.59 32.80 22-4 W5 6,761.80 35,651.52 43,070.87 10,834.25 3,061.59 11,676.51 32.80 24-4 V7 6,761.80 35,651.52 43,070.87 10,834.25 1,437.30 2,206.56 22.35 26-4 W4 6,761.80 35,651.52 26,413.19 6,730.37 13,560.19 3,061.59 32.80 26-4 W3 3,472.28 20,920.27 26,413.19 6,730.37 2,405.12 12,337.25 25.37 28-4 V1S 3,472.28 20,920.27 0.00 0.00 3,282.27 6,871.37 26.38 30-6 W2 3,472.28 22,864.07 0.00 0.00 27,783.95 5,427.78 44.09 29-4 STRESS ANALYSIS - PAGE 2 .0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:01:07 PM NEW NI I L L E N N I U NI Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 24LH344/230 J32 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.1207 0.8991 0.5436 1.6512 0.8225 0.9058 0.9280 A44A=2.8750 x.209 BC 1.1207 0.8991 0.5436 1.6512 0.8225 0.9058 0.9280 A44A=2.8750 x.209 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bndg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 563.69 623.00 934.50 22-1 1/4 20-2 7/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 33.50 26.00 24.00 1.1250 Min Weld Len 2X: Bending Load 451.00 451.00 451.00 815.58 884.11 0.6156 Axial Load 18,126.93 17,588.41 57,129.46 20,920.27 22,864.07 Max Load Fifers TC: fa 4,418.62 7,847.06 25,488.29 9,333.57 5,573.34 57,038.39 Maximum K L/r 44.15 47.83 30.81 47.83 44.15 Max Load no Fillers TC: Fcr 40,650.88 39,728.11 43,504.19 39,728.11 40,650.88 52,631.07 TC Fa 24,390.53 23,836.86 26,102.51 23,836.86 24,390.53 234.9834.98 w. Fe 839,250.44 342,268.59 366,523.31 342,268.59 839,250.44 BC OAURyy: Cm 0.9974 0.9885 0.9534 0.9864 0.9967 234.98 Panel Point Moment 16,569.31 2,431.90 3,514.82 4,307.28 4,307.29 BC Stress: Mid Panel Moment 12,386.78 1,712.75 1,757.41 1,912.94 3,279.44 0.87 BC Panel Point fb 4,139.46 2,755.29 3,982.21 4,880.05 1,076.08 1 : 05.77 63 Mid Panel fb 3,094.55 777.62 797.90 868.51 837.29 TC Shear Stress: Fillers 0 0 2 0 0 15,284.45 Panel Point Stress 8,558.08 10,602.35 29,470.51 14,213.62 6,649.42 BC shear Stress: Mid Panel Stress 0.2024 0.3547 1.0039 0.4202 0.2554 15,284.45 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 27,783.95 28,624.38 5,427.78 11,601.40 9.98 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1S 3,282.27 14,381.54 6,871.37 8,609.56 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 2,405.12 24,373.24 12,337.25 14,277.58 4.43 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 13,560.19 14,381.54 3,061.59 7,478.66 6.09 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 2,086.73 5,758.64 3,711.13 3,741.07 2.78 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 3,061.59 24,373.24 11,676.51 12,020.02 4.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 10,353.12 10,742.43 3,061.59 5,746.77 5.40 x 0.129 1 C22BB = 1.125 x 1.110 x.129 V3 2,086.73 7,826.93 3,762.43 4,950.54 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W7 3,061.59 18,714.09 8,539.58 9,619.62 3.27 x 0.176 1 C34AA= 1.125 x 1.549 x .176 W8 8,539.29 8,984.69 3,759.39 3,860.39 4.87 x 0.118 1 C18BB= 1.125 x 1.035 x .118 V4 2,086.73 7,826.93 3,991.40 4,950.54 2.64 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 2,416.92 10,742.43 5,646.50 5,650.69 2.95 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W9 2,906.19 7,826.93 4,396.86 4,539.69 2.90 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V5 1,437.30 4,802.89 2,038.92 3,033.68 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W8 5,522.13 7,826.93 3,051.71 3,868.17 3.65 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 3,061.59 18,714.09 8,539.58 9,619.62 3.27 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V6 1,437.30 4,802.89 2,038.46 3,033.68 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W6 10,353.12 10,742.43 3,061.59 5,746.77 5.40 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 3,061.59 24,373.24 11,676.51 12,020.02 4.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 /' Job Number: Job Name: Date Run: �! 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:01:07 PM NEW MI L LE N N I UM Location: Joist Description: Mark: aLJILoItiG SYSTEMS TIGARD,OR Long Span 24LH3441230 J32 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld _ Qty Material V7 1,437.30 4,802.89 2,206.56 3,033.68 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W4 13,560.19 14,381.54 3,061.59 7,478.66_ 6.09 x 0.150 _ 1 C28BB= 1.125 x 1.344 x.150 W3 2,405.12 24,373.24 12,337.25 14,277.58 4.43 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1S 3,282.27 14,381.54 6,871.37 8,609.56 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W2 27,783.95 28,624.38 5,427.78 11,601.40 9.98 x 0.188 1 C40BA= 1.125 x 2.014 x.218 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:01:07 PM NEW MI L L E N N I UM Location: Joist Description: Mark: aLJILOING SYSTEMS TIGARD,OR Long Span 24LH344/230 J32 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-3 1/4 BPL Length 2-7 1/4 Clear Bearing 0-9 1/2 Clear Bearing 0-9 1/2 BPL Material: 2024=2 x 2 x.248 BPL Material: 2024=2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def U80 0.00 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L/120 0.00 Section Modulus 3.9167 Section Modulus 3.9167 Reqd SM 0.5523 Reqd SM 0.0000 Mom of Inertia 6.9287 Mom of Inertia 6.9287 Reqd MI 0.5845 Reqd MI 0.0000 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 �' Job Number Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:10:02 AM NEW Nil LL EN N I U N1 Location: Joist Description: Mark: 9u,Lo,NG SYSTEMS TIGARD,OR Long Span 24LH344/230 J33 Geometry i Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-8 32-4 24.00 22.69 7 @ 4-0 Parallel Chords Variable Left End Right End l BC Panel 3-4 3-4 „. „ ,,,,,,,,,fl m�mrtrr�ntiiflIDl ll „ TC Panel 2-2 2-0 ;'\, ��'�, i V I / A , i First Half 1-0 1-0 \ � \ . ' I / ���\�i� /i First Diag. 4-4 4-4 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 114.00 114.00 TC + 0-0 32-8 L-BL Uniform(plf) LL(1) 230.00 230.00 TC + 0-0 32-8 L-BL Uniform(plf) DL(1) 76.00 76.00 BC + 0-0 32-8 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) IP(1) 54.00 54.00 TC + 0-0 32-8 L-BL Uniform(plf) DL(1) 17.00 17.00 TC + 0-0 32-8 L-BL Uniform(plf) SM(1) 19.00 19.00 TC + 0-0 32-8 L-BL Uniform(plf) LL(1) 85.00 85.00 TC + 0-0 32-8 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Additional Shear(Ibs) LL(1) 600.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) SM (1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Uniform (plf) LL(1) 0.00 466.00 TC + 21-9 7/8 33-3 7/8 L-OAL Conc Load (Ibs) CL(1) 2,000.00 0.00 TC + 33-10 33-10 L-OAL Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-8 L-BL Axial(Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Stress Analysis Summary int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 8,849.27 12,463.77 3,115.94 41,168.31 40,996.71 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,744.78 15,311.80 0.00 0.00 23,621.17 2,315.66 44.26 0-2 V1S 1,353.76 14,787.65 0.00 0.00 1,217.04 1,866.85 26.66 2-2 W3 1,353.76 14,787.65 18,402.86 4,371.80 839.71 10,287.36 25.67 3-4 W4 1,951.66 24,734.72 18,402.86 4,371.80 10,629.09 985.88 33.03 4-4 W5 1,951.66 24,734.72 29,922.61 5,429.57 910.68 8,548.86 33.03 6-4 W6 2,863.26 34,247.88 29,922.61 5,429.57 7,250.43 910.68 33.03 8-4 W7 2,863.26 34,247.88 37,501.35 6,233.48 910.68 5,509.49 33.03 10-4 W8 3,540.23 39,881.58 37,501.35 6,233.48 4,535.68 910.68 33.03 12-4 W9 3,540.23 39,881.58 40,996.71 6,783.52 4,535.68 4,535.68 33.03 14-4 W9 3,540.23 41,168.31 40,996.71 6,783.52 4,535.68 4,535.68 33.03 16-4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 # Job Number: Job Name. Date Run' 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:10:02 AM NEW MILLENNIUM Location: Joist Description: Mark: SUILOING SYSTEMS TIGARD,OR Long Span 24LH344/230 J33 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W8 3,540.23 41,168.31 40,054.83 6,233.48 4,535.68 910.68 33.03 18-4 W7 2,863.26 37,837.96 40,054.83 6,233.48 910.68 5,509.49 33.03 20-4 W6 2,863.26 37,837.96 34,036.25 5,429.57 7,250.43 910.68 33.03 22-4 W5 _ 1,932.42 28,811.41 34,036.25 5,429.57 910.68 8,548.86 33.03 24-4 W4 1,932.42 28,811.41 21,981.94 4,371.80 ' 10,629.09 985.88 33.03 26-4 W3 1,057.11 17,918.67 21,981.94 4,371.80 839.71 10,287.36 25.67 28-4 V1S 1,057.11 17,918.67 0.00 0.00 734.18 4,381.14 27.76 30-8 W2 1,101.18 19,817.36 0.00 0.00 23,621.17 2,315.66 44.26 29-4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 470.21 2,240.60 22.69 STRESS ANALYSIS - PAGE 2 ' Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:10:02 AM NEW MILLENNIUM Location: Joist Description: Mark: SUILMING SYSTEMS TIGARD,OR Long Span 24LH344/230 J33 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.8084 0.6885 0.4106 1.3990 0.6554 0.3832 1.0000 A38B=2.2190 x 0.199 BC 0.8084 0.6885 0.4106 1.3990 0.6554 0.3832 1.0000 A38B=2.2190 x 0.199 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 417.70 461.65 692.47 18-8 3/4 23-6 j Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 24.00 28.00 22.00 1.1250 Bending Load 446.00 446.00 483.78 867.92 446.00 Min 0.5000d Len 2X: Axial Load 15,311.80 14,787.65 41,168.31 17,918.67 19,817.36 Max Load Fillers TC: fa 4,402.73 9,146.24 25,462.83 11,082.80 5,698.25 44,479.20 Maximum K L/r 58.45 63.32 43.84 68.19 53.58 Max Load no Fillers TC: Fcr 38,947.56 37,294.54 43,445.47 35,587.98 40,532.97 41,142.93 Fa 23,368.54 22,376.72 26,067.28 21,352.79 24,319.78 Tco3LiRyy: 277.33 Fe 835,977.38 200,705.34 418,755.59 173,057.16 994,882.19 BC oAURyy: Cm 0.9974 0.9772 0.9593 0.9680 0.9971 277.33 Panel Point Moment 16,569.29 2,202.36 1,935.14 4,792.01 4,792.00 BC Stress: Mid Panel Moment 12,523.48 1,432.20 967.57 2,657.76 2,744.11 0.85 Panel Point fb 4,640.60 4,493.24 3,948.04 9,776.59 1,342.11 BCUR0: 116.9021 Mid Panel fb 3,507.48 1,224.77 827.43 2,272.83 768.55 TC Shear Stress: Fillers 0 0 0 0 0 18,890.53 Panel Point Stress 9,043.33 13,639.48 29,410.87 20,859.39 7,040.35 BC Shear Stress: Mid Panel Stress 0.2118 0.4471 1.0030 0.5920 0.2572 18,890.53 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 23,621.17 24,373.24 2,315.66 10,037.09 7.99 x 0.199 1 C38BA= 1.125 x 1.845 x.199 W3 839.71 18,714.09 10,287.36 11,266.83 3.94 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 10,629.09 14,381.54 985.88 7,439.13 4.77 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 910.68 18,714.09 8,548.86 9,567.83 3.27 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 7,250.43 7,826.93 910.68 3,846.19 4.79 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W7 910.68 10,742.43 5,509.49 5,717.01 2.88 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W8 4,535.68 4,802.89 910.68 1,927.10 3.97 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W9 4,535.68 8,984.69 4,535.68 4,657.35 2.59 x 0.118 1 C18BB = 1.125 x 1.035 x.118 W9 4,535.68 8,984.69 4,535.68 4,657.35 2.59 x 0.118 1 C18BB = 1.125 x 1.035 x.118 W8 4,535.68 4,802.89 910.68 1,927.10 3.97 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W7 910.68 10,742.43 5,509.49 5,717.01 2.88 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W6 7,250.43 7,826.93 910.68 3,846.19 4.79 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W5 910.68 18,714.09 8,548.86 9,567.83 3.27 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 10,629.09 14,381.54 985.88 7,439.13 4.77 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W3 839.71 18,714.09 10,287.36 11,266.83 3.94 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W2 23,621.17 24,373.24 2,315.66 10,037.09 7.99 x 0.199 1 C38BA= 1.125 x 1.845 x.199 V1 1,217.04 8,984.69 4,381.14 5,253.48 2.50 x 0.118 1 C18BB = 1.125 x 1.035 x.118 V2 470.21 4,802.89 2,240.60 3,010.07 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:10:02 AM NEW MILLENNIUM Location: Joist Description: Mark: aL111_171,tiG SYSTEMS TIGARD,OR Long Span 24LH344/230 J33 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-5 BPL Length 2-7 3/4 Clear Bearing 0-9 3/4 Clear Bearing 0-9 3/4 BPL Material:2024=2 x 2 x .248 BPL Material:2024=2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def U80 0.00 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L1120 0.00 Section Modulus 3.1434 Section Modulus 3.1434 Reqd SM 0.5523 Reqd SM 0.0000 Mom of Inertia 5.8509 Mom of Inertia 5.8509 Reqd MI 0.5845 Reqd MI 0.0000 Seat Type.Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS -PAGE 1 �, Job Number: Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:10:50 AM NEW MI L L E N N I URA Location: Joist Description: Mark: A,„1_o,tiG SYSTEMS TIGARD,OR Long Span 24LH344/230 J35 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-8 32-4 24.00 22.69 7 @ 4-0 Parallel Chords Variable Left End Right End ,a),>mmm❑mnmitil niaiIIIliitl) First Half 1-0 1-0 �J //\\ �\` / \ /\ / / BC Panel 3-4 TC Panel 2-2 2-0 /`, First Diag. 4-4 4-4 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) LL(1) 230.00 230.00 TC + 0-0 32-8 L-BL Uniform (plf) DL(1) 114.00 114.00 TC + 0-0 32-8 L-BL Uniform (plf) LL(1) 85.00 85.00 TC + 0-0 32-8 L-BL Uniform (plf) IP(1) 54.00 54.00 TC + 0-0 32-8 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 18.00 18.00 TC + 0-0 32-8 L-BL Axial(Ibs) SM (1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) SM(1) 19.00 19.00 TC + 0-0 32-8 L-BL Additional Shear(Ibs) LL(1) 600.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform(plf) DL(1) 76.00 76.00 BC + 0-0 32-8 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Uniform (plf) LL(1) 0.00 466.00 TC + 21-9 7/8 33-3 7/8 L-OAL Conc Load (Ibs) CL(1) 2,000.00 0.00 TC + 33-10 33-10 L-OAL Axial(Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-8 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 8,865.43 12,479.94 3,119.98 41,236.36 41,065.82 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,744.78 15,337.21 0.00 0.00 23,650.92 2,315.66 44.26 0-2 VIS 1,353.76 14,811.76 0.00 0.00 1,214.71 1,869.43 26.66 2-2 W3 1,353.76 14,811.76 18,433.89 4,371.80 839.71 10,302.25 25.67 3-4 W4 1,951.66 24,777.39 18,433.89 4,371.80 10,645.10 985.88 33.03 4-4 W5 1,951.66 24,777.39 29,974.79 5,429.57 910.68 8,561.96 33.03 6-4 W6 2,863.26 34,307.47 29,974.79 5,429.57 7,260.62 910.68 33.03 8-4 W7 2,863.26 34,307.47 37,566.23 6,233.48 910.68 5,516.77 33.03 10-4 W8 3,540.23 39,949.63 37,566.23 6,233.48 4,541.57 910.68 33.03 12-4 W9 3,540.23 39,949.63 41,065.82 6,783.52 4,541.57 4,541.57 33.03 14-4 W9 3,540.23 41,236.36 41,065.82 6,783.52 4,541.57 4,541.57 33.03 16-4 Continued on Next Page... STRESS ANALYSIS -PAGE 1 -0Job Number. Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:10:50 AM NEW MILLENNIUM Location: Joist Description: Mark: euiLoiNo SYSTEMS TIGARD,OR Long Span 24LH344/230 J35 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W8 3,540.23 41,236.36 40,119.71 6,233.48 4,541.57 910.68 33.03 18-4 W7 2,863.26 37,897.55 40,119.71 6,233.48 910.68 5,516.77 33.03 20-4 W6 2,863.26 37,897.55 34,088.44 5,429.57 7,260.62 910.68 33.03 22-4 W5 1,932.42 28,854.08 34,088.44 5,429.57 910.68 8,561.96 33.03 24-4 W4 1,932.42 28,854.08 22,012.98 4,371.80 10,645.10 985.88 33.03 26-4 W3 1,057.11 17,942.74 22,012.98 4,371.80 839.71 10,302.25 25.67 28-4 V1S 1,057.11 17,942.74 0.00 0.00 734.18 4,383.81 27.76 30-8 W2 1,101.18 19,842.90 0.00 0.00 23,650.92 2,315.66 44.26 29-4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 470.21 2,242.81 22.69 STRESS ANALYSIS - PAGE 2 �/� Job Number: Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:10:50 AM NEW MILLENNIUM Location: Joist Description: Mark: PIM O1NG SYSTEMS TIGARD,OR Long Span 24LH344/230 J35 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.8084 0.6885 0.4106 1.3990 0.6554 0.3832 1.0000 A38B=2.2190 x 0.199 BC 0.8084 0.6885 0.4106 1.3990 0.6554 0.3832 1.0000 A38B=2.2190 x 0.199 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 417.70 461.65 692.47 18-8 3/4 23-6 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 24.00 28.00 22.00 1.1250 Min Weld Len 2X: Bending Load 447.00 447.00 484.78 868.92 447.00 0.5000 Axial Load 15,337.21 14,811.76 41,236.36 17,942.74 19,842.90 Max Load Fillers TC: fa 4,410.03 9,161.16 25,504.92 11,097.69 5,705.59 44,476.48 Maximum K L/r 58.45 63.32 43.84 68.19 53.58 Max Load no Fillers TC: Fcr 38,947.56 37,294.54 43,445.47 35,587.98 40,532.97 41,140.43 TC Fa 23,368.54 22,376.72 26,067.28 21,352.79 24,319.78 277.3377.33 yy: Fe 835,977.38 200,705.34 418,755.59 173,057.16 994,882.19 BC oAURyy. Cm 0.9974 0.9772 0.9592 0.9679 0.9971 277.33 Panel Point Moment 16,569.29 2,206.66 1,939.14 4,797.73 4,797.72 BC Stress: Mid Panel Moment 12,520.98 1,434.58 969.57 2,660.69 2,746.07 0.85 Panel Point fb 4,640.60 4,502.01 3,956.20 9,788.26 1,343.71 1 URz: 16.9021 Mid Panel fb 3,506.78 1,226.81 829.14 2,275.34 769.10 TC Shear Stress: Fillers 0 0 0 0 0 18,914.32 Panel Point Stress 9,050.63 13,663.17 29,461.12 20,885.95 7,049.30 BC Shear Stress: Mid Panel Stress 0.2120 0.4479 1.0047 0.5928 0.2575 18,914.32 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 23,650.92 24,373.24 2,315.66 10,037.09 8.00 x 0.199 1 C38BA= 1.125 x 1.845 x.199 W3 839.71 18,714.09 10,302.25 11,266.83 3.94 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 10,645.10 14,381.54 985.88 7,439.13 4.78 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 910.68 18,714.09 8,561.96 9,567.83 3.28 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 7,260.62 7,826.93 910.68 3,846.19 4.79 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 910.68 10,742.43 5,516.77 5,717.01 2.88 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 4,541.57 4,802.89 910.68 1,927.10 3.97 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 4,541.57 8,984.69 4,541.57 4,657.35 2.59 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W9 4,541.57 8,984.69 4,541.57 4,657.35 2.59 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 4,541.57 4,802.89 910.68 1,927.10 3.97 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W7 910.68 10,742.43 5,516.77 5,717.01 2.88 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W6 7,260.62 7,826.93 910.68 3,846.19 4.79 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 910.68 18,714.09 8,561.96 9,567.83 3.28 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 10,645.10 14,381.54 985.88 7,439.13 4.78 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 839.71 18,714.09 10,302.25 11,266.83 3.94 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W2 23,650.92 24,373.24 2,315.66 10,037.09 8.00 x 0.199 1 C38BA= 1.125 x 1.845 x.199 V1 1,214.71 8,984.69 4,383.81 5,253.48 2.50 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V2 470.21 4,802.89 2,242.81 3,010.07 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS - PAGE 3 l/ Job Number: Job Name Date Run: 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:10:50 AM NEW MILLENNIUM Location: Joist Description: Mark: BU1LO1NG SV5TEM5 TIGARD, OR Long Span 24LH344/230 J35 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-5 1/4 BPL Length 2-9 1/4 Clear Bearing 0-9 3/4 Clear Bearing 0-9 3/4 BPL Material: 2024=2 x 2 x.248 BPL Material: 2024=2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def U80 0.00 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L/120 0.00 Section Modulus 3.1434 Section Modulus 3.1434 Reqd SM 0.5523 Reqd SM 0.0000 Mom of Inertia 5.8509 Mom of Inertia 5.8509 Reqd MI 0.5845 Reqd MI 0.0000 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) —�— Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: /� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:02:00 PM NEW MILLENNIUM1Location: Joist Description: Mark: a"'LO'^'° SYSTEMS TIGARD,OR Long Span 24LH344/230 J36 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-8 32-4 24.00 22.41 7 Special Parallel Chords Variable Left End Right End BC Panel 3-4 3-4 MITI O(iT1IIU4R 1 rarrrnin Iklll TC t Half 2-0 2-2 \� ._..,......_._i` _,. -. ,,,� sam,nm ,. _..» ...� First Half 1-0 1-0 �\, m - First Diag. 4-4 4-4 l Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) DL(1) 114.00 114.00 TC + 0-0 32-8 L-BL Uniform(plf) LL(1) 230.00 230.00 TC + 0-0 32-8 L-BL Uniform(plf) DL(1) 23.00 23.00 TC + 0-0 32-8 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Uniform(plf) LL(1) 85.00 85.00 TC + 0-0 32-8 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Additional Shear(Ibs) LL(1) 600.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp (Ibs) WL(1) 400.00 0.00 TC + Uniform(plf) SM(1) 19.00 19.00 TC + 0-0 32-8 L-BL Uniform(plf) DL(1) 76.00 76.00 BC + 0-0 32-8 L-BL Axial(Ibs) SM(1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Uniform(plf) IP(1) 54.00 54.00 TC + 0-0 32-8 L-BL Conc Load (Ibs) LL(1) 4,000.00 0.00 TC + 18-3 1/2 19-4 1/2 L-OAL Uniform(plf) LL(1) 0.00 466.00 TC + 21-9 7/8 33-3 7/8 L-OAL Conc Load(Ibs) CL(1) 2,000.00 0.00 TC + 33-10 33-10 L-OAL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Axial(Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-8 L-BL Conc Load(Ibs) LL(2) 4,000.00 0.00 TC - 18-3 1/2 19-4 1/2 L-OAL Stress Analysis Summary int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 33.50 57.50 10,986.86 15,071.38 3,767.84 57,063.94 58,098.55 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 4,490.00 18,115.09 0.00 0.00 27,765.01 5,418.25 44.11 0-2 V1S 4,058.66 17,576.55 0.00 0.00 3,280.08 6,869.21 26.42 2-2 W3 4,058.66 17,576.55 22,064.43 7,186.31 2,403.85 12,345.57 25.42 3-4 W4 7,203.20 31,069.88 22,064.43 7,186.31 13,559.15 3,057.72 32.83 4-4 V2 7,203.20 31,069.88 22,064.43 7,186.31 2,086.73 3,713.06 22.41 6-4 W5 7,203.20 31,069.88 38,822.21 11,124.97 3,057.72 11,674.92 32.83 6-4 W6 11,395.90 45,606.32 38,822.21 11,124.97 10,350.27 3,057.72 32.83 8-4 V3 11,395.90 45,606.32 38,822.21 11,124.97 2,086.73 3,764.32 22.41 10-4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Numbers Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:02:00 PM NEW MILLENNIUM Location: Joist Description: Mark: aLELMING SYSTEMS TIGARD,OR Long Span 24LH344/230 J36 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W7 11,395.90 45,606.32 51,064.371 14,870.85 3,057.72 8,536.09 32.83 10-4 W8 16,418.42 57,063.94 51,064.37 14,870.85 8,530.00 3,753.24 40.30 12-4 V4 16,418.42 57,063.94 51,064.37 14,870.85 2,086.73 3,993.70 22.41 15-11/2 W9 16,418.42 57,063.94 58,098.55 17,629.16 2,413.50 5,645.14 33.57 15-11/2 _ W9 15,497.13 56,822.69 58,098.55 17,629.16 2,904.35 4,398.81 26.16 17-21/2 V5 15,497.13 56,822.69 58,098.55 17,629.16 1,437.30 2,038.92 22.41 18-4 W8 15,497.13 56,822.69 53,487.07 14,715.34 5,521.07 3,047.85 32.83 18-4 W7 11,121.47 49,042.30 53,487.07 14,715.34 3,057.72 8,536.09 32.83 20-4 V6 11,121.47 49,042.30 53,487.07 14,715.34 1,437.30 2,038.46 22.41 22-4 W6 11,121.47 49,042.30 43,021.85 10,813.95 10,350.27 3,057.72 32.83 22-4 W5 6,745.81 35,610.41 43,021.85 10,813.95 3,057.72 11,674.92 32.83 24-4 V7 6,745.81 35,610.41 43,021.85 10,813.95 1,437.30 2,208.36 22.41 26-4 W4 6,745.81 35,610.41 26,382.14 6,719.77 13,559.15 3,057.72 32.83 26-4 W3 3,464.07 20,895.21 26,382.14 6,719.77 2,403.85 12,345.57 25.42 28-4 V1S 3,464.07 20,895.21 0.00 0.00 3,280.08 6,869.21 26.42 30-6 W2 3,464.07 22,835.71 0.00 0.00 27,765.01 5,418.25 44.11 29-4 1 STRESS ANALYSIS - PAGE 2 G,.1 Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:02:00 PM NEW MILLENNIUM Location: Joist Description: Mark: aUILoING S,.SrFMz TIGARD,OR Long Span 24LH344/230 J36 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.1875 0.8021 0.4813 1.5548 0.7695 0.7639 1.0000 A46A=2.5938 x.250 BC 1.1207 0.8991 0.5436 1.6512 0.8225 0.9058 0.9280 A44A=2.8750 x.209 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 582.35 643.62 965.44 20-9 3/4 20-3 1/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 33.50 26.00 24.00 1.1250 Min Weld Len 2X: Bending Load 452.00 452.00 452.00 816.58 885.11 0.6149 Axial Load 18,115.09 17,576.55 57,063.94 20,895.21 22,835.71 Max Load Fillers TC: fa 4,276.46 7,400.65 24,026.92 8,797.98 5,390.87 63,483.07 Maximum K L/r 49.86 54.02 34.80 54.02 49.86 Max Load no Fillers TC: Fcr 41,688.11 40,392.83 45,762.59 40,392.83 41,688.11 56,842.68 Fa 25,012.87 24,235.70 27,457.56 24,235.70 25,012.87 TC OAL/Ryy: 249.54 F'e 820,501.69 272,400.63 291,704.19 272,400.63 820,501.69 BCOAL/Ryy: Cm 0.9974 0.9864 0.9448 0.9839 0.9967 234.98 Panel Point Moment 16,569.30 2,372.78 3,522.62 4,275.07 4,275.07 BC Stress: Mid Panel Moment 12,422.15 1,633.25 1,761.31 1,928.74 3,295.51 0.86 Panel Point fb 4,241.62 2,833.26 4,206.25 5,104.73 1,094.39 BCLRz: 105.7763 Mid Panel fb 3,179.98 822.61 887.11 971.44 805.41 TC Shear Stress: Fillers 0 0 1 0 0 14,770.52 Panel Point Stress 8,518.08 10,233.91 28,233.17 13,902.71 6,485.25 BC Shear Stress: Mid Panel Stress 0.1921 0.3305 0.9039 0.3930 0.2396 15,296.50 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 27,765.01 28,624.38 5,418.25 11,593.71 8.58 x 0.218 1 C4OBA= 1.125 x 2.014 x.218 V1S 3,280.08 14,381.54 6,869.21 8,601.47 3.08 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W3 2,403.85 24,373.24 12,345.57 14,262.81 4.43 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 13,559.15 14,381.54 3,057.72 7,472.41 6.09 x 0.150 1 C28BB = 1.125 x 1.344 x.150 V2 2,086.73 5,758.64 3,713.06 3,736.86 2.78 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 3,057.72 24,373.24 11,674.92 12,009.39 4.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 10,350.27 10,742.43 3,057.72 5,742.06 5.40 x 0.129 1 C22BB= 1.125 x 1.110 x.129 V3 2,086.73 7,826.93 3,764.32 4,944.53 2.49 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 3,057.72 18,714.09 8,536.09 9,611.43 3.27 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 8,530.00 8,984.69 3,753.24 3,857.23 4.87 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V4 2,086.73 7,826.93 3,993.70 4,944.53 2.64 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 2,413.50 10,742.43 5,645.14 5,646.10 2.95 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W9 2,904.35 7,826.93 4,398.81 4,534.90 2.90 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V5 1,437.30 4,802.89 2,038.92 3,029.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W8 5,521.07 7,826.93 3,047.85 3,864.69 3.65 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W7 3,057.72 18,714.09 8,536.09 9,611.43 3.27 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V6 1,437.30 4,802.89 2,038.46 3,029.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W6 10,350.27 10,742.43 3,057.72 5,742.06 5.40 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 3,057.72 24,373.24 11,674.92 12,009.39 4.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 Continued on Next Page... STRESS ANALYSIS -PAGE 2 ' Job Number: Job Name: Date Run: �J 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:02:00 PM 1 NEW MILLENNIUM Location: Joist Description: Mark: aLELoItiC SYSTEMS TIGARD,OR Long Span 24LH344/230 J36 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 1,437.30 4,802.89 2,208.36 3,029.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W4 13,559.15_ 14,381.54 3,057.72 7,472.41 6.09 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W3 2,403.85 24,373.24 12,345.57 14,262.81 4.43 x 0.188 1 C38BA= 1.125 x 1.845 x .199 V1 S 3,280.08 14,381.54 6,869.21 8,601.47 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W2 27,765.01 28,624.38 5,418.25 11,593.71 8.58 x 0.218 1 C40BA= 1.125 x 2.014 x .218 STRESS ANALYSIS - PAGE 3 G� Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:02:00 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD, OR Long Span 24LH344/230 J36 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-3 1/8 BPL Length 2-7 1/8 Clear Bearing 0-9 3/8 Clear Bearing 0-9 1/2 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L1120 0.27 Reqd TL Def L/80 0.00 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L/120 0.00 Section Modulus 3.9064 Section Modulus 3.9064 Reqd SM 0.5523 Reqd SM 0.0000 Mom of Inertia 6.9946 Mom of Inertia 6.9946 Reqd MI 0.5845 Reqd MI 0.0000 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case Sd: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case Be: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS -PAGE 1 0 Job Number. Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:08:48 AM NEW M I L L E N NI U M Location: Joist Description: Mark: aLIII_oItiG SYSTEMS TIGARD,OR Long Span 24LH344/230 J38 Geomet Base Length: Working Length: Joist Depth: Effective Depth: SC Panel Length: Shape: 32-5 7/8 32-1 7/8 24.00 22.69 7 @ 4-0 Parallel Chords Variable Left End _ Right End BC Panel 3-4 3-1 7/8 ,.rnmmi u-iliamllflI:I U9 TC Panel 2-2 2-0 1 First Half 1 0 1-0 z, ,.�,,,., a .,...... �s � < ,..rfr,1_�r� . ., First Diag. 4-4 4-1 7/8 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 230.00 230.00 TC + 0-0 32-5 7/8 L-BL Uniform (plf) DL(1) 114.00 114.00 TC + 0-0 32-5 7/8 L-BL Uniform(plf) LL(1) 85.00 85.00 TC + 0-0 32-5 7/8 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM (1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 76.00 76.00 BC + 0-0 32-5 7/8 L-BL Uniform(plf) IP(1) 54.00 54.00 TC + 0-0 32-5 7/8 L-BL Uniform(plf) SM (1) 19.00 19.00 TC + 0-0 32-5 7/8 L-BL Additional Shear(Ibs) LL(1) 600.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 17.00 17.00 TC + 0-0 32-5 7/8 L-BL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Uniform(plf) LL(1) 0.00 466.00 TC + 21-9 7/8 33-3 7/8 L-DAL Conc w/bending(Ibs) CL(1) 2,000.00 0.00 TC + 33-10 33-10 L-OAL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-5 7/8 L-BL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Stress Analysis Summary int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Camp.: Max BC Tension 24.00 48.00 8,738.16 12,881.67 3,220.42 40,102.03 40,047.82 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,741.63 15,154.84 0.00 0.00 17,262.30 2,311.91 44.26,0-2 V1S 1,350.61 14,630.69 0.00 0.00 1,216.81 4,254.69 26.66 2-2 W3 1,350.61 14,630.69 18,196.33 4,365.94 842.78 10,015.62 25.67 3-4 W4 1,945.51 24,429.06 18,196.33 4,365.94 10,526.92 993.70 33.03 4-4 W5 1,945.51 24,429.06 29,517.81 5,418.10 910.57 8,387.13 33.03 6-4 W6 2,848.97 33,743.95 29,517.81 5,418.10 7,088.71 910.57 33.03 8-4 W7 2,848.97 33,743.95 36,787.23 6,216.38 910.57 5,347.76 33.03 10-4 W8 3,520.33 39,050.07 36,787.23 6,216.38 4,687.76 910.57 33.03 12-4 W9 3,520.33 39,050.07 40,047.82 6,742.07 4,687.76 4,687.76 33.03 14-4 W9 3,495.98 40,102.03 40,047.82 6,742.07 4,687.76 4,687.76 33.03 16-4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:08:48 AM NEW MILLENNIUM Location: Joist Description: Mark: 13E111_OING SYSTEMS TIGARD,OR Long Span 24LH3441230 J38 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W8 3,495.98 40,102.03 38,873.54 6,186.41 4,687.76 910.57 33.03 18-4 W7 2,813.38 36,560.56 38,873.54 6,186.41 910.57 5,347.76 33.03 20-4 W6 2,813.38 36,560.56 32,700.62 5,376.89 7,088.71 910.57 33.03 22-4 W5 1,876.93 27,474.32 32,700.62 5,376.89 910.57 8,387.13 33.03 24-4 W4 1,876.93 27,474.32 20,864.55 4,313.50 10,526.92 993.70 33.03 26-4 W3 998.81 16,894.45 20,864.55 4,313.50 842.78 10,015.62 25.67 28-4 V1S 998.81 16,894.45 0.00 0.00 1,216.81 4,254.69 26.60 30-5 7/8 W2 1,035.41 18,531.21 0.00 0.00 22,302.31 1,593.43 42.45 29-4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 470.11 2,162.34 22.69 STRESS ANALYSIS - PAGE 2 ' Job Number. Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:08:48 AM NEW MILLENNIUM Location: Joist Description: Mark: BLJILOING SVSTFMS TIGARD,OR Long Span 24LH3441230 J38 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.8084 0.6885 0.4106 1.3990 0.6554 0.3832 1.0000 A38B=2.2190 x 0.199 BC 0.8084 0.6885 0.4106 1.3990 0.6554 0.3832 1.0000 A38B=2.2190 x 0.199 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 417.70 469.32 703.97 18-8 7/8 23-6 7/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE cap Between Chords: Length 24.00 26.00 24.00 25.88 22.00 1.1250 Min Weld Len 2X: Bending Load 446.00 446.00 479.31 815.02 881.47 0.5000 1 Axial Load 15,154.84 14,630.69 40,102.03 16,894.45 18,531.21 Max Load Fillers TC: fa 4,357.59 9,049.16 24,803.33 10,449.31 5,328.43 44,491.36 Maximum K L/r 58.45 63.32 43.84 63.02 53.58 Max Load no Fillers TC: Fcr 38,947.56 37,294.54 43,445.47 37,399.56 40,532.97 41,154.13 Fa 23,368.54 22,376.72 26,067.28 22,439.73 24,319.78 275..8181 TC Ryy: F'e 835,977.38 200,705.34 418,755.59 202,649.20 994,882.19 BC oAURyy: Cm 0.9974 0.9775 0.9603 0.9742 0.9973 275.81 Panel Point Moment 16,569.29 2,202.36 1,917.24 4,982.16 4,982.16 BC Stress: Mid Panel Moment 12,523.48 1,432.20 958.62 1,628.18 10,007.96 0.83 BC Panel Point fb 4,640.60 4,493.24 3,911.53 10,164.55 1,395.37 116.90 16.9021 Mid Panel fb 3,507.48 1,224.77 819.78 1,392.36 3,183.78 TC Shear Stress: Fillers 0 0 0 0 0 18,484.78 Panel Point Stress 8,998.20 13,542.40 28,714.87 20,613.86 6,723.79 BC Shear Stress: Mid Panel Stress 0.2109 0.4428 0.9774 0.5096 0.3140 18,484.78 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 17,262.30 18,714.09 2,311.91 8,090.53 6.61 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W3 842.78 18,714.09 10,015.62 11,266.83 3.83 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 10,526.92 14,381.54 993.70 7,439.13 4.73 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W5 910.57 18,714.09 8,387.13 9,567.83 3.21 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 7,088.71 7,826.93 910.57 3,846.19 4.68 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 910.57 10,742.43 5,347.76 5,717.01 2.79 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 4,687.76 4,802.89 910.57 1,927.10 4.10 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 4,687.76 10,742.43 4,687.76 5,717.01 2.45 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W9 4,687.76 10,742.43 4,687.76 5,717.01 2.45 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W8 4,687.76 4,802.89 910.57 1,927.10 4.10 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W7 910.57 10,742.43 5,347.76 5,717.01 2.79 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W6 7,088.71 7,826.93 910.57 3,846.19 4.68 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 910.57 18,714.09 8,387.13 9,567.83 3.21 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 10,526.92 10,742.43 993.70 5,717.01 5.50 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 842.78 18,714.09 10,015.62 11,266.83 3.83 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W2 22,302.31 24,373.24 1,593.43 10,478.39 8.01 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1 1,216.81 7,826.93 4,254.69 4,482.37 2.81 x 0.102 1 C16BB = 1.125 x 1.025 x.102 V2 470.11 4,802.89 2,162.34 3,010.07 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS - PAGE 3 0 Job Number: 5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:08:48 AM NEW MILLENNIUM Location: Joist Description: Mark: erLLMING SYSTEMS TIGARD,OR Long Span 24LH344/230 J38 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-1 1/8 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-5 1/4 BPL Length 2-8 1/4 Clear Bearing 0-10 1/8 Clear Bearing 0-9 3/8 BPL Material:2024 =2 x 2 x.248 BPL Material:2024 =2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def L/80 0.01 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L/120 0.01 Section Modulus 3.1434 Section Modulus 3.1434 Reqd SM 0.5523 Reqd SM 0.0047 Mom of Inertia 5.8509 Mom of Inertia 5.8509 Reqd MI 0.5845 Reqd MI 0.0003 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c:DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 �/� Job Number: Job Name- Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:15:03 AM NEW MILLENNIUM Location: Joist Description: Mark: Rl,^ ninir GYTe^^s TIGARD,OR Long Span 24LH344/230 J40 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-8 32-4 24.00 22.54 7©4-0 Parallel Chords Variable Left End Right End BC Panel 3-4 3-4 _.._._... _........ . ......."--'._,_.-, .....,_,;._ u...,.1...I;.' L 11.. ..,.._. TC Panel 2-2 2-0 First Half 1-0 1-0 First Diag. 4-4 4-4 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) LL(1) 230.00 230.00 TC + 0-0 32-8 L-BL Uniform(plf) DL(1) 114.00 114.00 TC + 0-0 32-8 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform(plf) IP(1) 54.00 54.00 TC + 0-0 32-8 L-BL Uniform(plf) LL(1) 85.00 85.00 TC + 0-0 32-8 L-BL Uniform(plf) DL(1) 21.00 21.00 TC + 0-0 32-8 L-BL Axial(Ibs) SM(1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) SM(1) 19.00 19.00 TC + 0-0 32-8 L-BL Additional Shear(Ibs) LL(1) 600.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 76.00 76.00 BC + 0-0 32-8 L-BL Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 18-11 1/2 18-11 1/2 L-OAL Conc©any pp(Ibs) SM (1) 400.00 0.00 TC + Conc @ any pp (Ibs) WL(1) 400.00 0.00 TC + 1 Uniform(plf) LL(1) 0.00 466.00 TC + 21-97/8 33-37/8 L-OAL Conc Load(Ibs) CL(1) 2,000.00 0.00 TC + 33-10 33-10 L-OAL Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-8 L-BL Axial(Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp (Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM(2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 10,417.80 14,024.57 3,506.14 53,004.33 54,429.04 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,756.51 18,037.51 0.00 0.00 26,790.79 2,327.14 44.18 0-2 V1S 1,362.86 17,504.65 0.00 0.00 1,222.76 1,893.66 26.53 2-2 W3 1,362.86 17,504.65 21,972.76 4,381.02 840.95 12,057.17 25.53 3-4 W4 1,964.78 29,995.47 21,972.76 4,381.02 12,916.73 989.39 32.92 4-4 W5 1,964.78 29,995.47 36,858.02 5,445.90 913.92 10,828.71 32.92 6-4 W6 2,882.50 42,843.62 36,858.02 5,445.90 9,513.98 913.92 32.92 8-4 W7 2,882.50 42,843.62 47,756.83 6,255.21 913.92 7,755.16 32.92 10-4 W8 3,564.03 51,767.27 47,756.83 6,255.21 6,440.43 913.92 32.92 12-4 W9 3,564.03 51,767.27 54,429.04 6,808.95 2,717.26 5,121.82 32.92 14-4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 ' ,/ Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:15:03 AM NEW MILLENNIUM Location: Joist Description: Mark: aLJILOING SYSTEMS TIGARD,OR Long Span 24LH344/230 J40 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W9 3,564.03 53,004.33 54,429.04 6,808.95 2,717.26 5,121.82 32.92 16-4 W8 3,564.03 53,004.33 50,277.38 6,255.21 6,440.43 913.92 32.92 18-4 W7 2,882.50 46,431.10 50,277.38 6,255.21 913.92 7,755.16 32.92 20-4 W6 2,882.50 46,431.10 40,980.81 5,445.90_ 9,513.98 913.92 32.92 22-4 W5 1,945.41 34,089.31 40,980.81 5,445.90 913.92 10,828.71 32.92 24-4 W4 1,945.41 34,089.31 25,558.74 4,381.02 12,916.73 989.39 32.92 26-4 W3 1,064.22 20,643.50 25,558.74 4,381.02 840.95 12,057.17 25.53 28-4 V1S 1,064.22 20,643.50 0.00 0.00 735.82 4,414.72 27.64 30-8 W2 1,108.59 22,560.88 0.00 0.00 26,790.79 2,327.14 44.18 29-4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 470.28 2,274.99 22.54 STRESS ANALYSIS - PAGE 2 �) Job Number: Job Name: Date Run: � 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:15:03 AM NEW MILLENNIUM Location: Joist Description: Mark: BLELOING SYSTEMS TIGARD,OR Long Span 24LH344/230 J40 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.0162 0.8183 0.4925 1.5555 0.7604 0.6804 0.9652 A42A=2.6250 x.209 BC 0.9485 0.7361 0.4403 1.4631 0.7019 0.5140 1.0000 A40B=2.3750 x 0.218 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 500.78 553.47 830.21 20-9 7/8 26-6 7/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 24.00 28.00 22.00 1.1250 Min Weld Len 2X: Bending Load 450.00 450.00 487.78 871.92 450.00 0.5711 Axial Load 18,037.51 17,504.65 53,004.33 20,643.50 22,560.88 Max Load Fillers TC: fa 4,632.84 8,612.80 26,079.68 10,157.21 5,794.65 55,618.67 Maximum K L/r 48.73 52.79 24.37 56.85 44.67 Max Load no Fillers TC: Fcr 40,813.40 39,643.03 46,279.65 38,416.70 41,920.64 52,782.36 Fa 24,488.04 23,785.82 27,767.79 23,050.02 25,152.38 TCo4URyy. 249.44 F'e 834,195.50 283,515.06 591,531.44 244,459.42 992,761.56 BCOAL/Ryy: Cm 0.9972 0.9848 0.9705 0.9792 0.9971 1265.19 Panel Point Moment 16,569.30 2,348.44 1,951.14 4,663.38 4,663.38 BC Stress: Mid Panel Moment 12,436.54 1,608.15 975.57 2,723.40 2,625.72 0.96 BC Panel Point fb 4,341.47 3,217.89 2,673.49 6,389.87 1,221 89 109.01 09.0166 Mid Panel fb 3,258.61 898.62 545.14 1,521.81 687.99 TC Shear Stress: Fillers 0 0 2 0 0 16,544.76 Panel Point Stress 8,974.32 11,830.69 28,753.17 16,547.08 7,016.54 BC Shear Stress: Mid Panel Stress 0.2079 0.3907 0.9567 0.4898 0.2516 18,046.71 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 26,790.79 28,624.38 2,327.14 11,574.81 9.62 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W3 840.95 24,373.24 12,057.17 14,226.67 4.33 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 12,916.73 14,381.54 989.39 7,457.08 5.80 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W5 913.92 24,373.24 10,828.71 11,983.32 3.89 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 9,513.98 10,742.43 913.92 5,730.53 4.97 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W7 913.92 16,730.22 7,755.16 8,333.09 3.31 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 6,440.43 7,826.93 913.92 3,856.17 4.25 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W9 2,717.26 10,742.43 5,121.82 5,730.53 2.67 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W9 2,717.26 10,742.43 5,121.82 5,730.53 2.67 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 6,440.43 7,826.93 913.92 3,856.17 4.25 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 913.92 16,730.22 7,755.16 8,333.09 3.31 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W6 9,513.98 10,742.43 913.92 5,730.53 4.97 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 913.92 24,373.24 10,828.71 11,983.32 3.89 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 12,916.73 14,381.54 989.39 7,457.08 5.80 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 840.95 24,373.24 12,057.17 14,226.67 4.33 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 26,790.79 28,624.38 2,327.14 11,574.81 9.62 x 0.188 1 C40BA= 1.125 x 2.014 x.218 V1 1,222.76 8,984.69 4,414.72 5,267.67 2.52 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V2 470.28 4,802.89 2,274.99 3,020.76 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS -PAGE 3 G� Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 11:15:03 AM NEW M I L L E N N I UM Location: Joist Description: Mark. SLELOING SYSTEMS TIGARD,OR Long Span 24LH344/230 J40 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-5 BPL Length 2-7 3/4 Clear Bearing 0-9 5/8 Clear Bearing 0-9 3/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def L/80 0.00 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L/120 0.00 Section Modulus 3.6568 Section Modulus 3.6568 Reqd SM 0.5523 Reqd SM 0.0000 Mom of Inertia 6.5361 Mom of Inertia 6.5361 Reqd MI 0.5845 Reqd MI 0.0000 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a:LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c:DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case Sc: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: r/ 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:04:48 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 24LH344/230 J41 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-7 3/4 32-3 3/4 24.00 22.52 7 Special Parallel Chords Variable Left End Right End BC Panel 3-4 3-3 3/4 11RJITITSIITIJTIITIIII II II III Till,IIII.11 111111r11J 111I,IJlJ1IlJ,I11,41uJITRRIl,Il➢IIITI IUIHp41 1(111,11111.77111Y11#i IIIIIIIilJJJIRRIIIIII,UIlIlU lip41) TC Panel 2-2 2-2 S \ k\ � j WW\ / ��X�`. /fP // First Half 1-0 1-0 \' , ,‘ 11IlifI(111UII[DIIIIIIiINII dfil(�li r IIITIII ,--- First Diag. 4-4 4-3 3/4 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference 1 ' Uniform(plf) LL(1) 230.00 230.00 TC + 0-0 32-7 3/4 L-BL Uniform (plf) DL(1) 114.00 114.00 TC + 0-0 32-7 3/4 L-BL Additional Shear(Ibs) LL(1) 600.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) SM(1) 19.00 19.00 TC + 0-0 32-7 3/4 L-BL Uniform(plf) DL(1) 76.00 76.00 BC + 0-0 32-7 3/4 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM(1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Axial(Ibs) SM(1) 450.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) IP(1) 54.00 54.00 TC + 0-0 32-7 3/4 L-BL Axial(Ibs) WL(1) 450.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 22.00 22.00 TC + 0-0 32-7 3/4 L-BL Conc Load (Ibs) LL(1) 4,000.00 0.00 TC + 18-3 1/2 19-4 1/2 L-OAL Conc @ any pp(Ibs) SM(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 300.00 0.00 TC + Conc @ any pp(Ibs) WL(1) 300.00 0.00 TC + Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Axial(Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-7 3/4 L-BL Conc Load (Ibs) LL(2) 4,000.00 0.00 TC - 18-3 1/2 19-4 1/2 L-OAL Conc @ any pp (Ibs) SM(2) 300.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 300.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 33.50 57.50 9,028.61 8,940.34 2,257.15 46,305.01 46,667.39 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 4,478.22 16,151.82 0.00 0.00 18,083.44 5,830.36 44.17 0-2 V1S 4,084.30 15,699.86 0.00 0.00 3,273.97 4,115.01 26.52 2-2 W3 4,084.30 15,699.86 19,197.69 7,410.83 2,623.37 9,502.19 25.52 3-4 W4 7,263.94 26,431.06 19,197.69 7,410.83 11,140.77 3,315.22 32.91 4-4 V2 7,263.94 26,431.06 19,197.69 7,410.83 2,085.51 3,511.43 22.52 6-4 ' Continued on Next Page... STRESS ANALYSIS -PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:04:48 PM NEW MILLENNIUM Location; Joist Description: Mark: SUILoItiG SYSTEMS TIGARD,OR Long Span 24LH344/230 J41 Stress Analois Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W5 7,263.94 26,431.06 31,962.17 11,569.10 3,154.30 9,682.34 32.91 6-4 W6 11,339.03 37,424.48 31,962.17 11,569.10 8,612.63 3,088.54 32.91 8-4 V3 11,339.03 37,424.48 31,962.17 11,569.10 2,085.51 3,549.06 22.52 10-4 W7 11,339.03 37,424.48 41,511.64 15,535.56 3,047.67 7,054.71 32.91 10-4 W8 16,336.51 46,305.01 41,511.64 15,535.56 7,080.86 3,737.93 40.37 12-4 V4 16,336.51 46,305.01 41,511.64 15,535.56 2,085.51 3,729.46 22.52 15-1 1/2 W9 16,336.51 _ 46,305.01 46,667.39 18,447.38 3,956.19 3,372.27 33.65 15-1 1/2 W9 15,397.96 45,132.52 46,667.39 18,447.38 2,426.28 3,729.88 26.26 17-21/2 V5 15,397.96 45,132.52 46,667.39 18,447.38 1,438.52 2,040.14 22.52 18-4 W8 15,397.96 45,132.52 41,502.53 15,360.85 5,911.11 3,041.16 32.91 18-4 W7 11,074.03 37,377.60 41,502.53 15,360.85 3,047.67 7,054.71 32.91 20-4 V6 11,074.03 37,377.60 41,502.53 15,360.85 1,438.52 2,039.68 22.52 22-4 W6 11,074.03 37,377.60 31,906.18 11,239.25 8,612.63 3,088.54 32.91 22-4 W5 6,856.52 26,365.96 31,906.18 11,239.25 3,154.30 9,682.34 32.91 24-4 V7 6,856.52 26,365.96 31,906.18 11,239.25 1,438.52 2,039.23 22.52 26-4 W4 6,856.52 26,365.96 19,123.49 6,925.84 11,140.77 3,315.22 32.91 26-4 W3 3,560.65 15,623.04 19,123.49 6,925.84 2,623.37 9,502.19 25.52 28-4 V1S 3,560.65 15,623.04 0.00 0.00 2,392.32 4,035.05 26.39 30-5 3/4 W2 3,590.69 16,064.72 0.00 0.00 17,906.23 4,741.96 43.96 29-4 STRESS ANALYSIS - PAGE 2 G' Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:04:48 PM NEW MILLENNIUM Location: Joist Description: Mark: BUIL.OiNG SYSTEMS TIGARD,OR Long Span 24LH344/230 J41 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 1.1207 0.8991 0.5436 1.6512 0.8225 0.9058 0.9280 A44A=2.8750 x.209 BC 0.8084 0.6885 0.4106 1.3990 0.6554 0.3832 1.0000 A38B=2.2190 x 0.199 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 479.02 530.45 795.67 22-11/4 14-3 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 33.50 25.75 24.00 1.1250 Min Weld Len 2X Bending Load 366.00 366.00 366.00 366.00 366.00 0.5000 Axial Load 16,151.82 15,699.86 46,305.01 15,623.04 16,064.72 Max Load Fillers TC: fa 3,937.16 7,004.49 20,658.97 6,970.22 3,915.93 57,369.77 Maximum K Ur 44.15 47.83 46.22 47.37 44.15 Max Load no Fillers TC: Fcr 40,650.88 39,728.11 40,138.28 39,846.30 40,650.88 52,935.76 Fa 24,390.53 23,836.86 24,082.97 23,907.78 24,390.53 TCOAURyy: 234.83 Fe 839,250.44 342,268.59 366,523.31 348,946.84 839,250.44 BC OAURyy: Cm 0.9977 0.9898 0.9622 0.9900 0.9977 277.16 Panel Point Moment 16,569.31 2,069.04 2,852.39 1,834.42 1,834.42 BC Stress: Mid Panel Moment 12,597.59 1,561.88 1,426.19 837.94 1,292.15 0.96 Panel Point fb 4,139.46 2,344.17 3,231.69 2,078.35 458.29 BCUR3: 140.0390 Mid Panel fb 3,147.22 709.12 647.52 380.44 329.90 TC Shear Stress: Fillers 0 0 0 0 0 9,994.07 Panel Point Stress 8,076.62 9,348.66 23,890.65 9,048.57 4,374.22 BC Shear Stress: Mid Panel Stress 0.1944 0.3171 0.8798 0.3040 0.0922 14,394.90 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 18,083.44 18,714.09 5,830.36 8,106.78 6.92 x 0.176 1 C34AA= 1.125 x 1.549 x .176 V1S 3,273.97 7,826.93 4,115.01 4,497.24 2.72 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W3 2,623.37 16,730.22 9,502.19 9,868.44 4.05 x 0.158 1 C32BA= 1.125 x 1.520 x .158 W4 11,140.77 14,381.54 3,315.22 7,458.93 5.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 2,085.51 5,758.64 3,511.43 3,727.80 2.63 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 3,154.30 24,373.24 9,682.34 11,986.46 3.48 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 8,612.63 8,984.69 3,088.54 4,670.17 4.92 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V3 2,085.51 5,758.64 3,549.06 3,727.80 2.66 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 3,047.67 14,381.54 7,054.71 7,458.93 3.17 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 7,080.86 8,984.69 3,737.93 3,850.39 4.04 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V4 2,085.51 7,826.93 3,729.46 4,931.62 2.46 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 3,956.19 7,826.93 3,372.27 3,786.73 2.61 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W9 2,426.28 7,826.93 3,729.88 4,524.60 2.46 x 0.102 1 C16BB = 1.125 x 1.025 x.102 V5 1,438.52 4,802.89 2,040.14 3,021.86 2.00 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W8 5,911.11 7,826.93 3,041.16 3,857.19 3.90 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W7 3,047.67 14,381.54 7,054.71 7,458.93 3.17 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V6 1,438.52 4,802.89 2,039.68 3,021.86 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W6 8,612.63 8,984.69 3,088.54 4,670.17 4.92 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 3,154.30 24,373.24 9,682.34 11,986.46 3.48 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 ' Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:04:48 PM NEW MILLENNIUM Location: Joist Description: Mark: 9LI,L01NG SYSTEMS TIGARD,OR Long Span 24LH344/230 J41 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 1,438.52 4,802.89 2,039.23 3,021.86 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W4 11,140.77 14,381.54 3,315.22 7,458.93 5.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 2,623.37 16,730.22 9,502.19 9,868.44 4.05 x 0.158 1 C32BA= 1.125 x 1.520 x.158 V1S 2,392.32 7,826.93 4,035.05 4,510.99 2.66 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W2 17,906.23 18,714.09 4,741.96 8,147.71 6.85 x 0.176 1 C34AA= 1.125 x 1.549 x.176 , STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:04:48 PM NEW NI I L L E N N I U N1 Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 24LH344/230 J41 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 1/4 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-3 1/8 BPL Length 2-7 3/8 Clear Bearing 0-10 1/8 Clear Bearing 0-10 1/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x .248 Total Load 344.00 Total Load 344.00 Reqd TL Def U120 0.27 Reqd TL Def L/80 0.00 Live Load 230.00 Live Load 230.00 Reqd LL Def U180 0.18 Reqd LL Def L/120 0.00 Section Modulus 3.9167 Section Modulus 3.9167 Reqd SM 0.5523 Reqd SM 0.0024 Mom of Inertia 6.9287 Mom of Inertia 6.9287 Reqd MI 0.5845 Reqd MI 0.0001 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 ' Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:59 PM NEW M I LL EN N I UM Location: Joist Description: Mark: eLJII_o,tiG SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J42 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 81-81/4 81.41/4 68.00 65A5 9 Special Double Pitch with Ridge @ 40-8 Variable Left End Right End BC Panel 5-8 6-0 1/4 «, alut3utRn _ TC Panel 4-0 4-0 , n, i /\ , , , i_.�, ,- First Half 3-0 3-0 }{i[lill D111I} �I11-,]i1ClIIlt T,Iiii ft 11ICTI I ,I[I�YCIII(IIl;1�l 11 l[IIIIIIII�filliillIMILI1fil�iiiMIIIlltl,G�' First Diag. 8-8 9-0 1/4 Depth 47.50 47.50 Loads Load Type Category Load1 Load2 Position Direction Lot/Begin Sp/End Reference '' Uniform (plf) LL(1) 390.00 390.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) DL(1) 192.00 192.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) IP(1) 90.00 90.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) SM(1) 32.00 32.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) DL(1) 61.00 61.00 TC + 0-0 81-8 1/4 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 128.00 128.00 BC + 0-0 81-8 1/4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc w/bending(Ibs) LL(1) 5,000.00 0.00 TC + 18-101/2 18-101/2 L-OAL Concw/bending(Ibs) LL(1) 5,000.00 0.00 TC + 28-0 1/2 28-0 1/2 L-OAL Concw/bending(Ibs) LL(1) 5,000.00 0.00 TC + 37-2 1/2 37-2 1/2 L-OAL Conc Load(Ibs) LL(1) 1,000.00 0.00 BC + 39-3 39-3 L-OAL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM(1) 400.00 0.00 TC + Conc w/bending(Ibs) LL(1) 1,000.00 0.00 BC + 46-4 46-4 L-OAL Gross Uplift(plf) WL(2) 60.00 60.00 TC - 0-0 81-8 1/4 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Stress Analysis Summary int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 60.05 120.00 41,672.02 36,603.06 10,418.00 169,379.95 168,769.55 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,489.86 55,872.63 0.00 0.00 67,580.51 4,571.30 79.90 0-2 V1S 3,383.08 54,728.37 0.00 0.00 719.35 3,368.03 51.05 4-0 W3 3,383.08 54,728.37 80,150.51 4,933.89 2,851.02 43,210.47 61.06 5-8 W4 6,992.58 115,803.52 80,150.51 4,933.89 46,031.32 2,931.53 77.67 8-8 V2 6,992.58 115,803.52 80,150.51 4,933.89 731.92 4,544.02 51.84 13-8 W5 6,992.58 115,803.52 142,307.86 8,517.48 2,276.46 35,913.04 80.96 13-8 W6 9,604.86 158,821.69 142,307.86 8,517.48 22,104.66 1,668.03 80.96 18-8 V3 9,604.86 158,821.69 142,307.86 8,517.48 721.90 4,800.79 56.88 23-8 W7 9,604.86 158,821.69 167,088.98 10,205.87 1,071.52 14,085.14 78.35 23-8 W8 10,564.90 169,379.95 167,088.98 10,205.87 13,578.55 3,589.30 78.35 27-11 1/2 V4 10,564.90 169,379.95 167,088.98 10,205.87 665.37 3,304.13 61.21 32-3 W9 10,564.90 169,379.95 168,769.55 10,660.18 12,161.38 5,501.97 72.32 32-3 Continued on Next Page... STRESS ANALYSIS - PAGE 1 ', Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:59 PM NEW IVI I L L E N N I U M Location: Joist Description: Mark: eLJILoItiG SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J42 Stress Analjsis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W10 10,672.90 165,987.94 168,769.55 10,660.18 679.96 11,609.89 70.64 35-3 V5 10,672.90 165,987.94 168,769.55 10,660.18 608.87 4,417.53 64.08 37-11 1/2 W11 10,672.90 165,987.94 160,435.02 10,586.00 12,156.75 737.10 73.07 37-11 1/2 W11 10,694.83 161,090.81 160,435.02 10,586.00 11,631.19 7,502.40 73.07 40-8 V6 10,694.83 161,090.81 160,435.02 10,586.00 608.91 2,697.43 64.10 43-4 1/2 W10 10,694.84 161,090.83 159,850.77 10,691.74 11,610.05 5,252.54 70.66 43-41/2 W9 10,607.39 157,632.59 159,850.77 10,691.74 5,500.83 12,158.87 72.34 46-1 V7 10,607.39 157,632.59 159,850.77 10,691.74 665.51 3,260.45 61.24 49-1 W8 10,607.39 157,632.59 150,774.70 10,265.54 13,575.34 860.23 78.39 49-1 W7 9,683.35 141,174.02 150,774.70 10,265.54 1,041.72 14,799.53 78.39 53-41/2 V8 9,683.35 141,174.02 150,774.70 10,265.54 722.22 3,803.39 56.95 57-8 W6 9,683.35 141,174.05 124,156.38 8,621.13 22,816.47 1,633.73 81.03 57-8 W5 7,125.66 102,011.54 124,156.38 8,621.13 2,236.77 30,024.88 81.03 62-8 V9 7,125.66 102,011.54 124,156.38 8,621.13 732.51 3,844.71 51.96 67-8 W4 7,125.66 102,011.55 72,145.68 5,102.17 38,590.05 2,887.36 77.76 67-8 W3 3,568.31 50,415.07 72,145.68 5,102.17 2,826.18 36,999.77 61.17 72-8 V1S 3,568.31 50,415.07 0.00 0.00 755.23 3,574.60 52.84 77-81/4 W2 3,702.73 51,855.68 0.00 0.00 61,542.32 4,762.24 83.44 75-8 STRESS ANALYSIS - PAGE 2 G,, Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:59 PM NEW MILLENNIUM Location: Joist Description: Mark: aLJILoING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J42 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 4.1882 1.5476 0.9861 2.5085 1.4117 10.0307 0.9798 5043=5 X 5 X.438 BC 2.8594 1.2346 0.7876 2.1017 1.1383 4.3586 1.0000 4037=4 x 4 x.375 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 14,587.07 1,012.11 1,518.17 35-6 1/2 42-0 3/8 Top Chord Check End Panel LE I First Panel LE Interior Panel First Panel RE ' End Panel RE Gap Between Chords: Length 46.04, 56.05 60.05 60.30 46.04 1.1250 Min Weld Len 2X: Bending Load 642.43' 642.43 642.43 642.44 642.44 1.7113 Axial Load 55,872.63 54,728.37 169,379.95 50,415.07 51,855.69 Max Load Fillers TC: fa 6,670.24 6,533.64 18,960.61 6,018.70 6,190.69 224,236.31 Maximum K Ur 46.69 56.84 39.20 61.15 46.69 Max Load no Fillers TC: Fcr 41,905.18 38,866.49 43,880.47 37,475.16 41,905.38 210,955.14 TC OAURyy: Fa 25,143.11 23,319.89 26,328.28 22,485.10 25,143.22 389.18 Fe 323,395.41 218,209.39 458,682.84 188,516.14 323,405.19 BOOAURyy: Cm 0.9897 0.9850 0.9723 0.9840 0.9904 464.51 Panel Point Moment 12,933.74 14,604.67 45,069.44 16,425.63 15,243.80 BC Stress: Mid Panel Moment 5,508.67 7,253.98 19,459.18 8,500.21 7,405.47 0.98 Panel Point fb 2,313.41 2,612.28 8,061.39 2,937.98 2,726.59 BC 152.363616 Mid Panel fb 387.64 510.45 1,369.32 598.15 521.12 TC Shear Stress: Fillers 0 0 0 0 0 9,774.13 Panel Point Stress 8,983.65 9,145.92 27,022.00 8,956.69 8,917.28 BC Shear Stress: Mid Panel Stress 0.2773 0.2962 0.7634 0.2865 0.2623 13,602.52 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 67,580.51 71,606.18 4,571.30 43,268.26 18.20 x 0.250 2 A46A=2.5938 x.250 V1S 719.35 10,742.43 3,368.03 3,475.50 2.00 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 2,851.02 61,276.80 43,210.47 45,095.57 13.92 x 0.209 2 A42A=2.6250 x.209 W4 46,031.32 48,746.47 2,931.53 25,345.13 16.53 x 0.188 2 A38B=2.2190 x 0.199 V2 731.92 16,730.22 4,544.02 4,937.94 2.00 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W5 2,276.46 61,276.80 35,913.04 36,714.76 12.90 x 0.188 2 A42A=2.6250 x.209 W6 22,104.66 24,373.24 1,668.03 3,394.50 7.94 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V3 721.90 18,714.09 4,800.79 4,868.95 2.00 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W7 1,071.52 37,440.23 14,085.14 15,438.98 5.39 x 0.176 2 A34A= 1.9380 x 0.176 W8 13,578.55 24,373.24 3,589.30 3,592.70 4.88 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V4 665.37 14,381.54 3,304.13 3,394.14 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W9 12,161.38 28,624.38 5,501.97 7,937.29 4.37 x 0.188 1 CW4OBA= 1.5 x 1.926 x .218 W10 679.96 28,769.10 11,609.89 11,897.03 5.21 x 0.150 2 A28B= 1.7350 x 0.150 V5 608.87 24,373.24 4,417.53 5,027.16 2.00 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W11 12,156.75 15,659.90 737.10 3,901.72 8.03 x 0.102 2 A16B= 1.3750 x 0.102 W11 11,631.19 23,408.44 7,502.40 7,634.72 5.89 x 0.133 2 A24B= 1.5940 x 0.133 V6 608.91 14,381.54 2,697.43 3,146.63 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W10 11,610.05 28,624.38 5,252.54 8,228.71 4.17 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W9 5,500.83 31,392.15 12,158.87 13,256.68 5.18 x 0.158 2 A30B= 1.7970 x 0.158 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 0 Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:59 PM NEW MI L L E N N I UM Location: Joist Description: Mark: BUILoING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J42 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 665.51 14,381.54 3,260.45 3,390.83 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 13,575.34 14,381.54 860.23 2,232.97 6.09 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 1,041.72 37,440.23 14,799.53 15,424.43 5.66 x 0.176 2 A34A= 1.9380 x 0.176 V8 722.22 14,381.54 3,803.39 3,811.02 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 22,816.47 24,373.24 1,633.73 3,389.82 8.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W5 2,236.77 57,194.49 30,024.88 30,796.75 10.78 x 0.188 2 A40B=2.3750 x 0.218 V9 732.51 14,381.54 3,844.71 4,398.32 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 38,590.05 43,005.92 2,887.36 20,253.13 13.86 x 0.188 2 A36B=2.0780 x 0.188 W3 2,826.18 57,194.49 36,999.77 40,189.95 13.29 x 0.188 2 A40B=2.3750 x 0.218 V1 S 755.23 14,381.54 3,574.60 4,285.52 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W2 61,542.32 67,578.15 4,762.24 42,048.96 19.83 x 0.209 2 A44A=2.8750 x.209 STRESS ANALYSIS .- PAGE 3 �, Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:59 PM NEW MILLENNIUNI Location: Joist Description: Mark: Q"" niNG SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J42 TCX Design TCX Left TCX Right TCX Length 0-11 1/2 TCX Length 0-0 3/4 TCX Type S TCX Type R TCX Depth 9 TCX Depth 9 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-11 Clear Bearing 1-0 1/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 582.00 Total Load 582.00 Reqd TL Def L/80 0.14 Reqd TL Def L/80 0.01 Live Load 390.00 Live Load 390.00 Reqd LL Def U120 0.10 Reqd LL Def L/120 0.01 Section Modulus 5.5908 Section Modulus 5.5908 Reqd SM 0.1473 Reqd SM 0.0061 Mom of Inertia 20.0614 Mom of Inertia 20.0614 Reqd MI 0.0414 Reqd MI 0.0003 -Seat Type:T-Plate 1" Seat Type: i-I'tate T" 1 J r Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+A)(+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 , Job Number Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:18:54 AM N E Al M I L L E N N I U M Location: Joist Description: Mark: aLJILoING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J57 Geometry Base Length: Working Length: Joist Depth: Effective Depth BC Panel Length: Shape: 81-8 1/4 81-4 1/4 68.00 1 65.45 19 Special Double Pitch with Ridge @ 40-8 Variable Left End Right End BC Panel 5-8 6-0 1/4 TC Panel 4-0 5-3 A First Half 3-0 1-3 ,`. ilIIetta>� III�IIIItiJ ld 1"ItImilnitifrlii ?Ii1f16wi[1IlIJInitE •}ifAl{' i l lidI[iTifft.- First Diag. 8-8 7-3 1/4 Depth 47.50 47.50 Loads Load Type Category Loadi Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 390.00 390.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) DL(1) 192.00 192.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) SM (1) 32.00 32.00 TC + 0-0 81-8 1/4 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 128.00_ 128.00 BC + 0-0 81-8 1/4 L-BL Uniform(plf) IP(1) 90.00 90.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) DL(1) 60.00 60.00 TC + 0-0 81-8 1/4 L-BL Concw/bending(Ibs) LL(1) 4,000.00 0.00 TC + 10-1 11-2 L-OAL Concw/bending(Ibs) LL(1) 1,000.00 0.00 BC + 11-1 11-1 L-OAL Conc Load(Ibs) LL (1) 1.00_ 0.00 TC + 11-7 11-7 L-OAL Conc w/bending (Ibs) CL(1) 3,000.00 0.00 TC + 13-8 5/8 13-8 5/8 L-OAL Conc w/bending(Ibs) LL(1) 1,000.00 0.00 BC + 21-6 21-6 L-OAL Conc w/bending(Ibs) CL(1) 3,000.00 0.00 TC + 22-0 22-0 L-OAL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Concw/bending(Ibs) LL(1) 1,000.00 0.00 BC + 42-9 1/2 42-9 1/2 L-OAL Conc w/bending (Ibs) CL(1) 3,000.00 0.00 TC + 61-5 5/8 61-5 5/8 L-OAL Conc w/bending (Ibs) LL(1) 1,000.00 0.00 BC + 61-9 61-9 L-OAL Conc w/bending(Ibs) CL(1) 3,000.00 0.00 TC + 69-1 7/8 69-1 7/8 L-OAL Conc w/bending(Ibs) LL(1) 1,000.00 0.00 BC + 72-2 72-2 L-OAL Conc w/bending(Ibs) LL(1) 4,000.00 0.00 TC + 75-11 77-0 L-OAL Gross Uplift(plf) WL(2) 60.00 60.00 TC - 0-0 81-8 1/4 L-BL Conc w/bending(Ibs) LL(2) 4,000.00 0.00 TC - 10-1 11-2 L-OAL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Conc w/bending (Ibs) LL(2) 4,000.00 0.00 TC - 75-11 77-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear. Max TC Comp.: Max BC Tension 96.59 120.00 43,030.52 43,262.67 10,815.67 154,914.23 154,330.38 Member I TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 6,693.21 57,678.14 0.00 0.00 70,049.55 8,572.23 79.90 0-2 VIS 6,578.93 56,535.66 0.00 0.00 4,286.81 7,359.00 51.05 4-0 W3 6,578.93 56,535.66 82,534.61 9,708.14 5,800.46 44,608.82 61.06 5-8 "Continued on Next Page... STRESS ANALYSIS -PAGE 1 �/� Job Number: Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:18:54 AM NEW M I L L E N N!Linn Location: Joist Description: Mark: eu,Lomn SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J57 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W4 13,627.38 119,230.23 82,534.61 9,708.14 49,377.41 6,773.84 77.67 8-8 V2 13,627.38 119,230.23 82,534.61 9,708.14 3,830.72 10,863.09 62.15 13-8 W5 11,804.47 113,195.50 134,889.48 12,568.34 2,418.98 30,724.49 80.96 13-8 W6 12,975.87 147,964.27 134,889.48 12,568.34 18,688.71 1,860.90 80.96 18-8 V3 12,975.87 147,964.27 134,889.48 12,568.34 721.90 5,438.86 56.88 23-8 W7 12,975.87 147,964.27 152,581.75 13,095.11 2,256.03 14,622.78 78.35 23-8 W8 13,065.55 154,811.95 152,581.75 13,095.11 14,096.85 2,174.89 78.35 27-11 1/2 V4 13,065.55 154,811.95 152,581.75 13,095.11 665.37 3,410.24 61.21 32-3 W9 13,065.55 154,811.95 154,185.03 12,932.85 12,625.59 8,447.20 72.32 32-3 W10 12,774.47 152,967.47 154,185.03 12,932.85 1,872.03 12,053.05 70.64 35-3 V5 12,774.47 152,967.47 154,185.03 12,932.85 608.87 2,801.57 64.08 37-11 1/2 W11 12,774.47 152,967.47 150,178.56 12,540.14 12,076.24 1,427.08 73.07 37-11 1/2 W11 12,656.00 153,145.86 150,178.56 12,540.14 12,075.16 1,426.95 73.07 40-8 V6 12,656.00 153,145.86 150,178.56 12,540.14 608.91 2,803.34 64.10 43-41/2 W10 12,656.01 153,145.88 154,330.38 12,681.20 1,872.05 12,053.21 70.66 43-4 1/2 W9 12,658.56 154,914.20 154,330.38 12,681.20 12,622.98 8,445.46 72.34 46-1 V7 12,658.56 154,914.20 154,330.38 12,681.20 665.51 3,413.59 61.24 49-1 W8 12,658.56 154,914.23 152,626.41 12,453.61 14,093.52 1,665.47 78.39 49-1 W7 12,080.84 147,947.20 152,626.41 12,453.61 1,727.00 14,614.21 78.39 53-4 1/2 V8 12,080.84 147,947.20 152,626.41 12,453.61 722.22 5,313.70 56.95 57-8 W6 12,080.84 147,947.22 134,961.14 11,355.48 18,227.30 1,859.54 81.03 57-8 W5 10,320.92 115,288.91 134,961.14 11,355.48 2,248.84 27,611.88 81.03 62-8 V9 10,320.92 115,288.91 134,961.14 11,355.48 785.01 7,408.60 51.96 67-8 W4 10,320.92 115,288.94 71,003.48 8,292.23 52,659.09 3,682.58 94.45 67-8 W3 7,144.68 60,320.93 71,003.48 8,292.23 3,910.89 36,388.44 50.85 74-5 V1S 7,144.68 60,320.93 0.00 0.00 4,281.44 6,857.09 48.46 76-51/4 W2 7,331.26 60,968.12 0.00 0.00 72,667.27 9,209.35 83.44 75-8 STRESS ANALYSIS - PAGE 2 0 Job Number.5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:18:54 AM NEW MILLENNIUM Location: Joist Description: Mark: 9lnLO11JG SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J57 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 4.1882 1.5476 0.9861 2.5085 1.4117 10.0307 0.9798 5043=5 X 5 X.438 BC 2.8594 1.2346 0.7876 2.1017 1.1383 4.3586 1.0000 4037=4 x 4 x .375 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 14,587.07 1,012.11 1,518.17 35-61/2 42-0 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.04 56.05 96.59 24.27 61.05 1.1250 Min Weld Len 2X: Bending Load 641.43 641.43 641.43 641.44 641.44 1.2197 Axial Load 57,678.15 56,535.66 154,914.23 60,320.93 60,968.13 Max Load Fillers TC: fa 6,885.79 6,749.40 13,513.62 7,201.30 7,278.56 184,473.56 Maximum K L/r 46.69 56.84 73.46 24.61 61.91 Max Load no Fillers TC: Fcr 41,905.18 38,866.49 33,281.19 46,907.34 37,224.50 149,279.48 TC OAU Fa 25,143.11 23,319.89 19,968.71 28,144.40 22,334.70 389.1889.18Ryy: F'e 323,395.41 218,209.39 130,638.84 1,163,695.00 183,908.98 BCDAURyy: Cm 0.9894 0.9845 0.9307 0.9969 0.9802 464.51 Panel Point Moment 15,068.28 15,068.35 82,949.02 31,215.56 20,572.36 BC Stress: Mid Panel Moment 4,620.56 10,092.69 42,742.04 15,119.46 15,158.69 0.90 Panel Point fb 2,695.20 2,695.21 14,836.75 5,583.40 3,679.69 15• L/R6: 2.3616 Mid Panel fb 325.14 710.21 3,007.71 2,704.36 1,066.70 TC Shear Stress: Fillers 0 0 0 0 0 10,167.35 Panel Point Stress 9,580.99 9,444.61 28,350.37 12,784.69 10,958.25 BC Shear Stress: Mid Panel Stress 0.2840 0.3117 0.7791 0.3383 0.3597 14,124.21 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 70,049.55 71,606.18 8,572.23 43,268.26 18.87 x 0.250 2 A46A=2.5938 x .250 V1S 4,286.81 28,624.38 7,359.00 8,199.08 2.64 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 5,800.46 61,276.80 44,608.82 45,095.57 14.37 x 0.209 2 A42A=2.6250 x .209 W4 49,377.41 57,194.49 6,773.84 32,384.23 15.25 x 0.218 2 A40B=2.3750 x 0.218 V2 3,830.72 28,597.25 10,863.09 11,278.54 3.90 x 0.188 1 A40B=2.3750 x 0.218 W5 2,418.98 57,194.49 30,724.49 30,827.02 11.04 x 0.188 2 A40B=2.3750 x 0.218 W6 18,688.71 18,714.09 1,860.90 2,687.91 7.15 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V3 721.90 24,373.24 5,438.86 6,072.84 2.00 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W7 2,256.03 37,440.23 14,622.78 15,438.98 5.60 x 0.176 2 A34A= 1.9380 x 0.176 W8 14,096.85 14,381.54 2,174.89 2,235.05 6.33 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V4 665.37 16,730.22 3,410.24 3,836.18 2.00 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W9 12,625.59 28,597.25 8,447.20 9,206.93 4.53 x 0.188 1 A40B=2.3750 x 0.218 W10 1,872.03 31,392.15 12,053.05 13,797.48 5.14 x 0.158 2 A30B= 1.7970 x 0.158 V5 608.87 14,381.54 2,801.57 3,147.58 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W11 12,076.24 15,659.90 1,427.08 3,901.72 7.97 x 0.102 2 A16B= 1.3750 x 0.102 W11 12,075.16 15,659.90 1,426.95 3,901.72 7.97 x 0.102 2 A16B= 1.3750 x 0.102 V6 608.91 14,381.54 2,803.34 3,146.63 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W10 1,872.05 31,392.15 12,053.21 13,790.76 5.14 x 0.158 2 A30B= 1.7970 x 0.158 W9 12,622.98 28,597.25 8,445.46 9,202.89 4.53 x 0.188 1 A40B=2.3750 x 0.218 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 , Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:18:54 AM NEW MI L L E N N I U M Location: Joist Description: Mark: eUILOINO SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J57 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 665.51 16,730.22 3,413.59 3,832.58 2.00 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 14,093.52 14,381.54 1,665.47 2,232.97 6.33 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 1,727.00 37,440.23 14,614.21 15,424.43 5.59 x 0.176 2 A34A= 1.9380 x 0.176 V8 722.22 24,373.24 5,313.70 6,060.62 2.00 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 18,227.30 18,714.09 1,859.54 2,684.15 6.97 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W5 _ 2,248.84 57,194.49 27,611.88 30,796.75 9.92 x 0.188 2 A40B =2.3750 x 0.218 V9 785.01 28,624.38 7,408.60 7,986.31 2.66 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 52,659.09 57,194.49 3,682.58 24,662.11 18.91 x 0.188 2 A408 =2.3750 x 0.218 W3 3,910.89 48,746.47 36,388.44 36,830.25 13.07 x 0.188 2 A38B=2.2190 x 0.199 V1S 4,281.44 24,373.24 6,857.09 7,721.40 2.46 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 72,667.27 79,023.08 9,209.35 52,262.48 21.56 x 0.227 2 3022=3 x 3 x.227 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:18:54 AM NEW MI L LE N N I U M Location: Joist Description: Mark: aLJILoItin SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J57 TCX Design TCX Left TCX Right TCX Length 0-11 1/2 TCX Length 0-0 3/4 TCX Type S TCX Type R TCX Depth 9 TCX Depth 9 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-11 Clear Bearing 1-0 1/8 BPL Material: 4037=4 x 4 x.375 BPL Material:4037=4 x 4 x.375 Total Load 582.00 Total Load 582.00 Reqd TL Def L/80 0.14 Reqd TL Def L/80 0.01 Live Load 390.00 Live Load 390.00 Reqd LL Def L/120 0.10 Reqd LL Def L/120 0.01 Section Modulus 5.5908 Section Modulus 5.5908 Reqd SM 0.1473 Reqd SM 0.0061 Mom of Inertia 20.0614 Mom of Inertia 20.0614 Reqd MI 0.0414 Reqd MI 0.0003 Seat Type:T-Plate 1" Seat Type: i-t ate f f,. Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 �/� Job Number: Job Name: Date Run: �%� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:59 PM NEW MILLENNIUM Location: Joist Description: Mark: SCALDING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J59 Geometry Base Length: Working Length: Joist Depth: Effective Depth BC Panel Length: Shape. 81-81/4 81-41/4 68.00 65.70 9 Special Double Pitch with Ridge @ 40-8 Variable Left End Right End 1 BC Panel 5-8 6-0 1/4 TC Panel 4-0 4-0 t3 /, ; / \ , First Half 3-0 3-0 ��� � 1��I�II iID I I I 1111 ' I i , III '!III(I11i41l?Ntl0111illll!IIII, IL�IIi)Ilili[�"� First Diag. 8-8 9-0 1/4 Depth 47.50 47.50 Loads --- .- - Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) DL(1) 192.00 192.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) LL(1) 390.00 390.00 TC + 0-0 81-8 1/4 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 47.00 47.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) DL(1) 128.00 128.00 BC + 0-0 81-8 1/4 L-BL Uniform(plf) IP (1) 90.00 90.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) SM (1) 32.00 32.00 TC + 0-0 81-8 1/4 L-BL Conc w/bending (Ibs) LL(1) 1,000.00 0.00 BC + 11-1 11-1 L-OAL Conc w/bending (Ibs) CL(1) 3,000.00 0.00 TC + 13-8 5/8 13-8 5/8 L-OAL Conc w/bending (Ibs) LL(1) 1,000.00 0.00 BC + 21-6 21-6 L-OAL Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 24-11 1/2 24-11 1/2 L-OAL Conc @ any pp(Ibs) WL (1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 58-6 1/8 58-6 1/8 L-OAL Conc w/bending(Ibs) LL(1) 1,000.00 0.00 BC + 61-9 61-9 L-OAL •Conc w/bending(Ibs) CL(1) 3,000.00 0.00 TC + 69-1 7/8 69-1 7/8 L-OAL Conc w/bending(Ibs) LL(1) 1,000.00 0.00 BC + 72-2 72-2 L-OAL Gross Uplift(plf) WL(2) 60.00 60.00 TC - 0-0 81-8 1/4 L-BL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL (2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 60.05 120.00 38,130.33 38,005.79 9,532.58 144,545.77 143,778.63 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,471.66 50,789.42 0.00 0.00 61,492.95 4,555.41 80.04 0-2 V1S 3,365.44 49,729.02 0.00 0.00 718.74 3,292.29 51.28 4-0 W3 3,365.44 49,729.02 72,258.41 4,908.95, 2,846.82 38,581.15 61.26 5-8 W4 6,958.93 103,072.65 72,258.41 4,908.95 39,863.76 2,924.78 77.83 8-8 V2 6,958.93 103,072.65 72,258.41 4,908.95 731.77 6,253.83 52.09 13-8 W5 6,958.93 103,072.65 122,493.98 8,478.40 2,272.59 26,394.95 81.13 13-8 W6 9,562.73 137,102.22 122,493.98 8,478.40 19,599.77 1,666.23 81.13 18-8 V3 9,562.73 137,102.22 122,493.98 8,478.40 721.71 6,514.88 57.13 23-8 W7 9,562.73 137,102.22 141,862.78 10,162.74 1,071.63 12,863.53 78.54 23-8 Continued on Next Page... STRESS ANALYSIS - PAGE 1 l/� Job Number: Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:59 PM NEW M I L L E N N I U M Location: Joist Description: Mark: aLIILoING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J59 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W8 10,521.82 144,070.02 141,862.78 10,162.74 12,402.79 858.93 78.54 27-11 1/2 V4 10,521.82 144,070.02 141,862.78 10,162.74 665.18 3,181.92 61.46 32-3 W9 10,521.82 144,070.02 143,478.47 10,617.75 11,116.29 7,581.48 72.53 32-3 W10 10,631.33 142,296.19 143,478.47 10,617.75 679.42 10,614.69 70.86 35-3 V5 10,631.33 142,296.19 143,478.47 10,617.75 608.69 2,611.54 64.34 37-11 1/2 W11 10,631.33 142,296.19 139,722.69 10,545.62 10,635.59 736.54 73.30 37-11 1/2 W11 10,653.19 142,441.31 139,722.69 10,545.62 10,634.64 736.48 73.30 40-8 V6 10,653.19 142,441.31 139,722.69 10,545.62 608.73 2,612.23 64.35 43-41/2 W10 10,653.19 142,441.31 143,778.63 10,649.20 735.11 10,614.84 70.88 43-41/2 W9 10,564.16 144,545.77 143,778.63 10,649.20 11,114.01 5,328.09 72.55 46-1 V7 10,564.16 144,545.77 143,778.63 10,649.20 665.32 3,184.18 61.49 49-1 W8 10,564.16 144,545.77 142,611.83 10,222.19 12,399.90 858.73 78.58 49-1 W7 9,640.93 138,284.70 142,611.83 10,222.19 1,041.89 12,856.04 78.58 53-41/2 V8 9,640.93 138,284.70 142,611.83 10,222.19 722.03 6,673.46 57.20 57-8 W6 9,640.93 138,284.70 124,078.54 8,581.64 19,062.65 1,632.03 81.20 57-8 W5 7,091.46 105,120.33 124,078.54 8,581.64 2,233.03 25,778.66 81.20 62-8 V9 7,091.46 105,120.33 124,078.54 8,581.64 732.36 6,488.64 52.21 67-8 W4 7,091.46 105,120.34 74,592.11 5,076.45 39,525.92 2,880.80 77.92 67-8 W3 3,549.76 52,269.17 74,592.11 5,076.45 2,822.10 38,135.04 61.38 72-8 V1S 3,549.76 52,269.17 0.00 0.00 754.38 3,519.49 53.06 77-81/4 W2 3,683.49 53,671.09 0.00 0.00 63,800.28 4,745.06 83.58 75-8 STRESS ANALYSIS - PAGE 2 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:59 PM NEW MI L L E N N I U M Location: Joist Description: Mark: aLAILOING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J59 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 3.3122 1.2260 0.7846 2.1152 1.1611 4.9786 1.0000 4043=4 X 4 X.438 BC 2.8594 1.2346 0.7876 2.1017 1.1383 4.3586 1.0000 4037=4 x 4 x .375 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 13,267.04 920.52 1,380.79 29-11 5/8 42-0 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.04 56.05 60.05 60.30 46.04 1.1250 Min Weld Len 2X: Bending Load 628.45 628.45 628.46 628.46 628.46 1.4900 Axial Load 50,789.42 49,729.02 144,545.77 52,269.17 53,671.09 Max Load Fillers TC: fa 7,667.02 7,506.95 20,875.05 7,890.40 8,102.03 173,493.50 Maximum K L/r 58.68 71.44 57.40 76.86 58.68 Max Load no Fillers TC: Fcr 38,871.16 34,428.64 39,294.61 32,463.50 38,871.46 151,814.50 Fa 23,322.70 20,657.18 23,576.77 19,478.10 23,322.88 TC DAL/Ryy: 461.55 Fe 202,953.84 136,942.06 212,080.64 118,307.42 202,960.00 BC oAURyy: Cm 0.9811 0.9726 0.9341 0.9667 0.9800 464.51 Panel Point Moment 10,973.92 20,321.13 15,738.63 18,873.41 14,115.60 BC Stress: Mid Panel Moment 6,179.67 4,917.94 7,869.32 7,310.61 7,506.85 0.84 Panel Point fb 3,128.78 5,793.76 4,487.25 5,381.00 4,024.50 BC 152.363616 Mid Panel fb 720.61 573.48 917.63 852.48 875.37 TC Shear Stress: Fillers 0 0 0 0 0 11,206.96 Panel Point Stress 10,795.80 13,300.71 25,362.30 13,271.40 12,126.53 BC Shear Stress: Mid Panel Stress 0.3511 0.3816 0.9158 0.4326 0.3746 12,439.68 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 61,492.95 96,902.01 4,555.41 69,274.07 14.74 x 0.281 2 3028=3 X 3 X.281 V1S 718.74 10,742.43 3,292.29 3,450.99 2.00 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 2,846.82 57,194.49 38,581.15 40,148.20 11.92 x 0.218 2 A40B=2.3750 x 0.218 W4 39,863.76 43,005.92 2,924.78 20,225.34 14.32 x 0.188 2 A36B=2.0780 x 0.188 V2 731.77 24,373.24 6,253.83 6,943.22 2.25 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W5 2,272.59 57,194.49 26,394.95 30,747.75 9.48 x 0.188 2 A40B=2.3750 x 0.218 W6 19,599.77 24,373.24 1,666.23 3,382.27 7.04 x 0.188 1 C38BA= 1.125 x 1.845 x.199 l V3 721.71 28,624.38 6,514.88 6,910.63 2.34 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W7 1,071.63 33,466.47 12,863.53 13,680.62 5.48 x 0.158 2 A32B= 1.9060 x 0.158 W8 12,402.79 14,381.54 858.93 2,225.64 5.57 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V4 665.18 14,381.54 3,181.92 3,371.61 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W9 11,116.29 28,624.38 7,581.48 7,900.10 3.99 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W10 679.42 28,769.10 10,614.69 11,830.90 4.77 x 0.150 2 A28B= 1.7350 x 0.150 V5 608.69 14,381.54 2,611.54 3,127.32 2.00 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W11 10,635.59 15,659.90 736.54 3,877.85 7.02 x 0.102 2 A16B= 1.3750 x 0.102 W11 10,634.64 15,659.90 736.48 3,877.85 7.02 x 0.102 2 A16B= 1.3750 x 0.102 V6 608.73 14,381.54 2,612.23 3,126.37 2.00 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W10 735.11 28,769.10 10,614.84 11,824.69 4.77 x 0.150 2 A28B= 1.7350 x 0.150 W9 11,114.01 28,624.38 5,328.09 7,896.61 3.99 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 "Continued on Next Page... STRESS ANALYSIS -PAGE 2 ' Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:59 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILOING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J59 Web Design, Continued... I Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material I V7 665.32 14,381.54 3,184.18 3,368.33 2.00 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W8 12,399.90 14,381.54 858.73 2,223.57 5.57 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W7 1,041.89 33,466.47 12,856.04 13,667.85 5.48 x 0.158 2 A32B= 1.9060 x 0.158 V8 722.03 28,624.38 6,673.46 6,896.75 2.40 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W6 19,062.65 24,373.24 1,632.03 3,377.61 6.85 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W5 2,233.03 57,194.49 25,778.66 30,717.42_ 9.26 x 0.188 2 A40B=2.3750 x 0.218 V9 732.36 24,373.24 6,488.64 6,919.85 2.33 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 39,525.92 43,005.92 2,880.80 20,190.54 14.16 x 0.188 2 A36B=2.0780 x 0.188 W3 2,822.10 57,194.49 38,135.04 40,095.88 11.78 x 0.218 2 A40B=2.3750 x 0.218 V1S 754.38 14,381.54 3,519.49 4,257.76 2.00 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W2 63,800.28 96,902.01 4,745.06 67,204.39 15.29 x 0.281 2 3028=3 X 3 X.281 STRESS ANALYSIS - PAGE 3 , Job Number: Job Name Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:59 PM NEW Ni I L L E N N I U NI Location: Joist Description: Mark: BUILaING SYSTEMS TIGARD, OR Deep Long Span 68DLH582/390 J59 TCX Design TCX Left TCX Right TCX Length 0-11 1/2 TCX Length 0-0 3/4 TCX Type S TCX Type R i TCX Depth 9 TCX Depth 9 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-10 1/2 Clear Bearing 0-11 7/8 BPL Material: 2024=2 x 2 x.248 BPL Material: 2024=2 x 2 x.248 Total Load 582.00 Total Load 582.00 Reqd TL Def L/80 0.14 Reqd TL Def L/80 0.01 Live Load 390.00 Live Load 390.00 Reqd LL Def L/120 0.10 Reqd LL Def L/120 0.01 Section Modulus 3.5074 Section Modulus 3.5074 Reqd SM 0.1473 Reqd SM 0.0061 Mom of Inertia 9.9572 Mom of Inertia 9.9572 Reqd MI 0.0414 Reqd MI 0.0003 eat Type:T-Plate 1" Seat Type: I-Plate Y i111i Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case Sb: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case Sf: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(0L)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 ) Job Number. Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 12:03:13 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILoING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J61 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 81-8 1/4 81-4 1/4 68.00 65.43 9 Special Double Pitch with Ridge @ 40-8 Variable Left End Right End BC Panel 5-8 6-0 1/4 TC Panel 4-0 5-3 3#tuiur[ut First Half 3-0 1-3 :', 1lifilliMIllilillllilNt1I11 II1)1111 1U(Ulili[liltC i[([ftlVNIlliiiNl 'I 1fiJ111I11LIIlT1fiNr -� First Diag. 8-8 7-3 1/4 Depth 47.50 47.50 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin SplEnd Reference Uniform(plf) LL(1) 390.00 390.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) DL(1) 192.00 192.00 TC + 0-0 81-8 1/4 L-BL Uniform(plf) DL(1) 128.00 128.00 BC + 0-0 81-8 1/4 L-BL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Uniform(plf) IP (1) 90.00 90.00 TC + 0-0 81-8 1/4 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 66.00 66.00 TC + 0-0 81-8 1/4 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Uniform(plf) SM (1) 32.00 32.00 TC + 0-0 81-8 1/4 L-BL Concw/bending (Ibs) LL(1) 4,000.00 0.00 TC + 10-1 11-2 L-OAL Conc w/bending (Ibs) LL(1) 1,000.00 0.00 BC + 11-1 11-1 L-OAL Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 13-8 5/8 13-8 5/8 L-OAL Concw/bending (lbs) CL(1) 3,000.00 0.00 TC + 16-7 1/2 16-7 1/2 L-OAL Conc w/bending (Ibs) LL(1) 900.00 0.00 BC + 21-6 21-6 L-OAL Conc w/bending (lbs) CL(1) 3,000.00 0.00 TC + 22-0 22-0 L-OAL Conc Load(lbs) LL(1) 1,000.00 0.00 BC + 39-3 39-3 L-BL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 41-7 1/2 41-7 1/2 L-OAL Conc w/bending (Ibs) LL(1) 900.00 0.00 BC + 42-9 1/2 42-9 1/2 L-OAL Conc w/bending (Ibs) LL(1) 1,000.00 0.00 BC + 46-4 46-4 L-OAL Conc w/bending (Ibs) CL(1) 3,000.00 0.00 TC + 61-5 5/8 61-5 5/8 L-OAL Concw/bending (Ibs) LL(1) 900.00 0.00 BC + 61-9 61-9 L-OAL Concw/bending (Ibs) CL(1) 3,000.00 0.00 TC + 66-7 1/2 66-7 1/2 L-OAL Concw/bending (Ibs) CL(1) 3,000.00 0.00 TC + 69-1 7/8 69-1 7/8 L-OAL Conc w/bending (Ibs) LL(1) 1,000.00 0.00 BC + 72-2 72-2 L-OAL Concw/bending (Ibs) LL(1) 4,000.00 0.00 TC + 75-11 77-0 L-OAL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Gross Uplift(plf) WL(2) 60.00 60.00 TC - 0-0 81-8 1/4 L-BL Conc @ any pp (Ibs) WL(2) 400.00 0.00 TC - Conc w/bending(Ibs) LL(2) 4,000.00 0.00 TC - 10-1 11-2 L-OAL Conc w/bending(Ibs) LL(2) 4,000.00 0.00 TC - 75-11 77-0 L-OAL Stress Analysis Summary Int Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 81.07 120.00 48,607.96 48,872.34 12,218.08 180,520.17 180,539.75 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 6,696.40 65,400.25 0.00 0.00 79,377.25 8,575.02 79.89 0-2 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 li Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 12:03:13 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILoItiG SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J61 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. 1 V1S 6,582.07 64,246.54 0.00 0.00 4,287.11 7,425.31 51.03 4-0 W3 6,582.07 64,246.54 94,060.48 9,712.63 5,801.36 51,075.98 61.04 5-8 W4 12,149.93 133,913.78 94,060.48 9,712.63 55,901.04 6,703.51 77.65 8-8 V2 12,149.93 133,913.78 94,060.48 9,712.63 1,572.00 10,061.72 52.50 13-8 W5 11,865.35 131,966.50 155,555.33 12,573.61 2,319.29 33,298.14 80.95 13-8 W6 12,981.07 170,3 59.88 155,55 5.33 12,573.61 20,992.97 1,861.31 80.95 18-8 V3 12,981.07 170,359.88 155,555.33 12,573.61 721.92 5,578.70 56.86 23-8 W7 12,981.07 170,359.88 176,342.16 13,100.17 1,728.31 16,521.72 78.33 23-8 W8 13,070.42 179,858.41 176,342.16 13,100.17 15,927.27 860.57 78.33 27-11 1/2 V4 13,070.42 179,858.41 176,342.16 13,100.17 665.38 3,557.34 61.18 32-3 W9 13,070.42 179,858.41 180,027.86 12,937.55 8,641.44 14,264.04 72.30 32-3 W10 12,779.01 179,530.39 180,027.86 12,937.55 9,196.83 13,616.91 70.62 35-3 V5 12,779.01 179,530.39 180,027.86 12,937.55 608.89 2,950.62 64.06 37-11 1/2 W 11 12,779.01 179,530.39 177,013.08 12,544.51 13,643.06 1,427.18 73.05 37-11 1/2 W 11 12,660.51 179,909.02 177,013.08 12,544.51 13,641.83 1,427.05 73.05 40-8 V6 12,660.51 179,909.02 177,013.08 12,544.51 608.93 2,953.39 64.07 43-4 1/2 W10 12,660.51 179,909.05 180,539.75 12,685.81 2,118.83 13,617.09 70.64 43-4 1/2 W9 12,663.27 180,520.16 180,539.75 12,685.81 8,639.65 14,261.09 72.32 46-1 V7 12,663.27 180,520.16 180,539.75 12,685.81 665.53 3,563.48 61.22 49-1 W8 12,663.27 180,520.17 176,934.45 12,458.42 15,923.50 1,665.73 78.37 49-1 W7 12,085.68 170,878.88 176,934.45 12,458.42 1,727.30 16,512.03 78.37 53-4 1/2 V8 12,085.68 170,878.88 176,934.45 12,458.42 722.24 5,456.23 56.93 57-8 W6 12,085.68 170,878.88 156,149.50 11,360.24 20,551.34 1,859.95 81.01 57-8 W5 10,325.45 133,179.47 156,149.50 11,360.24 2,249.24 32,080.88 81.01 62-8 V9 10,325.45 133,179.47 156,149.50 11,360.24 785.03 9,333.28 51.93 67-8 W4 10,325.45 133,179.48 80,847.37 8,296.12 62,017.19 3,683.61 94.44 67-8 W3 7,148.08 68,551.18 80,847.37 8,296.12 3,910.90 41,864.43 50.82 74-5 V1S 7,148.08 68,551.18 0.00 0.00 4,281.50 6,919.88 48.44 76-51/4 W2 7,334.75 69,202.79 0.00 0.00 82,428.27 9,212.47 83.43 75-8 STRESS ANALYSIS - PAGE 2 4 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 12:03:13 PM N E W MI L L E N N I UM Location: Joist Description: Mark: euILo.KM SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J61 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 4.1882 1.5476 0.9861 2.5085 1.4117 10.0307 0.9798 5043=5 X 5 X .438 BC 3.3122 1.2260 0.7846 2.1152 1.1611 4.9786 1.0000 4043=4 X 4 X.438 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 15,864.59 1,100.75 1,651.13 35-6 1/2 42-3 5/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.04 56.05 81.07 24.27 61.05 1.1250 Min Weld Len 2X: Bending Load 647.43 647.43 647.44 647.44 647.44 1.8412 Axial Load 65,400.25 64,246.54 180,520.17 68,551.18 69'202.79 Max Load Fillers TC: fa 7,807.68 7,669.95 20,400.04 8,183.85 8,261.64 214,262.86 Maximum K L/r 46.69 56.84 45.67 24.61 61.91 Max Load no Fillers TC: Fcr 41,905.18 38,866.49 42,187.75 46,907.34 37,224.50 197,255.64 TC OAL/ Fa 25,143.11 23,319.89 25,312.65 28,144.40 22,334.70 389.18Ryy: 89.18 F'e 323,395.41 218,209.39 337,938.44 1,163,695.00 183,908.98 BCDacmyy: Cm 0.9879 0.9824 0.9596 0.9965 0.9775 461.55 Panel Point Moment 10,139.02 25,293.56 41,280.44 27,291.78 21,307.45 BC Stress: Mid Panel Moment 7,016.25 3,642.08 29,708.06 11,951.71 15,120.50 0.91 Panel Point fb 1,813.53 4,524.16 7,383.66 4,881.57 3,811.18 15 : 52.949442 Mid Panel fb 493.73 256.29 2,090.53 2,137.75 1,064.01 TC Shear Stress: Fillers 0 0 0 0 0 11,529.98 Panel Point Stress 9,621.21 12,194.10 27,783.70 13,065.42 12,072.81 BC Shear Stress: Mid Panel Stress 0.3259 0.3370 0.8734 0.3560 0.4039 13,729.50 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 79,377.25 86,681.16 8,575.02 60,534.98 21.38 x 0.250 2 3025=3 x 3 x.250 V1S 4,287.11 28,624.38 7,425.31 8,204.08 2.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 5,801.36 71,606.18 51,075.98 53,365.12 13.76 x 0.250 2 A46A=2.5938 x.250 W4 55,901.04 57,194.49 6,703.51 32,391.09 17.27 x 0.218 2 A40B=2.3750 x 0.218 V2 1,572.00 28,624.38 10,061.72 12,372.06 3.61 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W5 2,319.29, 61,276.80 33,298.14 36,721.38 11.96 x 0.188 2 A42A=2.6250 x.209 W6 20,992.97 24,373.24 1,861.31 3,395.61 7.54 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V3 721.92 24,373.24 5,578.70 6,076.62 2.00 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W7 1,728.31 43,005.92 16,521.72 20,028.33 5.93 x 0.188 2 A36B=2.0780 x 0.188 W8 15,927.27 16,730.22 860.57 2,560.20 6.79 x 0.158 1 C32BA= 1.125 x 1.520 x.158 V4 665.38 16,730.22 3,557.34 3,838.42 2.00 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W9 8,641.44 33,466.47 14,264.04 15,641.42 6.08 x 0.158 2 A32B = 1.9060 x 0.158 W10 9,196.83 31,392.15 13,616.91 13,803.98 5.80 x 0.158 2 A30B = 1.7970 x 0.158 V5 608.89 14,381.54 2,950.62 3,149.44 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W11 13,643.06 15,659.90 1,427.18 3,903.90 9.01 x 0.102 2 A16B= 1.3750 x 0.102 W11 13,641.83 15,659.90 1,427.05 3,903.90 9.01 x 0.102 2 A16B= 1.3750 x 0.102 V6 608.93 14,381.54 2,953.39 3,148.48 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W10 2,118.83 31,392.15 13,617.09 13,797.26 5.80 x 0.158 2 A30B= 1.7970 x 0.158 W9 8,639.65 33,466.47 14,261.09 15,634.83 6.08 x 0.158 2 A32B= 1.9060 x 0.158 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 , Job Number: Job Name: Date Run 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 12:03:13 PM NEW M I L L E N N I U M Location: Joist Description: Mark: SUILoING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J61 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 665.53 16,730.22 3,563.48 3,834.82 2.00 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 15,923.50 16,730.22 1,665.73 2,557.88 6.79 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W7 1,727.30 43,005.92 16,512.03 20,012.04 5.93 x 0.188 2 A36B=2.0780 x 0.188 V8 722.24 24,373.24 5,456.23 6,064.38 2.00 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 20,551.34 24,373.24 1,859.95 3,390.93 7.38 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W5 2,249.24 61,276.80 32,080.88 36,693.57 11.52 x 0.188 2 A42A=2.6250 x.209 V9 785.03 28,624.38 9,333.28 12,514.79 3.35 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 W4 62,017.19 67,578.15 3,683.61 37,582.85 19.98 x 0.209 2 A44A=2.8750 x.209 W3 3,910.90 57,194.49 41,864.43 44,830.75 12.93 x 0.218 2 A408=2.3750 x 0.218 V1S 4,281.50 24,373.24 6,919.88 7,726.57 2.49 x 0.188 1 C38BA= 1.125 x 1.845 x.199 ' W2 82,428.27 86,681.16 9,212.47 58,805.18 22.20 x 0.250 2 3025=3 x 3 x.250 STRESS ANALYSIS - PAGE 3 ' Job Number. Job Name Date Run: 5618-0007 TIGARD HIGH SCHOOL -SHOPORDERS 10/8/2019 12:03:13 PM N EVV MILLENNIUM Location: Joist Description: Mark: BIJILOING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 J61 TCX Design TCX Left TCX Right TCX Length 0-11 1/2 TCX Length 0-0 3/4 TCX Type S TCX Type R TCX Depth 9 TCX Depth 9 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-10 3/4 Clear Bearing 0-11 3/4 BPL Material:2024=2 x 2 x .248 BPL Material:2024=2 x 2 x .248 Total Load 582.00 Total Load 582.00 Reqd TL Def U80 0.14 Reqd TL Def U80 0.01 Live Load 390.00 Live Load 390.00 Reqd LL Def L/120 0.10 Reqd LL Def L/120 0.01 Section Modulus 5.5908 Section Modulus 5.5908 Reqd SM 0.1473 _Reqd SM 0.0061 Mom of Inertia 20.0614 Mom of Inertia 20.0614 Reqd MI 0.0414 Reqd MI 0.0003 Seat Type:T-Plate 1" Seat Type: -t'ate r Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 �/� Job Number: Job Name: Date Run. 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:39:49 PM NEW MI L L E N N I UM Location: Joist Description: Mark: aLrLortiG SYSTEMS TIGARD,OR Long Span 24LH386/260 J62 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 41-11 1/2 41-7 1/2 24.00 22.29 9 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-11 3/4 2-11 TC Panel 2-6 2-11 i First Half 1-6 1-6 3/4 -\ First Diag. 5-5 3/4 4-5 3/4 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position I Direction Loc./Begin Sp/End Reference Uniform (plf) DL(1) 126.00 126.00 TC + 0-0 41-11 1/2 L-BL Uniform (plf) LL(1) 260.00 260.00 TC + 0-0 41-11 1/2 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) LL(1) 95.00 95.00 TC + 0-0 41-11 1/2 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Uniform(plf) DL(1) 84.00 84.00 BC + 0-0 41-11 1/2 L-BL Uniform(plf) IP(1) 60.00 60.00 TC + 0-0 41-11 1/2 L-BL Uniform(plf) SM (1) 21.00 21.00 TC + 0-0 41-11 1/2 L-BL Uniform (plf) DL(1) 37.00 37.00 TC + 0-0 41-11 1/2 L-BL Conc w/bending(Ibs) CL(1) 100.00 0.00 TC + 19-1 19-1 L-OAL Conc Load(Ibs) LL(1) 4,000.00 0.00 TC + 37-7 3/4 38-8 3/4 L-OAL Uniform(plf) LL(1) 0.00 130.00 TC + 38-9 1/2 41-8 3/4 L-OAL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 41-11 1/2 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM(2) 400.00 0.00 TC - Conc Load(Ibs) LL(2) 4,000.00 0.00 TC - 37-7 3/4 38-8 3/4 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 12,690.52 16,571.95 4,142.99 74,489.55 74,974.09 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 2,495.91 25,362.51 0.00 0.00 27,591.63 3,132.43 50.89 0-2 V1S 2,438.81 24,359.49 0.00 0.00 640.80 2,404.14 28.50 2-6 W3 2,438.81 24,359.49 32,200.88 3,362.90 1,622.61 13,576.77 28.65 3-11 3/4 W4 4,522.65 42,171.02 32,200.88 3,362.90 13,626.35 1,756.23 32.76 5-5 3/4 W5 4,522.65 42,171.02 50,686.68 5,624.27 1,634.40 11,641.25 32.76 7-5 3/4 W6 6,667.76 58,087.03 50,686.68 5,624.27 10,118.98 1,555.05 32.76 9-5 3/4 W7 6,667.76 58,087.03 64,010.28 7,653.11 1,435.88 8,103.02 32.76 11-5 3/4 W8 8,580.32 68,818.22 64,010.28 7,653.11 6,580.76 1,415.19 32.76 13-5 3/4 W9 8,580.32 68,818.22 72,149.06 9,449.40 1,415.19 6,087.55 32.76 15-5 3/4 W10 10,260.34 74,343.30 72,149.06 9,449.40 6,087.55 1,415.19 32.76 17-5 3/4 W11 10,260.34 74,343.30 74,974.09 10,932.40 6,087.55 6,056.82 32.76 19-5 3/4 W11 11,304.10 74,489.55 74,974.09 10,932.40 3,140.65 6,087.55 32.76 21-5 3/4 *Continued on Next Page... STRESS ANALYSIS -PAGE 1 ' Job Number: Job Name Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:39:49 PM NEW VIILLENNIUNI Location: Joist Description: Mark: elELCONC SYSTEMS TIGARD,OR Long Span 24LH386/260 J62 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W10 11,304.10 74,489.55 72,527.95 11,617.66 6,087.55 1,384.46 32.76 23-53/4 W9 11,873.09 69,450.99 72,527.95 11,617.66 1,384.46 6,087.55 32.76 25-5 3/4 W8 11,873.09 69,450.99 64,896.98 12,070.38 7,210.52 1,384.46 32.76 27-5 3/4 W7 12,209.54 59,227.63 64,896.98 12,070.38 1,384.46 8,732.78 32.76 29-5 3/4 W6 12,209.54 59,227.63 52,081.21 12,290.56 10,748.75 1,384.46 32.76 31-5 3/4 W5 12,871.96 43,819.45 52,081.21 12,290.56 1,384.46 12,271.01 32.76 33-53/4 W4 12,871.96 43,819.45 34,100.40 13,601.00 14,259.97 1,384.46 32.76 35-53/4 W3 11,165.10 22,718.15 34,100.40 13,601.00 4,148.63 18,047.47 29.13 37-53/4 W2 11,165.10 22,718.15 0.00 0.00 27,565.60 13,623.44 39.82 39-01/2 Standard Verticals Member Position Max Tension Max Comp. Length V1 End Panel _ 7,934.07 5,009.99 28.50 V2 Interior 492.88 1,878.34 22.29 STRESS ANALYSIS - PAGE 2 ',,, Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:39:49 PM N E W M I LL EN N I U M Location: Joist Description: Mark: aI,II nitir. wsTFnns TIGARD,OR Long Span 24LH386/260 J62 Chord Properties Chord Area Rx d Rz Ryy Y lx d Q Material TC 1.6070 0.9260 0.5907 d 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 BC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bndg BC: 0.75 50,000.00 30,000.00 804.14 416.55 624.83 22-0 1/8 28-3 5/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 35.75 24.00 18.75 33.00 1.1250 Min Weld Len 2X: Bending Load 518.00 518.00 518.00, 541.55 606.55 0.8026 Axial Load 25,362.51 24,359.49 74,489.55 22,718.15 22,718.15 Max Load Fillers TC: fa 4,997.54 7,579.18 23,176.59 7,068.50 4,064.80 92,992.19 Maximum K L/r 47.40 60.52 30.47 31.74 55.87 Max Load no Fillers TC: Fcr 42,424.94 38,252.39 46,717.98 46,448.93 39,798.29 89,550.84 Fa 25,454.96 22,951.43 28,030.79 27,869.36 23,878.97 TC .2L/Ryy: 295.21 Fe 606,108.69 192,029.36 757,486.25 698,099.25 1,023,520.25 BCOAL/Ryy: Cm 0.9959 0.9803 0.9795 0.9949 0.9980 295.21 Panel Point Moment 4,932.02 4,932.02 2,072.00 11,792.32 139,247.98 BC stress: Mid Panel Moment 2,116.30 2,645.77 1,036.00 10,121.86 110,252.07 0.78 BC Panel Point fb 1,107.89 3,841.10 1,613.69 3,652.37 16,596.36 81.259 1.2595 Mid Panel fb 403.71 819.46 320.87 3,134.98 13,140.46 TC Shear Stress: Fillers 0 0 0 0 0 9,817.89 Panel Point Stress 6,105.43 11,420.28 24,790.28 10,720.86 20,661.16 BC Shear Stress: Mid Panel Stress 0.1118 0.3557 0.8366 0.3476 0.5252 9,817.89 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 27,591.63 28,624.38 3,132.43 9,686.23 9.91 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W3 1,622.61 28,624.38 13,576.77 15,354.71 4.88 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W4 13,626.35 14,381.54 1,756.23 7,485.99 6.12 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W5 1,634.40 24,373.24 11,641.25 12,032.48 4.18 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 10,118.98 10,742.43 1,555.05 5,752.28 5.28 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W7 1,435.88 16,730.22 8,103.02 8,366.44 3.45 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 6,580.76 7,826.93 1,415.19 3,872.25 4.34 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W9 1,415.19 14,381.54 6,087.55 7,485.99 2.73 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W10 6,087.55 7,826.93 1,415.19 3,872.25 4.02 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W11 6,087.55 14,381.54 6,056.82 7,485.99 2.73 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W11 3,140.65 14,381.54 6,087.55 7,485.99 2.73 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W10 6,087.55 7,826.93 1,384.46 3,872.25 4.02 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W9 1,384.46 14,381.54 6,087.55 7,485.99 2.73 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W8 7,210.52 7,826.93 1,384.46 3,872.25 4.76 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W7 1,384.46 18,714.09 8,732.78 9,629.22 3.34 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 10,748.75 14,381.54 1,384.46 7,485.99 4.83 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,384.46 28,624.38 12,271.01 13,902.98 4.41 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W4 14,259.97 14,381.54 1,384.46 7,485.99 6.40 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 4,148.63 28,624.38 18,047.47 18,623.92 6.48 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:39:49 PM NEW MILLENNIUM Location: Joist Description: Mark: BWLOINO SYSTEMS TIGARD,OR Long Span 24LH3861260 J62 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 27,565.60 29,969.07 13,623.44 18,653.01 5.36 x 0.245 1 WR11A2OB=Wrapped R112 with P V1 7,934.07 14,381.54 5,009.99 9,361.40 3.56 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 492.88 4,802.89 1,878.34 3,038.10 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS -PAGE 3 Job Number. Job Name: Date Run 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:39:49 PM NEW MILLENNIUM Location: Joist Description: Mark: ROIL-CIING SYSTEMS TIGARD,OR Long Span 24LH386/260 J62 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 9-8 1/4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 5 BPL Length 3-2 BPL Length 12-10 7/8 Clear Bearing 0-11 1/8 Clear Bearing 10-3 3/4 BPL Material: 2024=2 x 2 x.248 BPL Material: 302025=3 x 2 x.250 Total Load 386.00 Total Load 956.00 Reqd TL Def L/80 0.00 Reqd TL Def L/120 0.97 Live Load 260.00 Live Load 830.00 Reqd LL Def L/120 0.00 Reqd LL Def L/360 0.32 Section Modulus 4.4517 Section Modulus 8.3903 Reqd SM 0.0000 Reqd SM 4.6416 Mom of Inertia 8.4257 Mom of Inertia 21.7651 Reqd MI 0.0000 Reqd MI 18.4860 Seat Type:Bird Cage(Reinforced) Seat Type:Pegged or Butled(Reinforced) I Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+A)(+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL -SHOPORDERS 10/7/2019 5:51:14 PM NEW MI L L E N N I U M Location: Joist Description: Mark: 6Lllt_01NC SYSTEMS TIGARD,OR Long Span 24LH386/260 J64 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 41-11 1/2 41-7 1/2 24.00 22.30 9 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-11 3/4 _2-3 3/4 TC Panel 2-6 2-3 3/4 First Half 1-6 2-2 --- fmirrlr :rCnq,uttllii f, � First Diag. 5-5 3/4 4-5 3/4 Depth 24.00 24.00 1' Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) LL(1) 260.00 260.00 TC + 0-0 41-11 1/2 L-BL Uniform(plf) DL(1) 126.00 126.00 TC + 0-0 41-11 1/2 L-BL Uniform(plf) LL (1) 95.00 95.00 TC + 0-0 41-10 5/8 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) SM(1) 21.00 21.00 TC + 0-0 41-10 5/8 L-BL Uniform(plf) DL(1) 84.00 84.00 BC + 0-0 41-10 5/8 L-BL Uniform(plf) IP(1) 60.00 60.00 TC + 0-0 41-10 5/8 L-BL Uniform(plf) DL(1) 32.00 32.00 TC + 0-0 41-10 5/8 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Uniform(plf) LL(1) 0.00 130.00 TC + 38-9 1/2 41-8 3/4 L-OAL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 41-10 5/8 L-BL Conc @ any pp (Ibs) SM(2) 400.00 0.00 TC - Conc @ any pp (Ibs) WL(2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear Max TC Comp.: Max BC Tension 24.00 50.00 12,123.91 12,784.80 3,196.20 69,073.70 69,325.06 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,881.76 24,430.95 0.00 0.00 26,300.74 2,515.72 50.90 0-2 V1S 1,824.69 23,439.00 0.00 0.00 640.67 2,097.00 28.50 2-6 W3 1,824.69 23,439.00 30,639.52 2,507.18 1,228.75 12,870.52 28.66 3-11 3/4 W4 3,344.83 40,042.60 30,639.52 2,507.18 14,108.22 1,343.56 32.76 5-5 3/4 W5 3,344.83 40,042.60 48,002.71 4,124.38 1,181.16 12,097.20 32.76 7-5 3/4 W6 4,845.82 54,858.80 48,002.71 4,124.38 10,590.04 1,101.69 32.76 9-5 3/4 W7 4,845.82 54,858.80 60,249.32 5,509.15 982.54 8,589.31 32.76 11-5 3/4 W8 6,114.38 64,535.84 60,249.32 5,509.15 7,082.15 903.22 32.76 13-5 3/4 W9 6,114.38 64,535.84 67,356.78 6,661.50 781.42 5,081.42 32.76 15-5 3/4 W10 7,150.52 69,073.70 67,356.78 6,661.50 4,695.11 702.10 32.76 17-5 3/4 W11 7,150.52 69,073.70 69,325.06 7,500.72 4,695.11 4,695.11 32.76 19-5 3/4 W11 7,550.71 68,472.41 69,325.06 7,500.72 4,695.11 4,695.11 32.76 21-5 3/4 W10 7,550.71 68,472.41 66,154.17 7,542.60 4,695.11 702.10 32.76 23-5 3/4 W9 7,476.38 62,731.93 66,154.17 7,542.60 781.42 5,081.42 32.76 25-5 3/4 W8 7,476.38 62,731.93 57,844.13 7,352.05 7,082.15 903.22 32.76 27-5 3/4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 �/� Job Number Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL -SHOPORDERS 10/7/2019 5:51:14 PM NEW MILLENNIUM Location: Joist Description: Mark: aLAILoItiG SYSTEMS TIGARD,OR Long Span 24LH386/260 J64 Stress Anal/sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W7 7,169.62 51,852.29 57,844.13 7,352.05 982.54 8,589.31 32.76 29-5 3/4 W6 7,169.62 51,852.29 44,394.90 6,929.08 10,590.04 1,101.69 32.76 31-5 3(4 W5 6,630.43 35,926.35 44,394.90 6,929.08 1,181.16 12,097.20 32.76 33-5 3/4 W4 6,630.43 35,926.35 25,798.98 6,273.68 14,108.22 1,343.56 32.76 35-5 3/4 W3 5,921.34 15,044.89 25,798.98 6,273.68 1,519.93 16,419.34 34.26 37-5 3/4 W2 5,921.34 15,044.89 0.00 0.00 18,074.18 7,928.20 34.07 39-7 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V1 End Panel 5,437.30 2,097.00 28.50 V2 Interior 492.87 1,569.64 22.30 STRESS ANALYSIS - PAGE 2 0 Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:51:14 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILoING SYSTEMS TIGARD,OR Long Span 24LH386/260 J64 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 _3028=3 X 3 X.281 BC 1.4375 0.9304 0.5924 1.6850 0.8424 1.2442 0.9613 3025=3 x 3 x.250 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 760.17 393.77 590.66 22-0 1/8 33-8 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 35.75 24.00 26.00 25.75 1.1250 Min Weld Len 2X: Bending Load 513.00 513.00 513.00 545.66 610.66 0.7443 Axial Load 24,430.95 23,439.00 69,073.70 15,044.89 15,044.89 Max Load Fillers TC: fa 4,813.98 7,292.78 21,491.51 4,681.05 2,691.88 93,002.12 Maximum K L/r 47.40 60.52 30.47 44.02 43.59 Max Load no Fillers TC: Fcr 42,424.94 38,252.39 46,717.98 43,396.02 43,513.83 89,560.38 Fa 25,454.96 22,951.43 28,030.79 26,037.61 26,108.30 TC OAL Ryy: 295.21 Fe 606,108.69 192,029.36 757,486.25 363,055.50 1,681,008.25 BCoAURyy. Cm 0.9960 0.9810 0.9810 0.9936 0.9992 296.44 Panel Point Moment 4,884.41 4,884.41 2,052.00 5,970.39 139,247.98 BC Stress: Mid Panel Moment 2,095.87 2,620.23 1,026.00 6,323.61 112,701.73 0.80 BC URz Panel Point fb 1,097.20 3,804.03 1,598.12 1,849.18 16,596.36 84.402: 4.4024 Mid Panel fb 399.82 811.55 317.78 1,958.58 13,432.43 -- TC Shear Stress: Fillers 0 0 0 0 0 7,762.50 Panel Point Stress 5,911.18 11,096.81 23,089.63 6,530.22 19,288.23 BC Shear Stress: Mid Panel Stress 0.1080 0.3429 0.7764 0.1562 0.5001 8,714.47 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 26,300.74 28,624.38 2,515.72 9,684.94 9.45 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W3 1,228.75 24,373.24 12,870.52 13,257.67 4.62 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W4 14,108.22 14,381.54 1,343.56 7,484.67 6.33 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W5 1,181.16 28,624.38 12,097.20 13,900.33 4.34 x 0.188 1 C40BA= 1.125 x 2.014 x .218 W6 10,590.04 10,742.43 1,101.69 5,751.29 5.53 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W7 982.54 18,714.09 8,589.31 9,627.49 3.29 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 7,082.15 7,826.93 903.22 3,871.51 4.68 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 781.42 10,742.43 5,081.42 5,751.29 2.65 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 4,695.11 4,802.89 702.10 1,953.48 4.11 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 4,695.11 10,742.43 4,695.11 5,751.29 2.45 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W11 4,695.11 10,742.43 4,695.11 5,751.29 2.45 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 4,695.11 4,802.89 702.10 1,953.48 4.11 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 781.42 10,742.43 5,081.42 5,751.29 2.65 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 7,082.15 7,826.93 903.22 3,871.51 4.68 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 982.54 18,714.09 8,589.31 9,627.49 3.29 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 10,590.04 10,742.43 1,101.69 5,751.29 5.53 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 1,181.16 28,624.38 12,097.20 13,900.33 4.34 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W4 14,108.22 14,381.54 1,343.56 7,484.67 6.33 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W3 1,519.93 28,624.38 16,419.34 17,177.39 5.90 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 ,/, Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:51:14 PM NEW MI L L E N N I U M Location: Joist Description: Mark: aLIILoING SYSTEMS TIGARD,OR Long Span 24LH386/260 J64 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 18,074.18 18,714.09 7,928.20 10,064.21 6.92 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V1 5,437.30 14,381.54 2,097.00 9,359.28 3.23 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 492.87 4,802.89 1,569.64 3,037.30 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS - PAGE 3 Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:51:14 PM NEW MILLENNIUM Location: I Joist Description: Mark: aLJII_oING SYSTEMS TIGARD,OR Long Span 24LH386/260 J64 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 9-8 1/4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 5 BPL Length 2-11 3/4 BPL Length 12-3 5/8 Clear Bearing 0-11 1/8 Clear Bearing 10-2 3/8 BPL Material: 2024=2 x 2 x.248 BPL Material: 302025=3 x 2 x.250 Total Load 386.00 Total Load 956.00 Reqd TL Def L/80 0.00 Reqd TL Def L/120 0.97 Live Load 260.00 Live Load 830.00 Reqd LL Def U120 0.00 Reqd LL Def U180 0.65 Section Modulus 4.4517 Section Modulus 8.3903 Reqd SM 0.0000 Reqd SM 4.6416 Mom of Inertia 8.4257 Mom of Inertia 21.7651 Reqd MI 0.0000 Reqd MI 9.2430 Seat Type:Bird Cage(Reinforced) Seat Type:Pegged or Butted(Reinforced) t , \\ \ I Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 Job Number Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:26:50 PM NEW MI L L E N N I UM Location: Joist Description: Mark: EIUILOING SYSTEMS TIGARD,OR Long Span 24LH3861260 J66 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 41-10 5/8 41-6 5/8 24.00 22.30 9 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-11 3/4 2-2 7/8 TC Panel 2-6 2-2 7/8 First Half 1-6 2-2 '-\!lIIJIL'lzlliLli'nunni' First Diag. 5-5 3/4 4-4 7/8 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin 1 Sp/End Reference Uniform(plf) LL(1) 260.00 260.00 TC + 0-0 41-10 5/8 L-BL Uniform(plf) DL(1) 126.00 126.00 TC + 0-0 41-10 5/8 L-BL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Uniform(plf) DL(1) 84.00 84.00 BC + 0-0 41-10 5/8 L-BL Uniform (plf) DL(1) 32.00 32.00 TC + 0-0 41-10 5/8 L-BL Uniform (plf) SM (1) 21.00 21.00 TC + 0-0 41-10 5/8 L-BL Uniform (plf) IP (1) 60.00 60.00 TC + 0-0 41-10 5/8 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) LL(1) 95.00 95.00 TC + 0-0 41-10 5/8 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) LL(1) 0.00 130.00 TC + 38-9 1/2 41-8 3/4 L-OAL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL (2) 400.00 _ 0.00 TC - Gross Uplift(plf) WL (2) 36.00 36.00 TC - 0-0 41-10 5/8 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 50.00 12,102.18 12,769.02 3,192.26 68,847.95 69,075.93 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,887.83 24,389.79 0.00 0.00 26,251.16 2,512.73 50.90 0-2 V1S 1,830.76 23,397.85 0.00 0.00 640.66 2,096.80 28.50 2-6 W3 1,830.76 23,397.85 30,577.41 2,515.63 1,229.86 12,842.60 28.66 3-11 3/4 W4 3,356.46 39,957.12 30,577.41 2,515.63 14,146.95 1,349.02 32.76 5-5 3/4 W5 3,356.46 39,957.12 47,893.85 4,139.19 1,186.62 12,135.93 32.76 7-5 3/4 _ W6 4,863.82 54,726.56 47,893.85 4,139.19 10,628.77 1,106.04 32.76 9-5 3/4 W7 4,863.82 54,726.56 60,093.71 5,530.33 986.89 8,628.04 32.76 11-5 3/4 W8 6,138.74 64,356.84 60,093.71 5,530.33 7,120.88 907.57 32.76 13-5 3/4 W9 6,138.74 64,356.84 67,154.42 6,689.05 785.76 5,120.15 32.76 15-5 3/4 W10 7,181.24 68,847.95 67,154.42 6,689.05 4,689.32 706.44 32.76 17-5 3/4 W11 7,181.24 68,847.95 69,075.93 7,528.75 4,689.32 4,689.32 32.76 19-5 3/4 W11 7,581.92 68,199.90 69,075.93 7,528.75 4,689.32 4,689.32 32.76 21-5 3/4 W10 7,581.92 68,199.90 65,858.28 7,576.99 4,689.32 706.44 32.76 23-5 3/4 W9 7,513.95 62,412.66 65,858.28 7,576.99 785.76 5,120.15 32.76 25-5 3/4 W8 7,513.95 62,412.66 57,501.47 7,392.81 7,120.88 907.57 32.76 27-5 3/4 Continued on Next Page... STRESS ANALYSIS -PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:26:50 PM NEW M I L L E N N I U M Location: Joist Description: Mark: eU,LOINC SYSTEMS TIGARD,OR Long Span 241H386/260 J66 Stress Anal jsis Summary,Continued... Member TC Tension TC Compresion BC Tension ,BC Compresion Web Tension Web Comp. Web Length PP Dist. W7 7,213.55 51,486.27 57,501.47 7,392.81 986.89 8,628.04 32.76 29-5 3/4 W6 7,213.55 51,486.27 44,005.50 6,976.20 10,628.77 1,106.04 32.76 31-5 3/4 W5 6,680.73 35,539.36 44,005.50 6,976.20 1,186.62 12,135.93 32.76 33-5 3/4 W4 6,680.73 35,539.36 25,362.81 6,327.16 14,146.95 1,349.02 32.76 35-5 3/4 W3 6,019.84 14,612.67 25,362.81 6,327.16 1,525.65 16,460.30 34.26 37-5 3/4 W2 6,019.84 14,612.67 0.00 0.00 17,729.09 8,117.59 33.41 39-7 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V1 End Panel 5,711.16 2,096.80 28.50 V2 Interior 492.80 1,568.60 22'.30 STRESS ANALYSIS - PAGE 2 ' Job Number: Job Name- TIGARD Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:26:50 PM NEW MILLENNIUM Location: Joist Description: Mark: BuiLoiNc SYSTEMS TIGARD,OR Long Span 24LH386/260 J66 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 BC 1.4375 0.9304 0.5924 1.6850 0.8424 1.2442 0.9613 3025=3 x 3 x.250 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 760.17 395.85 593.78 22-0 1/8 33-8 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 35.75 24.00 26.00 24.88 1.1250 Min Weld Len 2X: Bending Load 513.00 513.00 513.00 546.22 611.22 0.7418 Axial Load 24,389.79 23,397.85 68,847.95 14,612.67 14,612.67 Max Load Fillers TC: fa 4,805.87 7,279.98 21,421.27 4,546.57 2,614.54 93,002.12 Maximum K Ur 47.40 60.52 30.47 44.02 42.11 Max Load no Fillers TC: Fcr 42,424.94 38,252.39 46,717.98 43,396.02 43,919.62 89,560.38 Fa 25,454.96 22,951.43 28,030.79 26,037.61 26,351.77 TC OAURyy: 294.70 F'e 606,108.69 192,029.36 757,486.25 363,055.50 1,801,350.13 BCOA(JRyy: Cm 0.9960 0.9810 0.9811 0.9937 0.9993 295.92 Panel Point Moment 4,884.41 4,884.41 2,052.00 5,871.42 141,316.36 BC Stress: Mid Panel Moment 2,095.87 2,620.23 1,026.00 6,247.57 114,596.40 0.80 BC L/R Panel Pointfb 1,097.20 3,804.03 1,598.12 1,818.52 16,842.88 84.402: 4.4024 Mid Panel fb 399.82 811.55 317.78 1,935.02 13,658.25 TC Shear Stress: Fillers 0 0 0 0 0 7,747.87 Panel Point Stress 5,903.07 11,084.01 23,019.38 6,365.09 19,457.42 BC shear Stress: Mid Panel Stress 0.1079 0.3424 0.7739 0.1528 0.5057 8,698.04 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 26,251.16 28,624.38 2,512.73 9,684.94 9.43 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W3 1,229.86 24,373.24 12,842.60 13,257.67 4.61 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W4 14,146.95 14,381.54 1,349.02 7,484.67 6.35 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,186.62 28,624.38 12,135.93 13,900.33 4.36 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W6 10,628.77 10,742.43 1,106.04 5,751.29 5.55 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 986.89 18,714.09 8,628.04 9,627.49 3.30 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 7,120.88 7,826.93 907.57 3,871.51 4.70 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 785.76 10,742.43 5,120.15 5,751.29 2.67 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 4,689.32 4,802.89 706.44 1,953.48 4.10 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 4,689.32 10,742.43 4,689.32 5,751.29 2.45 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W11 4,689.32 10,742.43 4,689.32 5,751.29 2.45 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 4,689.32 4,802.89 706.44 1,953.48 4.10 x 0.077 1 C1OAB= 1.125 x 0.756 x.077 W9 785.76 10,742.43 5,120.15 5,751.29 2.67 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 7,120.88 7,826.93 907.57 3,871.51 4.70 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 986.89 18,714.09 8,628.04 9,627.49 3.30 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 10,628.77 10,742.43 1,106.04 5,751.29 5.55 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 1,186.62 28,624.38 12,135.93 13,900.33 4.36 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 14,146.95 14,381.54 1,349.02 7,484.67 6.35 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 1,525.65 28,624.38 16,460.30 17,177.39 5.91 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 0. Job Number' Job Name Date Run: 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:26:50 PM NEW M I L L E N N I UM Location.' Joist Description: Mark: BUILoING SYSTEMS TIGARD,OR Long Span 24LH386/260 J66 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 17,729.09 18,714.09 8,117.59 10,193.25 6.78 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V1 5,711.16 14,381.54 2,096.80 9,359.28 3.23 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 492.80 4,802.89 1,568.60 3,037.30 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:26:50 PM NEW MILLENNIUM Location: Joist Description: Mark: aLELOING SYSTEMS TIGARD,OR Long Span 24LH3861260 J66 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 9-9 1/8 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 5 BPL Length 3-2 BPL Length 12-3 3/4 Clear Bearing 0-11 1/8 Clear Bearing 10-3 1/8 BPL Material:2024=2 x 2 x.248 BPL Material: 302025=3 x 2 x.250 Total Load 386.00 Total Load 956.00 Reqd TL Def L/80 0.00 Reqd TL Def L/120 0.98 Live Load 260.00 Live Load 830.00 Reqd LL Def L/120 0.00 Reqd LL Def L/180 0.65 Section Modulus 4.4517 Section Modulus 8.3903 Reqd SM 0.0000 Reqd SM 4.7105 Mom of Inertia 8.4257 Mom of Inertia 21.7651 Reqd MI 0.0000 Reqd MI 9.4497 Seat Type:Bird Cage(Reinforced) Seat Type:Pegged or Butted(Reinforced) I Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+A)(+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+ L+AX+SMCase 8g: DL+CL+0 85( L)+0.75(WL+AX+SL+ SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 ) Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:24:14 PM NEW NI I L L E N N I U NI Location: Joist Descnption: Mark: BLELo NG SYSTEMS TIGARD,OR Long Span 24LH386/260 J68 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 41-111/2 41-71/2 24.00 22.30 9@4-0 Parallel Chords Variable Left End Right End BC Panel 3-11 3/4 2-3 3/4 TC Panel 2-6 First Half 1-6 2-2 I First Diag. 5-5 3/4 4-5 3/4 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference '' Uniform (plf) LL(1) 260.00 260.00 TC + 0-0 41-11 1/2 L-BL Uniform (plf) DL(1) 126.00 126.00 TC + 0-0 41-11 1/2 L-BL Uniform (plf) LL(1) 95.00 95.00 TC + 0-0 41-11 1/2 L-BL Uniform (plf) IP(1) 60.00 60.00 TC + 0-0 41-11 1/2 L-BL Uniform (plf) DL(1) 32.00 32.00 TC + 0-0 41-11 1/2 L-BL Uniform (plf) DL(1) 84.00 84.00 BC + 0-0 41-11 1/2 L-BL Uniform (plf) SM(1) 21.00 21.00 TC + 0-0 41-11 1/2 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Axial (Ibs) SM(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc w/bending(Ibs) CL(1) 300.00 0.00 TC + 14-7 1/2 14-7 1/2 L-OAL Conc w/bending(Ibs) CL(1) 300.00 0.00 TC + 22-21/2 22-21/2 L-OAL Uniform (plf) LL(1) 0.00 130.00 TC + 38-9 1/2 41-8 3/4 L-OAL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 41-11 1/2 L-BL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear. Max TC Comp.: Max BC Tension 24.00 50.00 12,460.84 13,047.87 3,261.97 71,791.16 72,082.27 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,881.76 25,122.07 0.00 0.00 27,069.63 2,515.72 50.90 0-2 V1S 1,824.69 24,130.12 0.00 0.00 640.67 2,100.46 28.50 2-6 W3 1,824.69 24,130.12 31,602.56 2,507.18 1,228.75 13,303.50 28.66 3-11 3/4 W4 3,344.83 41,368.20 31,602.56 2,507.18 14,494.65 1,343.56 32.76 5-5 3/4 W5 3,344.83 41,368.20 49,690.86 4,124.38 1,181.16 12,483.63 32.76 7-53/4 W6 4,845.82 56,909.52 49,690.86 4,124.38 10,976.47 1,101.69 32.76 9-53/4 W7 4,845.82 56,909.52 62,662.60 5,509.15 982.54 8,975.74 32.76 11-5 3/4 W8 6,114.38 67,173.80 62,662.60 5,509.15 7,468.58 903.22 32.76 13-5 3/4 W9 6,114.38 67,173.80 70,034.49 6,661.50 781.42 5,467.85 32.76 15-5 3/4 W10 7,150.52 71,791.16 70,034.49 6,661.50 4,791.72 702.10 32.76 17-53/4 W11 7,150.52 71,791.16 72,082.27 7,500.72 4,791.72 4,791.72 32.76 19-53/4 W11 7,550.71 71,064.23 72,082.27 7,500.72 4,791.72 4,791.72 32.76 21-5 3/4 W10 7,550.71 71,064.23 68,462.94 7,542.60 4,791.72 702.10 32.76 23-5 3/4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number. Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:24:14 PM NEW MILLENNIUM Location: Joist Description: Mark: SUILMING SYSTEMS TIGARD,OR Long Span 24LH386/260 J68 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W9 7,476.38 64,757.62 68,462.94 7,542.60 781.42 5,467.85 32.76 25-5 3/4 W8 7,476.38 64,757.62 59,586.75 7,352.05 7,468.58 903.22 32.76 27-5 3/4 W7 7,169.62 53,311.86 59,586.75 7,352.05 982.54 8,975.74 32.76 29-5 3/4 W6 7,169.62 53,311.86 45,571.39 6,929.08 10,976.47 1,101.69 32.76 31-5 3/4 W5 6,630.43 36,819.77 45,571.39 6,929.08 1,181.16 12,483.63 32.76 33-5 3/4 W4 6,630.43 36,819.77 26,409.34 6,273.68 14,494.65 1,343.56 32.76 35-5 3/4 W3 5,921.34 15,348.60 26,409.34 6,273.68 1,519.93 16,823.37 34.26 37-5 3/4 W2 5,921.34 15,348.60 0.00 0.00 18,475.97 7,928.20 34.07 39-7 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V1 End Panel 5,437.30 2,100.46 28.50 V2 Interior 492.87 1,733.69 22.30 STRESS ANALYSIS - PAGE 2 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:24:14 PM N E W M I L L E N N I U M Location: Joist Description: Mark: E,.IE OING SYSTEMS TIGARD,OR Long Span 24LH386/260 J68 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 BC 1.4375 0.9304 0.5924 1.6850 0.8424 1.2442 0.9613 3025=3 x 3 x.250 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 760.17 393.77 590.66 22-0 1/8 33-8 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 35.75 24.00 26.00 25.75 1.1250 Min Weld Len 2X: Bending Load 513.00 513.00 513.00 545.66 610.66 0.7657 Axial Load 25,122.07 24,130.12 71,791.16 15,348.60 15,348.60 Max Load Fillers TC: fa 4,950.16 7,507.82 22,110.84 4,775.54 2,746.22 92,234.52 Maximum K L/r 47.40 60.52 30.47 44.02 43.59 Max Load no Fillers TC: Fcr 42,424.94 38,252.39 46,717.98 43,396.02 43,513.83 88,821.84 Fa 25,454.96 22,951.43 28,030.79 26,037.61 26,108.30 TC OAL/Ryy: 295.21 F'e 606,108.69 192,029.36 757,486.25 363,055.50 1,681,008.25 BCOAL/Ryy: Cm 0.9959 0.9805 0.9804 0.9934 0.9992 296.44 Panel Point Moment 4,884.41 4,884.41 3,111.85 5,970.39 139,247.98 Bc Stress: Mid Panel Moment 2,095.87 2,620.23 1,798.81 6,323.61 112,701.73 0.84 Panel Pointfb 1,097.20 3,804.03 2,423.54 1,849.18 16,596.36 BcuR2: 84.4024 Mid Panel fb 399.82 811.55 557.14 1,958.58 13,432.43 TC Shear Stress: Fillers 0 0 0 0 0 7,989.43 Panel Point Stress 6,047.36 11,311.85 24,534.38 6,624.72 19,342.57 BC Shear Stress: Mid Panel Stress 0.1107 0.3523 0.8058 0.1580 0.5012 8,969.23 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 27,069.63 28,624.38 2,515.72 9,684.94 9.72 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 1,228.75 28,624.38 13,303.50 15,351.57 4.78 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 14,494.65 16,730.22 1,343.56 8,364.92 6.18 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W5 1,181.16 28,624.38 12,483.63 13,900.33 4.48 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W6 10,976.47 14,381.54 1,101.69 7,484.67 4.93 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 982.54 18,714.09 8,975.74 9,627.49 3.43 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 7,468.58 7,826.93 903.22 3,871.51 4.93 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 781.42 10,742.43 5,467.85 5,751.29 2.85 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W10 4,791.72 4,802.89 702.10 1,953.48 4.19 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W 11 4,791.72 10,742.43 4,791.72 5,751.29 2.50 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W 11 4,791.72 10,742.43 4,791.72 5,751.29 2.50 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W10 4,791.72 4,802.89 702.10 1,953.48 4.19 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W9 781.42 10,742.43 5,467.85 5,751.29 2.85 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 7,468.58 7,826.93 903.22 3,871.51 4.93 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 982.54 18,714.09 8,975.74 9,627.49 3.43 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 10,976.47 14,381.54 1,101.69 7,484.67 4.93 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,181.16 28,624.38 12,483.63 13,900.33 4.48 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 14,494.65 16,730.22 1,343.56 8,364.92 6.18 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W3 1,519.93 28,624.38 16,823.37 17,177.39 6.04 x 0.188 1 CW4OBA= 1.5 x 1.926 x .218 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 /� Job Number. Job Name: Date Run �/J 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:24:14 PM N E W MI L L EN N I UM Location: Joist Description: Mark 9LI1L�1NG SYSTEMS TIGARD,OR Long Span 24LH386/260 J68 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 18,475.97 18,714.09 7,928.20 10,064.21 7.07 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V1 5,437.30 14,381.54 2,100.46 9,359.28 3.23 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 492.87 4,802.89 1,733.69 3,037.30 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS - PAGE 3 Job Number Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:24:14 PM NEW MILLENNIUM Location. Joist Description: Mark: BUILoING SYSTEMS TIGARD,OR Long Span 24LH386/260 J68 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 9-8 1/4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 5 BPL Length 3-2 BPL Length 12-3 3/4 Clear Bearing 0-11 1/8 Clear Bearing 10-2 3/8 BPL Material: 2024=2 x 2 x.248 BPL Material: 302025=3 x 2 x.250 Total Load 386.00 Total Load 956.00 Reqd TL Def L/80 0.00 Reqd TL Def U120 0.97 Live Load 260.00 Live Load 830.00 Reqd LL Def U120 0.00 Reqd LL Def L/180 0.65 Section Modulus 4.4517 Section Modulus 8.3903 Reqd SM 0.0000 Reqd SM 4.6416 Mom of Inertia 8.4257 Mom of Inertia 21.7651 Reqd MI 0.0000 Reqd MI 9.2430 Seat Type:Bird Cage(Reinforced) Seat Type:Pegged or Butted(Reinforced) I Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+A)(+IP STRESS ANALYSIS - PAGE 1 0 Job Number. Job Name: Date Run: /�/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:00:03 AM NEW MI L L E N N I UM Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ23 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 56-4 56-0 48.00 46.17 7 Special Parallel Chords Variable Left End Right End BC Panel 8-1 7-11 TC Panel 4-0 4-0 v . / ���i sv / �1 //\ First Half 0-10 0-10 ,I�III111111 Il NI}1(11111111l]111i111 NII111111111111111414�Il111111J1111tUNllll111111111[14ffilI1111I1111dN�Id111111111k1� First Diag. 8-11 8-9 Depth 48.00 48.00 Loads Load Type Category Load1 Load2 I Position Direction Loc/Begin Sp/End Reference Uniform(plf) LL(1) 370.00 370.00 TC + 0-0 56-4 L-BL Uniform(plf) DL(1) 180.00 180.00 TC + 0-0 56-4 L-BL Uniform(plf) DL(1) 41.00 41.00 TC + 0-0 56-4 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + ,0-0 0-0 L-BL Axial(lbs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 120.00 120.00 BC + 0-0 56-4 L-BL Uniform(plf) IP(1) 84.00 84.00 TC + 0-0 56-4 L-BL Uniform(plf) SM(1) 30.00 30.00 TC + 0-0 56-4 L-BL Axial(Ibs) SM (1) 3,500.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc Load (Ibs) SM (1) 2,800.00 0.00 TC + 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) WL(1) 2,400.00 0.00 TC + 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 4-11 1/2 4-11 1/2 L-OAL __ Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 9-1 1/2 9-1 1/2 L-OAL _ _Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + __ Conc Load (Ibs) LL(1) 1.00 0.00 TC + 30-3 30-3 L-OAL Conc Load(Ibs) LL(1) 4,000.00 0.00 TC + 30-3 31-4 L-OAL __ Conc Load(lbs) LL(1) 1.00 0.00 TC + 31-4 31-4 L-OAL Conc Load(Ibs) SM (1) 2,800.00 0.00 TC + 49-9 1/2 55-9 1/2 L-OAL _ Conc Load(Ibs) WL(1) 2,400.00 0.00 TC + 49-9 1/2 55-9 1/2 L-OAL Gross Uplift(plf) WL(2) 54.00 54.00 TC - 0-0 56-4 L-BL _ Conc Load(Ibs) SM (2) 2,800.00 0.00 TC - 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) WL(2) 2,400.00 0.00 TC - 1-9 1/2 7-9 1/2 L-OAL Conc @ any pp(Ibs) SM(2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - _ Conc Load(Ibs) LL(2) 4,000.00 0.00 TC - 30-3 31-4 L-OAL Conc Load(lbs) WL(2) 2,400.00 0.00 TC - 49-9 1/2 55-9 1/2 L-OAL Conc Load(Ibs) SM (2) 2,800.00 0.00 TC - 49-9 1/2 55-9 1/2 L-OAL Stress Analysis Summary int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 52.00 73.00 27,177.23 22,728.36 6,794.31 91,138.44 90,287.14 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 9,193.03 57,512.63 0.00 0.00 59,717.36 10,997.77 105.62 0-2 _ Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:00:03 AM NEW MILLENNIUM Location: Joist Description: Mark: BUILMINn ..VSTFMS TIGARD,OR Long Span 48LH5501370 TJ23 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. V1S 8,284.38 50,987.03 0.00 0.00 4,722.63 11,516.69 67.32 4-0 W3 8,284.38 50,987.03 50,668.41 9,066.63 3,899.06 19,751.11 47.24 8-1 W4 11,617.49 69,358.64 50,668.41 9,066.63 22,832.57 4,225.12 69.54 8-11 V2 11,617.49 69,358.64 50,668.41 9,066.63 1,896.45 4,355.41 46.17 13-3 W5 11,617.49 69,358.64 73,096.29 13,267.68 3,319.58 15,625.24 58.54 13-3 W6 14,823.11 83,437.16 73,096.29 13,267.68 13,376.88 3,165.51 58.54 16-3 V3 14,823.11 83,437.16 73,096.29 13,267.68 1,896.45 4,022.29 46.17 19-3 W7 14,823.11 83,437.16 84,902.01 16,283.80 2,970.67 10,209.15 58.54 19-3 W8 17,649.74 91,138.44 84,902.01 16,283.80 8,615.92 2,551.31 58.54 22-3 V4 17,649.74 91,138.44 84,902.01 16,283.80 1,896.45 4,345.40 46.17 25-3 W9 17,649.74 91,138.44 90,287.14 19,239.13 9,801.39 9,678.95 66.60 25-3 W9 18,629.84 91,051.20 90,287.14 19,239.13 2,118.65 7,590.83 51.58 29-3 V5 18,629.84 91,051.20 90,287.14 19,239.13 2,174.02 2,704.53 46.17 31-2 W8 18,629.84 91,051.20 83,738.75 17,098.10 8,707.19 2,844.27 59.16 31-2 W7 15,511.69 80,752.09 83,738.75 17,098.10 2,970.67 10,209.15 58.54 34-3 V6 15,511.69 80,752.09 83,738.75 17,098.10 2,174.98 2,329.40 46.17 37-3 W6 15,511.69 80,752.09 69,346.92 13,830.54 13,376.88 3,165.51 58.54 37-3 W5 12,054.64 64,172.52 69,346.92 13,830.54 3,319.58 15,625.24 58.54 40-3 V7 12,054.64 64,172.52 69,346.92 13,830.54 2,174.98 2,634.31 46.17 43-3 W4 12,054.64 64,172.52 43,675.98 9,322.18 22,832.57 4,225.12 69.54 43-3 W3 8,496.93 44,287.38 43,675.98 9,322.18 3,899.06 19,751.11 47.24 47-7 V1S 8,496.93 44,287.38 0.00 0.00 4,640.21 6,909.84 65.88 52-4 W2 9,336.90 47,351.57 0.00 0.00 48,694.70 11,277.95 103.83 48-5 STRESS ANALYSIS - PAGE 2 ,,. Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10l8/2019 9:00:03 AM NEW MILLENNIUM Location: Joist Description: Mark: euiLowG SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ23 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.9266 1.0861 0.6914 1.8874 0.9811 2.2726 0.9552 3528= 3 1/2 x 3 1/2 x.287 BC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 3,741.96 796.04 1,194.06 26-8 7/8 23-9 1/2 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.00 59.00 52.00 57.00 46.00 1.1250 Min Weld Len 2X: Bending Load 591.00 591.00 591.00 591.00 591.00 0.9820 Axial Load 57,512.63 50,987.04 91,138.44 44,287.38 47,351.57 Max Load Fillers TC: fa 14,925.94 13,232.39 23,652.66 11,493.66 12,288.90 98,140.42 Maximum K L/r 66.53 85.33 34.71 82.44 66.53 Max Load no Fillers TC: Fcr 35,058.03 28,719.75 43,903.36 29,709.86 35,058.03 88,364.67 TC OAU Fa 21,034.82 17,231.85 26,342.01 17,825.92 21,034.82 356.04Ryy: 56.04 Fe 159,559.14 96,991.42 260,514.80 103,917.25 159,559.14 Bc OAURyy: Cm 0.9532 0.9318 0.9392 0.9447 0.9615 397.16 Panel Point Moment 13,453.26 13,675.50 9,456.00 13,072.36 12,650.29 BC Stress: Mid Panel Moment 5,715.96 7,865.53 4,728.00 7,140.33 5,513.84 0.94 Panel Point fb 7,455.65 7,578.81 5,240.41 7,244.56 7,010.65 12 23.565822 Mid Panel fb 1,233.81 1,697.81 1,020.56 1,541.27 1,190.18 TC Shear Stress: Fillers 0 0 1 0 0 14,743.47 Panel Point Stress 22,381.59 20,811.20 28,893.07 18,738.22 19,299.55 BC Shear Stress: Mid Panel Stress 0.7528 0.8315 0.9330 0.7002 0.6250 17,592.11 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 59,717.36 96,902.01 10,997.77 56,746.63 14.31 x 0.281 2 3028=3 X 3 X.281 V1S 4,722.63 28,769.10 11,516.69 12,900.81 5.17 x 0.150 2 A28B= 1.7350 x 0.150 W3 3,899.06 31,392.15 19,751.11 21,736.10 8.42 x 0.158 2 A30B= 1.7970 x 0.158 W4 22,832.57 24,373.24 4,225.12 4,396.78 8.20 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V2 1,896.45 14,381.54 4,355.41 5,249.25 2.00 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W5 3,319.58 28,769.10 15,625.24 15,686.93 7.02 x 0.150 2 A28B= 1.7350 x 0.150 W6 13,376.88 14,381.54 3,165.51 3,647.35 6.01 x 0.150 1 C28BB = 1.125 x 1.344 x.150 V3 1,896.45 10,742.43 4,022.29 4,050.96 2.10 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W7 2,970.67 28,624.38 10,209.15 10,873.92 3.67 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 W8 8,615.92 10,742.43 2,551.31 2,788.19 4.50 x 0.129 1 C22BB = 1.125 x 1.110 x.129 V4 1,896.45 14,381.54 4,345.40 5,249.25 2.00 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W9 9,801.39 28,597.25 9,678.95 10,359.73 3.52 x 0.188 1 A40B=2.3750 x 0.218 W9 2,118.65 28,624.38 7,590.83 8,074.13 2.73 x 0.188 1 C40BA= 1.125 x 2.014 x.218 V5 2,174.02 8,984.69 2,704.53 3,237.39 2.00 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 8,707.19 14,381.54 2,844.27 3,586.10 3.91 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 2,970.67 28,624.38 10,209.15 10,873.92 3.67 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 V6 2,174.98 7,826.93 2,329.40 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 13,376.88 14,381.54 3,165.51 3,647.35 6.01 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 3,319.58 28,769.10 15,625.24 15,686.93 7.02 x 0.150 2 A28B= 1.7350 x 0.150 *Continued on Next Page... ' STRESS ANALYSIS - PAGE 2 , Job Number. Job Name. Date Run' �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:00:03 AM N E W MI L L E N N I U M Location: Joist Description: Mark: HULL MINIG SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ23 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 2,174.98 7,826.93 2,634.31 2,664.40 2.00 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W4 22,832.57 24,373.24 4,225.12 4,396.78 8.20 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 3,899.06 31,392.15 19,751.11 21,736.10 8.42 x 0.158 2 A30B= 1.7970 x 0.158 V1S 4,640.21 21,490.90 6,909.84 7,778.82 3.61 x 0.129 2 A22B= 1.5000 x 0.129 W2 48,694.70 79,023.08 11,277.95 45,607.18 14.45 x 0.227 2 3022=3 x 3 x.227 STRESS ANALYSIS -PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:00:03 AM NEW MILLENNIUM Location: Joist Description: Mark: aLELOING SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ23 TCX Design TCX Left TCX Right TCX Length 0-7 1/2 TCX Length 0-9 TCX Type S TCX Type S TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-8 1/8 Clear Bearing 0-8 1/4 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 550.00 Total Load 550.00 Reqd TL Def L/80 0.09 Reqd TL Def L/80 0.11 Live Load 370.00 Live Load 370.00 Reqd LL Def L/120 0.06 Reqd LL Def L/120 0.08 Section Modulus 1.8044 Section Modulus 1.8044 Reqd SM 0.0689 Reqd SM 0.0924 Mom of Inertia 4.5452 Mom of Inertia 4.5452 Reqd MI 0.0137 Reqd MI 0.0212 Seat Type:T-Plate 1" Seat Type:T-Plate 1" L Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c:DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS -PAGE 1 //� Job Number: Job Name: Date Run: �l 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 8:43:49 AM NEW Ni I L L E N N I U M Location: Joist Description: Mark: eL,II ninir SVSTFleS TIGARD,OR Long Span 48LH550/370 TJ25 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: '.. 56-4 56-0 48.00 46.17 7 Special Parallel Chords Variable Left End Right End BC Panel 8-1 7-11 TC Panel 4-0 4-0 -�"-,. First Half 0-10 0-10 4111l)IIIllII�WtID(1IIIIIilalf 1 Hill]iul allIIIRRIIILAIN11JillllilfllflfaldilniIIe,II,4ij11 I1I1/ First Diag. 8-11 8-9 Depth 48.00 48.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) LL(1) 370.00 370.00 TC + 0-0 56-4 L-BL Uniform(plf) DL(1) 180.00 180.00 TC + 0-0 56-4 L-BL Uniform(plf) SM(1) 30.00 30.00 TC + 0-0 56-4 L-BL Axial(Ibs) _ SM(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(pif) DL(1) 120.00 120.00 BC + 0-0 56-4 L-BL Axial(lbs) SM(1) 3,500.00 0.00 TC + 0-0 0-0 L-BL Axial(lbs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 39.00 39.00 TC + 0-0 56-4 L-BL Axial(lbs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(pif) IP(1) 84.00 84.00 TC + 0-0 56-4 L-BL Conc Load(Ibs) WL(1) 2,400.00 0.00 TC + 1-9 1/2 7-9 1/2 L-OAL Conc Load(lbs) SM (1) 2,800.00 0.00 TC + 1-9 1/2 7-9 1/2 L-OAL Conc w/bending(Ibs) CL(1) 500.00 0.00 TC + 28-9 1/2 28-9 1/2 L-OAL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc Load(lbs) LL (1) 1.00 0.00 TC + 30-3 30-3 L-OAL Conc Load(lbs) LL(1) 4,000.00 0.00 TC + 30-3 31-4 L-OAL Conc Load(lbs) LL (1) 1.00 0.00 TC + 31-4 31-4 L-OAL Conc Load(lbs) WL(1) 2,400.00 0.00 TC + 49-9 1/2 55-9 1/2 L-OAL Conc Load(Ibs) SM(1) 2,800.00 0.00 TC + 49-9 1/2 55-9 1/2 L-OAL Gross Uplift(plf) WL(2) 54.00 54.00 TC - 0-0 56-4 L-BL Conc Load(lbs) SM (2) 2,800.00 0.00 TC - 1-9 1/2 7-9 1/2 L-OAL Conc Load(Ibs) WL(2) 2,400.00 0.00 TC - 1-9 1/2 7-9 1/2 L-OAL Conc @ any pp(Ibs) SM(2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc Load (lbs) LL (2) 4,000.00 0.00 TC - 30-3 31-4 L-OAL Conc Load (Ibs) SM (2) 2,800.00 0.00 TC - 49-9 1/2 55-9 1/2 L-OAL Conc Load (lbs) WL(2) 2,400.00 0.00 TC - 49-9 1/2 55-9 1/2 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Camp.: Max BC Tension 52.00 73.00 22,040.87 22,252.72 5,563.18 88,122.74 87,147.58 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 9,193.03 46,950.80 0.00 0.00 47,974.49 10,997.77 105.62 0-2 V1S 8,284.38 43,672.67 0.00 0.00 4,722.63 7,002.14 67.32 4-0 *Continued on Next Page... STRESS ANALYSIS -PAGE 1 0 Job Number: Job Name Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 8:43:49 AM NEW MILLENNIUM Location: Joist Description: Mark: R,oll nimn SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ25 Stress Analysis Summary,Continued... Member 'I TC Tension ,TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 8,284.38 43,672.67 42,905.02 9,066.63 3,899.06 17,895.07 47.24 8-1 W4 11,617.49 62,592.66 42,905.02 9,066.63 22,148.52 4,225.12 69.54 8-11 V2 11,617.49 62,592.66 42,905.02 9,066.63 1,896.45 4,314.24 46.17 13-3 W5 11,617.49 62,592.66 67,026.50 13,267.68 3,319.58 15,058.64 58.54 13-3 W6 14,823.11 78,068.30 67,026.50 13,267.68 12,817.89 3,165.51 58.54 16-3 V3 14,823.11 78,068.30 67,026.50 13,267.68 1,896.45 3,989.44 46.17 19-3 W7 14,823.11 78,068.30 80,238.71 16,283.80 2,970.67 9,657.77 58.54 19-3 W8 17,649.74 87,185.39 80,238.71 16,283.80 7,054.71 2,551.31 58.54 22-3 V4 17,649.74 87,185.39 80,238.71 16,283.80 1,896.45 4,454.05 46.17 25-3 W9 17,649.74 87,185.39 87,147.58 19,239.13 2,737.31 8,025.38 66.60 25-3 W9 18,629.84 88,122.74 87,147.58 19,239.13 2,118.65 6,215.38 51.58 29-3 V5 18,629.84 88,122.74 87,147.58 19,239.13 2,174.02 2,684.89 46.17 31-2 W8 _ 18,629.84 88,122.74 81,153.93 17,098.10 7,464.14 2,844.27 59.16 31-2 W7 15,511.69 78,506.32 81,153.93 17,098.10 2,970.67 9,657.77 58.54 34-3 V6 15,511.69 78,506.32 81,153.93 17,098.10 2,174.98 2,312.17 46.17 37-3 W6 15,511.69 78,506.32 67,444.89 13,830.54 12,817.89 3,165.51 58.54 37-3 W5 12,054.64 62,618.92 67,444.89 13,830.54 3,319.58 15,058.64 58.54 40-3 V7 12,054.64 62,618.92 67,444.89 13,830.54 2,174.98 2,619.21 46.17 43-3 W4 12,054.64 62,618.92 42,633.91 9,322.18 22,148.52 4,225.12 69.54 43-3 W3 8,496.93_ 43,345.66 42,633.91 9,322.18 3,899.06 17,895.07 47.24 47-7 V1S 8,496.93 43,345.66 0.00 0.00 4,640.21 6,892.84 65.88 52-4 W2 9,336.90 46,401.11 0.00 0.00 47,633.58 11,277.95 103.83 48-5 STRESS ANALYSIS - PAGE 2 �,, Job Number Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 8:43:49 AM NEW M I L L E N N I U M Location: Joist Description: Mark: aLJILOING SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ25 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.9266 1.0861 0.6914 1.8874 0.9811 2.2726 0.9552 3528=3 1/2 x 3 1/2 x.287 BC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 3,741.96 796.04 1,194.06 26-8 7/8 23-9 1/2 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.00 59.00 52.00 57.00 46.00 1.1250 Min Weld Len 2X: Bending Load 589.00 589.00, 589.00 589.00 589.00 0.9394 Axial Load 46,950.80 43,672.67 88,122.74 43,345.66 46,401.11 Max Load Fillers TC: fa 12,184.89 11,334.13 22,626.75 11,249.26 12,042.23 96,627.61 Maximum K L/r 66.53 85.33 52.07 82.44 66.53 Max Load no Fillers TC: Fcr 35,058.03 28,719.75 39,519.82 29,709.86 35,058.03 87,011.37 TC Fa 21,034.82 17,231.85 23,711.89 17,825.92 21,034.82 356.04 yy: 56.04 F'e 159,559.14 96,991.42 260,514.80 103,917.25 159,559.14 BC OAURyy: Cm 0.9618 0.9416 0.9418 0.9459 0.9623 397.16 Panel Point Moment 13,406.07 13,629.70 12,879.95 13,028.76 12,605.21 BC Stress: Mid Panel Moment 5,692.51 7,839.51 6,583.97 7,116.99 5,489.68 0.90 Panel Point fb 7,429.49 7,553.43 7,137.93 7,220.40 6,985.67 BC 123.585822 Mid Panel fb 1,228.75 1,692.19 1,421.18 1,536.23 1,184.97 TC Shear Stress: Fillers 0 0 0 0 0 11,907.64 Panel Point Stress 19,614.38 18,887.56 29,764.68 18,469.66 19,027.89 BC Shear Stress: Mid Panel Stress 0.6213 0.7192 1.0028 0.6861 0.6130 14,207.73 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 47,974.49 57,194.49 10,997.77 24,523.86 14.82 x 0.218 2 A4013 =2.3750 x 0.218 V1S 4,722.63 21,490.90 7,002.14 7,449.28 3.66 x 0.129 2 A22B= 1.5000 x 0.129 W3 3,899.06 28,769.10 17,895.07 19,384.41 8.03 x 0.150 2 A28B= 1.7350 x 0.150 W4 22,148.52 24,373.24 4,225.12 4,396.78 7.95 x 0.188 1 C38BA= 1.125 x 1.845 x .199 V2 1,896.45 14,381.54 4,314.24 5,249.25 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W5 3,319.58 28,769.10 15,058.64 15,686.93 6.76 x 0.150 2 A28B= 1.7350 x 0.150 W6 12,817.89 14,381.54 3,165.51 3,647.35 5.75 x 0.150 1 C28BB= 1.125 x 1.344 x .150 V3 1,896.45 10,742.43 3,989.44 4,050.96 2.08 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W7 2,970.67 28,624.38 9,657.77 10,873.92 3.47 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W8 7,054.71 10,742.43 2,551.31 2,788.19 3.68 x 0.129 1 C22BB= 1.125 x 1.110 x .129 V4 1,896.45 14,381.54 4,454.05 5,249.25 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W9 2,737.31 28,624.38 8,025.38 9,010.04 2.88 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W9 2,118.65 24,373.24 6,215.38 7,046.40 2.23 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V5 2,174.02 8,984.69 2,684.89 3,237.39 2.00 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 7,464.14 14,381.54 2,844.27 3,586.10 3.35 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 2,970.67 28,624.38 9,657.77 10,873.92 3.47 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 V6 2,174.98 7,826.93 2,312.17 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W6 12,817.89 14,381.54 3,165.51 3,647.35 5.75 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 3,319.58 28,769.10 15,058.64 15,686.93 6.76 x 0.150 2 A28B= 1.7350 x 0.150 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 �/� Job Number: Job Name; Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 8:43:49 AM NEW Ni I L L E N N I U M Location; Joist Description: Mark: aLIILOING SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ25 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 2,174.98 7,826.93 2,619.21 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W4 22,148.52 24,373.24 4,225.12 4,396.78 7.95 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 3,899.06 28,769.10 17,895.07 19,384.41 8.03 x 0.150 2 A28B= 1.7350 x 0.150 V1S 4,640.21 21,490.90 6,892.84 7,778.82 3.60 x 0.129 2 A22B = 1.5000 x 0.129 W2 47,633.58 48,746.47 11,277.95 19,130.94 16.12 x 0.199 2 A38B=2.2190 x 0.199 STRESS ANALYSIS - PAGE 3 li Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 8:43:49 AM NEW MILLENNIUM Location: Joist Description: Mark: BLELCENG SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ25 TCX Design TCX Left TCX Right TCX Length 0-7 1/2 TCX Length 0-9 TCX Type S TCX Type S TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-9 7/8 Clear Bearing 0-10 1/8 BPL Material:2024 =2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 550.00 Total Load 550.00 Reqd TL Def L/80 0.09 Reqd TL Def L/80 0.11 Live Load 370.00 Live Load 370.00 Reqd LL Def L/120 0.06 Reqd LL Def U120 0.08 Section Modulus 1.8044 Section Modulus 1.8044 Reqd SM 0.0689 Reqd SM 0.0924 Mom of Inertia 4.5452 Mom of Inertia 4.5452 Reqd MI 0.0137 Reqd MI 0.0212 Seat Type:T-Plate 1" Seat Type:T-Plate 1' Load Combinations Case 1:DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c:DL+WL+A)(+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:58:15 PM NEW M I L L E N N I U M Location: Joist Description: Mark: BUILMING SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ28 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-6 7/8 32-2 7/8 24.00 22.48 7 Special Parallel Chords Variable Left End Right End BC Panel 3-4 3-2 7/8 _ TC Panel 2-2 2-1 First Half 1-0 1-0 i If i i ' First Diag. 4-4 4-2 7/8 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction LocBegin Sp/End Reference Uniform (plf) LL(1) 230.00 230.00 TC + 0-0 32-6 7/8 L-BL Uniform (plf) DL(1) 114.00 114.00 TC + 0-0 32-6 7/8 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) IP(1) 54.00 54.00 TC + 0-0 32-6 7/8 L-BL Uniform (plf) SM (1) 19.00 19.00 TC + 0-0 32-6 7/8 L-BL Uniform (plf) DL(1) 76.00 76.00 BC + 0-0 32-6 7/8 L-BL Uniform(plf) DL(1) 21.00 21.00 TC + 0-0 32-6 7/8 L-BL Conc w/bending (Ibs) CL(1) 3,000.00 0.00 TC + 8-3 8-3 L-OAL Conc Load (Ibs) LL(1) 1.00 0.00 TC + 18-3 1/2 18-3 1/2 L-OAL Conc Load (Ibs) LL(1) 4,000.00 0.00 TC + 18-3 1/2 19-4 1/2 L-OAL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Conc Load(Ibs) LL (1) 1.00 0.00 TC + 19-4 1/2 19-4 1/2 L-OAL Conc Load(Ibs) CL(1) 200.00 0.00 TC + 22-11 22-11 L-OAL Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-6 7/8 L-BL Conc Load(Ibs) LL(2) 4,000.00 0.00 TC - 18-3 1/2 19-4 1/2 L-OAL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 33.50 57.50 11,564.93 9,547.02 2,891.23 51,468.30 51,259.35 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 4,476.90 19,950.07 0.00 0.00 21,916.79 5,396.37 44.15 0-2 V1S 4,046.86 19,498.47 0.00 0.00 3,270.82 3,424.57 26.48 2-2 W3 4,046.86 19,498.47 23,700.04 5,092.01 2,407.75 11,705.06 25.48 3-4 W4 7,182.31 32,947.64 23,700.04 5,092.01 12,347.51 3,050.67 32.88 4-4 V2 7,182.31 32,947.64 23,700.04 5,092.01 2,081.23 4,816.21 22.48 6-4 W5 7,182.31 32,947.64 38,395.23 9,272.61 3,050.67 9,634.18 32.88 6-4 W6 11,362.92 43,430.45 38,395.23 9,272.61 8,566.22 3,050.67 32.88 8-4 V3 11,362.92 43,430.45 38,395.23 9,272.61 2,081.23 2,974.10 22.48 10-4 W7 11,362.92 43,430.45 47,329.41 13,453.22 3,050.67 7,053.52 32.88 10-4 W8 16,370.93 51,468.30 47,329.41 13,453.22 5,206.11 3,735.56 40.34 12-4 V4 16,370.93 51,468.30 47,329.41 13,453.22 2,081.23 3,149.39 22.48 15-11/2 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 , Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:58:15 PM NEW M I L L E N N I U M Location: Joist Description: Mark: BUILaINIO SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ28 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W9 16,370.93 51,468.30 51,259.35 16,579.53 4,324.54 3,119.03 33.62 15-11/2 W9 15,352.72 49,454.77 51,259.35 16,579.53 2,432.52 3,554.61 26.22 17-21/2 V5 15,352.72 49,454.77 51,259.35 16,579.53 2,042.80 2,044.43 22.48 18-4 W8 15,352.72 49,454.77 45,336.23 13,171.72 5,705.16 3,050.67 32.88 18-4 W7 10,990.72 40,233.53 45,336.23 13,171.72 3,050.67 7,053.52 32.88 20-4 V6 10,990.72 40,233.53 45,336.23 13,171.72 2,042.80 2,043.98 22.48 22-4 W6 10,990.72 40,233.53 34,026.69 8,809.73 8,566.22 3,050.67 32.88 22-4 W5 6,628.73 27,433.53 34,026.69 8,809.73 3,050.67 9,634.18 32.88 24-4 V7 6,628.73 27,433.53 34,026.69 8,809.73 2,042.80 2,043.52 22.48 26-4 W4 6,628.73 27,433.53 18,990.44 4,447.74 12,347.51 3,050.67 32.88 26-4 W3 3,357.24 15,834.36 18,990.44 4,447.74 2,407.75 11,705.06 25.48 28-4 V1S 3,357.24 15,834.36 0.00 0.00 3,270.82 3,424.57 26.41 30-57/8 W2 3,360.99 16,271.86 0.00 0.00 17,671.59 4,250.49 43.18 29-4 STRESS ANALYSIS - PAGE 2 0 Job Number 5618-0007 Job Name Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:58:15 PM NEW MILLENNIUN1 Location: Joist Description: Mark: aE LOING SYSTEMS TIGARD,OR Long Span 24LH3441230 TJ28 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.1207 0.8991 0.5436 1.6512 0.8225 0.9058 0.9280 A44A=2.8750 x.209 BC 0.9485 0.7361 0.4403 1.4631 0.7019 0.5140 1.0000 A40B=2.3750 x 0.218 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bndg BC: I 0.75 50,000.00 30,000.00 521.85 581.81 872.71 22-1 3/8 17-0 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 33.50 25.88 23.00 1.1250 Min Weld Len 2X: Bending Load 365.00 365.00 365.00 365.00 365.00 0.5546 Axial Load 19,950.07 19,498.47 51,468.30 15,834.36 16,271.86 Max Load Fillers TC: fa 4,863.03 8,699.24 22,962.57 7,064.49 3,966.42 57,373.68 Maximum K Ur 44.15 47.83 46.22 47.60 42.31 Max Load no Fillers TC: Fcr 40,650.88 39,728.11 40,138.28 39,787.30 41,091.95 52,939.34 Fa 24,390.53 23,836.86 24,082.97 23,872.38 24,655.17 TC OAURyy: 234.30 F'e 839,250.44 342,268.59 366,523.31 345,583.53 913,815.19 BC OAURyy: Cm 0.9971 0.9873 0.9580 0.9898 0.9978 264.42 Panel Point Moment 16,569.39 6,526.34 2,844.59 1,796.99 1,796.99 BC Stress: Mid Panel Moment 12,300.63 3,720.19 1,422.30 864.95 1,095.53 0.90 Panel Point fb 4,139.48 7,394.19 3,222.86 2,035.95 448.94 13 . 30.595928 Mid Panel fb 3,073.03 4,214.89 645.75 392.70 279.70 TC Shear Stress: Fillers 0 0 0 0 0 12,097.13 Panel Point Stress 9,002.51 16,093.43 26,185.43 9,100.45 4,415.36 BC Shear stress: Mid Panel Stress 0.2108 0.5037 0.9755 0.3088 0.0905 14,737.99 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 21,916.79 24,373.24 5,396.37 10,063.55 7.87 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1S 3,270.82 7,826.93 3,424.57 4,501.38 2.26 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W3 2,407.75 24,373.24 11,705.06 14,243.97 4.20 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 12,347.51 14,381.54 3,050.67 7,464.43 5.54 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 2,081.23 7,826.93 4,816.21 4,936.88 3.18 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 3,050.67 24,373.24 9,634.18 11,995.81 3.46 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 8,566.22 8,984.69 3,050.67 4,673.73 4.89 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V3 2,081.23 4,802.89 2,974.10 3,025.15 2.60 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W7 3,050.67 14,381.54 7,053.52 7,464.43 3.17 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W8 5,206.11 8,984.69 3,735.56 3,853.18 2.97 x 0.118 1 C18BB= 1.125 x 1.035 x .118 V4 2,081.23 5,758.64 3,149.39 3,731.49 2.36 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W9 4,324.54 7,826.93 3,119.03 3,789.69 2.86 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W9 2,432.52 7,826.93 3,554.61 4,528.80 2.35 x 0.102 1 C16BB= 1.125 x 1.025 x .102 V5 2,042.80 4,802.89 2,044.43 3,025.15 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W8 5,705.16 7,826.93 3,050.67 3,860.25 3.77 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W7 3,050.67 14,381.54 7,053.52 7,464.43 3.17 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V6 2,042.80 4,802.89 2,043.98 3,025.15 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W6 8,566.22 8,984.69 3,050.67 4,673.73 4.89 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 3,050.67 24,373.24 9,634.18 11,995.81 3.46 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... STRESS ANALYSIS -PAGE 2 , Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:58:15 PM NEW M I L L E N N I UM Location: Joist Description: Mark: auILOING SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ28 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 2,042.80 4,802.89 2,043.52 3,025.15 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W4 12,347.51 14,381.54 3,050.67 7,464.43 5.54 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 2,407.75 24,373.24 11,705.06 14,243.97 4.20 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1S 3,270.82 7,826.93 3,424.57 4,508.29 2.26 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W2 17,671.59 18,714.09 4,250.49 8,295.31 6.76 x 0.176 1 C34AA= 1.125 x 1.549 x.176 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Rung 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:58:15 PM NEW MILLENNIUM Location: Joist Description: Mark: eUILoItiG SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ28 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-1 1/8 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-5 BPL Length 2-9 1/8 Clear Bearing 0-9 3/4 Clear Bearing 0-9 7/8 BPL Material:2024 =2 x 2 x.248 BPL Material:2024 =2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def L/80 0.01 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L/120 0.01 Section Modulus 3.9167 Section Modulus 3.9167 Reqd SM 0.5523 Reqd SM 0.0047 Mom of Inertia 6.9287 Mom of Inertia 6.9287 Reqd MI 0.5845 Reqd MI 0.0003 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f:DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS -PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 1:52:00 PM NEW MILLENNIUM Location: Joist Desc,lption: Mark: eui1_oiNa SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ34 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-4 32-0 24.00 22.73 7 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-4 3-0 . . W w , ..___,.. „.,...,: ,.:u tlry..a Fir 2-2 2-0 First Half Half 1-0 1-0 / \ First Diag. 4-4 4-0 i Depth 24.00 24.00 Loads Load Type Category Loadl Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 230.00 230.00 TC + 0-0 32-4 L-BL Uniform (plf) DL(1) 114.00 114.00 TC + 0-0 32-4 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 17.00 17.00 TC + 0-0 32-4 L-BL Uniform(plf) LL(1) 85.00 85.00 TC + 0-0 32-4 L-BL Uniform(plf) DL(1) 76.00 76.00 BC + 0-0 32-4 L-BL Uniform (plf) IP(1) 54.00 54.00 TC + 0-0 32-4 L-BL Uniform(plf) SM (1) 19.00 19.00 TC + 0-0 32-4 L-BL Conc @ any pp(Ibs) SM (1) 400.00' 0.00 TC + Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Uniform(plf) LL(1) 0.00 466.00 TC + 21-9 7/8 33-3 7/8 L-OAL Conc w/bending(Ibs) CL(1) 2,000.00 0.00 TC + 33-10 33-10 L-OAL Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-4 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 8,681.43 12,832.88 3,208.22 39,482.73 39,489.13 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,734.85 15,045.04 0.00 0.00 15,959.68 2,304.58 44.28 0-2 V1S 1,344.51 14,521.79 0.00 0.00 1,163.61 1,424.01 26.69 2-2 W3 1,344.51 14,521.79 16,898.80 1,557.78 842.46 9,351.97 25.70 3-4 W4 1,934.83 24,220.36 16,898.80 1,557.78 9,750.17 996.20 33.05 4-4 W5 1,934.83 24,220.36 28,811.74 2,403.79 836.22 7,424.36 33.05 6-4 W6 2,831.44 33,408.68 28,811.74 2,403.79 6,127.12 748.97 33.05 8-4 W7 2,831.44 33,408.68 36,355.22 3,195.74 588.99 4,665.72 33.05 10-4 W8 3,496.68 38,553.62 36,355.22 3,195.74 4,665.72 501.73 33.05 12-4 W9 3,496.68 38,553.62 39,489.13 3,699.07 4,650.04 4,665.72 33.05 14-4 W9 3,450.92 39,482.73 39,489.13 3,699.07 4,650.04 4,665.72 33.05 16-4 W8 3,450.92 39,482.73 38,195.66 3,139.42 4,665.72 501.73 33.05 18-4 W7 2,764.57 35,824.41 38,195.66 3,139.42 588.99 4,665.72 33.05 20-4 W6 2,764.57 35,824.41 31,905.69 2,326.35 6,127.12 748.97 33.05 22-4 W5 1,824.79 26,618.24 31,905.69 2,326.35 836.22 7,424.36 33.05 24-4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 1:52:00 PM NEW M I L L E N N I U M Location: Joist Description: Mark: IMELoINC SYSTEMS TIGARD, OR Long Span 24LH344/230 TJ34 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W4 1,824.79 26,618.24 19,538.87 1,259.86 9,750.17 996.20 33.05 26-4 W3 945.72 16,046.37 19,538.87 1,259.86 842.46 9,351.97 25.70 28-4 V1S 945.72 16,046.37 0.00 0.00 520.73 3,197.04 25.70 30-4 W2 976.08 17,340.68 0.00 0.00 19,976.52 1,528.34 40.90 29-4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 470.00 1,650.26 22.73 STRESS ANALYSIS - PAGE 2 0 Job Number Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/20191:52:00 PM NEW MILLENNIUM Location: Joist Description: Mark: EUILoING SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ34 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.8084 0.6885 0.4106 1.3990 0.6554 0.3832 1.0000 A38B=2.2190 x 0.199 BC 0.7132 0.6446 0.3831 1.3432 0.6159 0.2963 1.0000 A36B=2.0780 x 0.188 Axial and Bending Analysis K: Fy: Fb: Mom of media: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 392.85 447.89 671.84 18-9 26-10 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 24.00 24.00 22.00 1.1250 Min Weld Len 2X: Bending Load 446.00 446.00 479.69 816.55 881.12 0.5000 Axial Load 15,045.04 14,521.79 39,482.73 16,046.37 17,340.68 Max Load Fillers TC: fa 4,326.02 8,981.81 24,420.29 9,924.77 4,986.11 44,490.32 Maximum K L/r 58.45 63.32 43.84 58.45 53.58 Max Load no Fillers TC: Fcr 38,947.56 37,294.54 43,445.47 38,947.56 40,532.97 41,153.20 Fa 23,368.54 22,376.72 26,067.28 23,368.54 24,319.78 TCOA1JRyy: 274.47 Fe 835,977.38 200,705.34 418,755.59 235,550.02 994,882.19 Bc OAURyy: Cm 0.9974 0.9776 0.9609 0.9789 0.9975 285.89 Panel Point Moment 16,569.29 2,202.36 1,918.75 4,483.96 4,483.97 BC Stress: Mid Panel Moment 12,523.48 1,432.20 959.37 1,234.81 12,200.31 0.92 Panel Point fb 4,640.60 4,493.24 3,914.60 9,148.13 1,255.84 12 .29: 25.2937 Mid Panel fb 3,507.48 1,224.77 820.42 1,055.96 3,881.22 TC Shear Stress: Fillers 0 0 0 0 0 17,124.67 Panel Point Stress 8,966.62 13,475.05 28,334.90 19,072.90 6,241.94 BC Shear Stress: Mid Panel Stress 0.2102 0.4397 0.9627 0.4577 0.3207 19,601.65 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 15,959.68 16,730.22 2,304.58 6,997.47 6.80 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W3 842.46 16,730.22 9,351.97 9,828.81 3.99 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W4 9,750.17 10,742.43 996.20 5,713.48 5.09 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 836.22 14,381.54 7,424.36 7,434.44 3.33 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,127.12 7,826.93 748.97 3,843.58 4.05 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 588.99 10,742.43 4,665.72 5,713.48 2.44 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 4,665.72 4,802.89 501.73 1,924.39 4.08 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 4,650.04 10,742.43 4,665.72 5,713.48 2.44 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W9 4,650.04 10,742.43 4,665.72 5,713.48 2.44 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 4,665.72 4,802.89 501.73 1,924.39 4.08 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W7 588.99 10,742.43 4,665.72 5,713.48 2.44 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W6 6,127.12 7,826.93 748.97 3,843.58 4.05 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W5 836.22 14,381.54 7,424.36 7,434.44 3.33 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W4 9,750.17 10,742.43 996.20 5,713.48 5.09 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W3 842.46 16,730.22 9,351.97 9,828.81 3.99 x 0.158 1 C32BA= 1.125 x 1.520 x .158 W2 19,976.52 24,373.24 1,528.34 10,859.95 7.17 x 0.188 1 C38BA= 1.125 x 1.845 x .199 V1 1,163.61 5,758.64 3,197.04 3,394.83 2.39 x 0.090 1 C12BB= 1.125 x 0.799 x .090 V2 470.00 4,802.89 1,650.26 3,007.29 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 1:52:00 PM NEW MILLENNIUNt Location: Joist Description: Mark: aLIILoINIG SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ34 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-5 BPL Length 2-6 1/2 Clear Bearing 0-10 1/8 Clear Bearing 0-9 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def U120 0.27 Reqd TL Def L/80 0.00 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def U120 0.00 Section Modulus 3.1434 Section Modulus 3.1434 Reqd SM 0.5523 Reqd SM 0.0000 Mom of Inertia 5.8509 Mom of Inertia 5.8509 Reqd MI 0.5845 Reqd MI 0.0000 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case Sf: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 f/� Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:07:07 PM NEW NI I L L E N N I U Nt'Location: Joist Description: Mark: e�,1_oItiG SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ37 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 32-4 32-0 24.00 22.35 7 Special Parallel Chords Variable Left End Right End BC Panel 3-4 3-0 TC Panel 2-2 2-0 t , _I rr�� 1 oimTm a millll(� First Half 1-0 1-0 First Diag. 4-4 4-0 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) DL(1) 114.00 114.00 TC + 0-0 32-4 L-BL Uniform(plf) LL(1) 230.00 230.00 TC + 0-0 32-4 L-BL Uniform(plf) SM (1) 19.00 19.00 TC + 0-0 32-4 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Uniform(plf) IP(1) 54.00 54.00 TC + 0-0 32-4 L-BL Uniform(plf) DL(1) 76.00 76.00 BC + 0-0 32-4 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) DL(1) 22.00 22.00 TC + 0-0 32-4 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) LL(1) 85.00 85.00 TC + 0-0 32-4 L-BL Conc @ any pp(Ibs) SM(1) 400.00 0.00 TC + Conc Load (Ibs) LL(1) 4,000.00 0.00 TC + 18-3 1/2 19-4 1/2 L-OAL Uniform(plf) LL(1) 0.00 466.00 TC + 21-9 7/8 33-3 7/8 L-OAL Conc w/bending(Ibs) CL(1) 2,000.00 0.00 TC + 33-10 33-10 L-OAL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-4 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc Load(Ibs) LL(2) 4,000.00 0.00 TC - 18-3 1/2 19-4 1/2 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear. Max TC Comp.: Max BC Tension 33.50 57.50 10,828.44 14,970.87 3,742.72 56,142.05 56,683.54 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 4,499.89 17,936.18 0.00 0.00 20,381.01 5,390.39 44.09 0-2 VIS 4,067.53 17,397.66 0.00 0.00 3,259.00 3,617.79 26.38 2-2 W3 4,067.53 17,397.66 21,810.20 5,117.95 2,427.60 11,796.74 25.37 3-4 W4 7,218.80 30,693.16 21,810.20 5,117.95 12,937.77 3,082.73 32.80 4-4 V2 7,218.80 30,693.16 21,810.20 5,117.95 2,067.01 3,089.37 22.35 6-4 W5 7,218.80 30,693.16 38,322.19 9,319.65 3,082.73 10,587.50 32.80 6-4 W6 11,420.49 44,982.83 38,322.19 9,319.65 9,264.11 3,082.73 32.80 8-4 V3 11,420.49 44,982.83 38,322.19 9,319.65 2,067.01 3,139.35 22.35 10-4 W7 11,420.49 44,982.83 50,316.43 13,521.34 3,082.73 7,450.57 32.80 10-4 W8 16,453.77 56,142.05 50,316.43 13,521.34 7,202.07 3,723.86 40.27 12-4 V4 16,453.77 56,142.05 50,316.43 13,521.34 2,082.27 3,380.02 22.35 15-11/2 W9 16,453.77 56,142.05 56,683.54 16,405.51 3,087.42 5,614.87 33.54 15-11/2 Continued on Next Page... STRESS ANALYSIS - PAGE 1 �' Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:07:07 PM NEW MILLENNIUM Location: Joist Description: Mark: RI III ^1�17 SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ37 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W9 15,171.67 55,331.25 56,683.54 16,405.51 2,454.55 4,372.23 26.12 17-21/2 V5 15,171.67 55,331.25 56,683.54 16,405.51 2,057.99 2,059.59 22.35 18-4 W8 15,171.67 55,331.25 51,858.50 12,978.18 5,491.20 3,082.73 32.80 18-4 W7 10,784.68 47,272.71 51,858.50 12,978.18 3,082.73 7,450.57 32.80 20-4 V6 10,784.68 47,272.71 51,858.50 12,978.18 2,057.99 2,059.13 22.35 22-4 W6 10,784.68 47,272.71 41,102.85 8,591.19 9,264.11 3,082.73 32.80 22-4 W5 6,397.69 33,530.63 41,102.85 8,591.19 3,082.73 10,587.50 32.80 24-4 V7 6,397.69 33,530.63 41,102.85 8,591.19 2,057.99 2,058.67 22.35 26-4 W4 6,397.69 33,530.63 24,125.80 4,204.20 12,937.77 3,082.73 32.80 26-4 W3 3,107.45 18,667.92 24,125.80 4,204.20 2,427.60 11,796.74 25.37 28-4 V1S 3,107.45 18,667.92 0.00 0.00 2,335.75 5,516.29 25.37 30-4 W2 3,107.45 20,041.62 0.00 0.00 24,091.16 4,035.78 40.69 29-4 STRESS ANALYSIS - PAGE 2 �/� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:07:07 PM NEW MILLENNIUM Location: Joist Description: Mark: 9LI1LO1NC. SVSTEKAS TIGARD,OR Long Span 24LH3441230 TJ37 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.1207 0.8991 0.5436 1.6512 0.8225 0.9058 0.9280 A44A=2.8750 x.209 BC 1.1207 0.8991 0.5436 1.6512 0.8225 0.9058 0.9280 A44A=2.8750 x.209 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Brldg BC: 0.75 50,000.00 30,000.00 563.69 642.67 964.01 22-15/8 21-0 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 33.50 24.00 22.00 1.1250 Min Weld Len 2X: Bending Load 451.00 451.00 451.00 821.55 886.12 0.6049 Axial Load 17,936.18 17,397.66 56,142.05 18,667.92 20,041.62 Max Load Fillers TC: fa 4,372.12 7,761.96 25,047.76 8,328.69 4,885.34 57,038.39 Maximum K Lir 44.15 47.83 30.81 44.15 40.47 Max Load no Fillers TC: Fcr 40,650.88 39,728.11 43,504.19 40,650.88 41,518.74 52,631.07 TC Fa 24,390.53 23,836.86 26,102.51 24,390.53 24,911.25 232.56 yy: 232.56 F'e 839,250.44 342,268.59 366,523.31 401,690.22 998,777.38 BC oALJRyy: Cm 0.9974 0.9887 0.9542 0.9896 0.9976 232.56 Panel Point Moment 16,569.31 2,431.90 3,514.82 5,412.94 5,412.94 BC Stress: Mid Panel Moment 12,386.78 1,712.75 1,757.41 912.68 11,761.04 0.84 Panel Point fb 4,139.46 2,755.29 3,982.21 6,132.73 1,352.30 BcuR7: 105.7763 Mid Panel fb 3,094.55 777.62 797.90 414.37 3,002.77 TC Shear Stress: Fillers 0 0 1 0 0 14,183.41 Panel Point Stress 8,511.58 10,517.25 29,029.97 14,461.42 6,237.64 BC Shear Stress: Mid Panel Stress 0.2015 0.3511 0.9870 0.3550 0.2065 114,183.41 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 20,381.01 24,373.24 5,390.39 10,078.41 7.32 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1S 3,259.00 7,826.93 3,617.79 4,512.11 2.39 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W3 2,427.60 24,373.24 11,796.74 14,277.58 4.24 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 12,937.77 14,381.54 3,082.73 7,478.66 5.81 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 2,067.01 5,758.64 3,089.37 3,741.07 2.31 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 3,082.73 24,373.24 10,587.50 12,020.02 3.80 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 9,264.11 10,742.43 3,082.73 5,746.77 4.84 x 0.129 1 C22BB = 1.125 x 1.110 x.129 V3 2,067.01 5,758.64 3,139.35 3,741.07 2.35 x 0.090 1 C12BB = 1.125 x 0.799 x.090 W7 3,082.73 14,381.54 7,450.57 7,478.66 3.34 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W8 7,202.07 8,984.69 3,723.86 3,860.39 4.11 x 0.118 1 C18BB = 1.125 x 1.035 x.118 V4 2,082.27 5,758.64 3,380.02 3,741.07 2.53 x 0.090 1 C12BB = 1.125 x 0.799 x.090 W9 3,087.42 10,742.43 5,614.87 5,650.69 2.93 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W9 2,454.55 7,826.93 4,372.23 4,539.69 2.89 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V5 2,057.99 4,802.89 2,059.59 3,033.68 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W8 5,491.20 7,826.93 3,082.73 3,868.17 3.63 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 3,082.73 14,381.54 7,450.57 7,478.66 3.34 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V6 2,057.99 4,802.89 2,059.13 3,033.68 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W6 9,264.11 10,742.43 3,082.73 5,746.77 4.84 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 3,082.73 24,373.24 10,587.50 12,020.02 3.80 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... STRESS ANALYSIS -PAGE 2 ,, Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:07:07 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS. TIGARD, OR Long Span 24LH344/230 TJ37 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 2,057.99 4,802.89 2,058.67 3,033.68 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W4 12,937.77 14,381.54 3,082.73 7,478.66 5.81 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 2,427.60 24,373.24 11,796.74 14,277.58 4.24 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1 S 2,335.75 8,984.69 5,516.29 5,530.07 3.15 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W2 24,091.16 24,373.24 4,035.78 10,911.01 8.65 x 0.188 1 C38BA= 1.125 x 1.845 x.199 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:07:07 PM NEW MILLENNIUM Location: Joist Description: Mark: aUILCIINC SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ37 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-3 1/4 BPL Length 2-4 7/8 Clear Bearing 0-9 7/8 Clear Bearing 0-9 1/8 BPL Material:2024=2 x 2 x.248 BPL Material: 2024=2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def L/80 0.00 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L/120 0.00 Section Modulus 3.9167 Section Modulus 3.9167 Reqd SM 0.5523 Reqd SM 0.0000 Mom of Inertia 6.9287 Mom of Inertia 6.9287 Reqd MI 0.5845 Reqd MI 0.0000 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c:DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+A)(+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+A)(+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 �/� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 1:52:12 PM NEW MILLENNIUM Location: Joist Description: Marc: SLELOING SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ39 Geometry Base Length: Working Length: Joist Depth: Effective Depth.. BC Panel Length: Shape. 1 32-4 32-0 24.00 22.73 7 @ 4-0 Parallel Chords 1 Variable Left End Right End BC Panel 3-4 3-0 , u u-c,ntmmmnirmytTri(;liiltfill1 TC Panel 2-2 2-0 x First Half 1-0 1-0 First Diag. 4-4 4-0 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference L' Uniform(plf) LL(1) 230.00 230.00 TC + 0-0 32-4 L-BL Uniform(plf) DL(1) 114.00 114.00 TC + 0-0 32-4 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 17.00 17.00 TC + 0-0 32-4 L-BL Uniform (plf) LL(1) 85.00 85.00 TC + 0-0 32-4 L-BL _Uniform (plf) DL(1) 76.00 76.00 BC + 0-0 32-4 L-BL Uniform (plf) IP(1) 54.00 54.00 TC + 0-0 32-4 L-BL Uniform (plf) SM(1) 19.00 19.00 TC + 0-0 32-4 L-BL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Conc @ any pp(Ibs) WL (1) 400.00 0.00 TC + Uniform (plf) LL(1) 0.00 466.00 TC + 21-9 7/8 33-3 7/8 L-OAL Conc w/bending(Ibs) CL(1) 2,000.00 0.00 TC + 33-10 33-10 L-OAL Gross Uplift(plf) WL(2) 30.00 30.00 TC - 0-0 32-4 L-BL Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 8,681.43 12,832.88 3,208.22 39,482.73 39,489.13 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,734.85 15,045.04 0.00 0.00 15,959.68 2,304.58 44.28 0-2 V1S 1,344.51 14,521.79 0.00 0.00 1,163.61 1,424.01 26.69 2-2 W3 1,344.51 14,521.79 16,898.80 1,557.78 842.46 9,351.97 25.70 3-4 W4 1,934.83 24,220.36 16,898.80 1,557.78 9,750.17 996.20 33.05 4-4 W5 1,934.83 24,220.36 28,811.74 2,403.79 836.22 7,424.36 33.05 6-4 W6 2,831.44 33,408.68 28,811.74 2,403.79 6,127.12 748.97 33.05 8-4 W7 2,831.44 33,408.68 36,355.22 3,195.74 588.99 4,665.72 33.05 10-4 W8 3,496.68 38,553.62 36,355.22 3,195.74 4,665.72 501.73 33.05 12-4 W9 3,496.68 38,553.62 39,489.13 3,699.07 4,650.04 4,665.72 33.05 14-4 W9 3,450.92 39,482.73 39,489.13 3,699.07 4,650.04 4,665.72 33.05 16-4 W8 3,450.92 39,482.73 38,195.66 3,139.42 4,665.72 501.73 33.05 18-4 W7 2,764.57 35,824.41 38,195.66 3,139.42 588.99 4,665.72 33.05 20-4 W6 2,764.57 35,824.41 31,905.69 2,326.35 6,127.12 748.97 33.05 22-4 W5 1,824.79 26,618.24 31,905.69 2,326.35 836.22 7,424.36 33.05 24-4 Continued on Next Page... STRESS ANALYSIS - PAGE 1 G,, Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 1:52:12 PM NEW M I L L E N N I UM Location: Joist Description: Mark: AUILOINtr: .„STFMS TIGARD,OR Long Span 24LH344/230 TJ39 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W4 1,824.79 26,618.24 19,538.87 1,259.86 9,750.17 996.20 33.05 26-4 W3 945.72 16,046.37 19,538.87 1,259.86 842.46 9,351.97 25.70 28-4 V1S 945.72 16,046.37 0.00 0.00 520.73 3,197.04 25.70 30-4 W2 976.08 17,340.68, 0.00 0.00 19,976.52 1,528.34 40.90 29-4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 470.00 1,650.26 22.73 STRESS ANALYSIS - PAGE 2 ,) Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 1:52:12 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING. SYSTEMS TIGARD,OR Long Span 24LH344/230 TJ39 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.8084 0.6885 0.4106 1.3990 0.6554 0.3832 1.0000 A38B=2.2190 x 0.199 BC 0.7132 0.6446 0.3831 1.3432 0.6159 0.2963 1.0000 A36B=2.0780 x 0.188 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 392.85 447.89 671.84 18-9 26-10 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 24.00 26.00 24.00 24.00 22.00 1.1250 Min Weld Len 2X: Bending Load 446.00 446.00 479.69 816.55 881.12 0.5000 Axial Load 15,045.04 14,521.79 39,482.73 16,046.37 17,340.68 Max Load Fillers TC fa 4,326.02 8,981.81 24,420.29 9,924.77 4,986.11 44,490.32 Maximum K L/r 58.45 63.32 43.84 58.45 53.58 Max Load no Fillers TC: Fcr 38,947.56 37,294.54 43,445.47 38,947.56 40,532.97 41,153.20 Fa 23,368.54 22,376.72 26,067.28 23,368.54 24,319.78 TC oauRyy. 274.47 Fe 835,977.38 200,705.34 418,755.59 235,550.02 994,882.19 Bc oAURyy: Cm 0.9974 0.9776 0.9609 0.9789 0.9975 285.89 Panel Point Moment 16,569.29 2,202.36 1,918.75 4,483.96 4,483.97 BC Stress: Mid Panel Moment 12,523.48 1,432.20 959.37 1,234.81 12,200.31 0.92 Panel Point fb 4,640.60 4,493.24 3,914.60 9,148.13 1,255.84 BcuR9 125.2937 Mid Panel fb 3,507.48 1,224.77 820.42 1,055.96 3,881.22 TC Shear Stress: Fillers 0 0 0 0 0 17,124.67 Panel Point Stress 8,966.62 13,475.05 28,334.90 19,072.90 6,241.94 BC Shear Stress: Mid Panel Stress 0.2102 0.4397 0.9627 0.4577 0.3207 19,601.65 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 15,959.68 16,730.22 2,304.58 6,997.47 6.80 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W3 842.46 16,730.22 9,351.97 9,828.81 3.99 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W4 9,750.17 10,742.43 996.20 5,713.48 5.09 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W5 836.22 14,381.54 7,424.36 7,434.44 3.33 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W6 6,127.12 7,826.93 748.97 3,843.58 4.05 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W7 588.99 10,742.43 4,665.72 5,713.48 2.44 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W8 4,665.72 4,802.89 501.73 1,924.39 4.08 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W9 4,650.04 10,742.43 4,665.72 5,713.48 2.44 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W9 4,650.04 10,742.43 4,665.72 5,713.48 2.44 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 4,665.72 4,802.89 501.73 1,924.39 4.08 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W7 588.99 10,742.43 4,665.72 5,713.48 2.44 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W6 6,127.12 7,826.93 748.97 3,843.58 4.05 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 836.22 14,381.54 7,424.36 7,434.44 3.33 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 9,750.17 10,742.43 996.20 5,713.48 5.09 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 842.46 16,730.22 9,351.97 9,828.81 3.99 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W2 19,976.52 24,373.24 1,528.34 10,859.95 7.17 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1 1,163.61 5,758.64 3,197.04 3,394.83 2.39 x 0.090 1 C12BB= 1.125 x 0.799 x.090 V2 470.00 4,802.89 1,650.26 3,007.29 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 1:52:12 PM NEW M I L L E N N I U M Location: Joist Description: Mark: SUILoING SYSTEMS TIGARD,OR Long Span 24LH3441230 TJ39 TCX Design TCX Left TCX Right TCX Length 2-8 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 5-5 BPL Length 2-6 1/2 Clear Bearing 0-10 1/8 Clear Bearing 0-9 BPL Material: 2024=2 x 2 x.248 BPL Material: 2024 =2 x 2 x.248 Total Load 344.00 Total Load 344.00 Reqd TL Def L/120 0.27 Reqd TL Def L/80 0.00 Live Load 230.00 Live Load 230.00 Reqd LL Def L/180 0.18 Reqd LL Def L/120 0.00 Section Modulus 3.1434 Section Modulus 3.1434 Reqd SM 0.5523 Reqd SM 0.0000 Mom of Inertia 5.8509 Mom of Inertia 5.8509 Reqd MI 0.5845 Reqd MI 0.0000 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0,85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 1 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 11:58:34 AM NEW MILLENNIUM Location: Joist Description: Mark: BLIILOINO SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 TJ56 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: ' 81-5 3/4 81-1 3/4 68.00 65.38 9 Special Double Pitch with Ridge @ 40-8 1'' Variable Left End Right End BC Panel 5-8 5-9 3/4 TC Panel 4-0 5-0 1/2 flAr1140u}f First Half 3-0 1-3 �. IDliii'i , ' pj {(t,}lGlf�i(Ill hill[ l[1PR twirit1t[li(Ilfi[SH IN'I 1iillillTlff�iI{ trainiir First Diag. 8-8 7-0 3/4 Depth 47.50 47.50 Loads Load Type Category Load1 Load2 Position Direction Loc./Begin Sp/End Reference Uniform (plf) DL(1) 192.00 192.00 TC + 0-0 81-5 3/4 L-BL Uniform(plf) LL(1) 390.00 390.00 TC + 0-0 81-5 3/4 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) SM (1) 32.00 32.00 TC + 0-0 81-5 3/4 L-BL Axial(ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 128.00 128.00 BC + 0-0 81-5 3/4 L-BL Uniform(plf) DL(1) 74.00 74.00 TC + 0-0 81-5 3/4 L-BL Uniform(plf) IP(1) 90.00 90.00 TC + 0-0 81-5 3/4 L-BL Concw/bending (Ibs) LL(1) 4,000.00 0.00 TC + 10-1 11-2 L-OAL Concw/bending (Ibs) LL(1) 1,000.00 0.00 BC + 11-1 11-1 L-OAL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 13-8 5/8 13-8 5/8 L-OAL Concw/bending(Ibs) LL(1) 5,000.00 0.00 TC + 18-10 1/2 18-10 1/2 L-OAL Concw/bending(Ibs) LL(1) 900.00 0.00 BC + 21-6 21-6 L-OAL Concw/bending(lbs) CL(1) 3,000.00 0.00 TC + 22-0 22-0 L-OAL Concw/bending(Ibs) LL(1) 5,000.00 0.00 TC + 28-0 1/2 28-0 1/2 L-OAL Conc w/bending(Ibs) LL(1) 5,000.00 0.00 TC + 37-2 1/2 37-2 1/2 L-OAL Conc Load (Ibs) LL(1) 1,000.00 0.00 BC + 39-3 39-3 L-OAL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM(1) 400.00 0.00 TC + Concw/bending(Ibs) LL(1) 900.00 0.00 BC + 42-9 1/2 42-9 1/2 L-OAL Concw/bending(ibs) LL (1) 1,000.00 0.00 BC + 46-4 46-4 L-OAL Conc w/bending(Ibs) CL(1) 3,000.00 0.00 TC + 61-5 5/8 61-5 5/8 L-OAL Concw/bending(Ibs) LL (1) 900.00 0.00 BC + 61-9 61-9 L-OAL Conc w/bending(lbs) CL(1) 3,000.00 0.00 TC + 69-1 7/8 69-1 7/8 L-OAL Concw/bending(Ibs) LL (1) 1,000.00 0.00 BC + 72-2 72-2 L-OAL Concw/bending(Ibs) LL (1) 4,000.00 0.00 TC + 75-11 77-0 L-OAL Gross Uplift(plf) WL(2) 60.00 60.00 TC - 0-0 81-5 3/4 L-BL Conc w/bending(Ibs) LL (2) 4,000.00 0.00 TC - 10-1 11-2 L-OAL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC • - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc w/bending(Ibs) LL (2) 4,000.00 0.00 TC - 75-11 77-0 L-OAL • Conc Load(Ibs) LL (3) 1.00 0.00 TC + 10-1 10-1 L-OAL Conc Load(Ibs) LL (3) 1.00 0.00 TC + 11-2 11-2 L-OAL Conc Load(Ibs) LL (3) 1.00 0.00 TC + 75-11 75-11 L-OAL Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 11:58:34 AM NEW NI I L L E N N I U Nt Location: Joist Description: Mark: BUIL-OING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 TJ56 Loads, Continued... Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Conc Load(Ibs) LL(3) 1.00 0.00 TC + 77-0 77-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 81.07 120.00 54,335.87 49,659.12 13,583.97 205,899.09 204,632.08 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 6,684.83 73,365.65 0.00 0.00 88,982.37 8,558.76 79.86 0-2 V1S 6,570.40 72,196.60 0.00 0.00 4,276.36 7,491.11 50.99 4-0 W3 6,570.40 72,196.60 105,937.20 9,694.76 5,787.61 57,711.96 61.01 5-8 W4 12,120.06 151,802.36 105,937.20 9,694.76 63,641.31 6,688.05 77.63 8-8 V2 12,120.06 151,802.36 105,937.20 9,694.76 1,571.91 9,291.36 52.45 13-8 W5 11,835.23 150,031.84 179,960.84 12,531.26 2,311.48 41,859.19 80.92 13-8 W6 12,927.26 197,477.31 179,960.84 12,531.26 24,610.83 1,863.40 80.92 18-8 V3 12,927.26 197,477.31 179,960.84 12,531.26 721.80 6,761.72 56.81 23-8 W7 12,927.26 197,477.31 204,632.08 13,037.21 1,730.09 18,375.00 78.30 23-8 W8 12,998.74 205,899.09 204,632.08 13,037.21 17,713.38 12,537.39 78.30 27-11 1/2 V4 12,998.74 205,899.09 204,632.08 13,037.21 665.22 3,707.63 61.14 32-3 W9 12,998.74 205,899.09 204,532.28 12,860.18 15,861.59 5,642.63 72.26 32-3 W10 12,696.55 201,135.66 204,532.28 12,860.18 1,425.63 15,141.34 70.58 35-3 V5 12,696.55 201,135.66 204,532.28 12,860.18 608.70 4,917.43 64.02 37-11 1/2 W11 12,696.55 201,135.66 194,785.44 12,457.29 15,169.89 1,428.31 73.01 37-11 1/2 W11 12,560.49 196,175.16 194,785.44 12,457.29 15,169.33 9,223.18 73.01 40-8 V6 12,560.49 196,175.16 194,785.44 12,457.29 608.72 3,047.45 64.02 43-41/2 W10 12,560.49 196,175.17 195,281.19 12,578.34 15,141.42 7,064.11 70.59 43-4 1/2 W9 12,547.13 193,510.45 195,281.19 12,578.34 7,399.46 15,860.23 72.27 46-1 V7 12,547.13 193,510.45 195,281.19 12,578.34 665.28 3,648.72 61.15 49-1 W8 12,547.13 193,510.47 187,201.81 12,328.87 17,711.63 1,667.63 78.31 49-1 W7 11,941.32 178,201.94 187,201.81 12,328.87 1,729.67 18,370.53 78.31 53-4 1/2 V8 11,941.32 178,201.94 187,201.81 12,328.87 721.93 5,521.23 56.84 57-8 W6 11,941.32 178,201.95 159,671.91 11,196.50 25,632.85 1,862.83 80.94 57-8 W5 10,139.30 133,860.44 159,671.91 11,196.50 2,264.00 35,870.10 80.94 62-8 V9 10,139.30 133,860.44 159,671.91 11,196.50 784.61 7,575.04 51.82 67-8 W4 10,139.30 133,860.44 80,076.34 8,073.66 63,637.40 3,709.17 94.37 67-8 W3 6,915.83 67,466.02 80,076.34 8,073.66 3,933.89 42,822.14 50.70 74-5 V1S 6,915.83 67,466.02 0.00 0.00 4,289.72 6,886.44 48.31 76-51/4_ W2 7,101.62 68,111.73 0.00 0.00 81,974.77 9,008.59 81.31 75-8 STRESS ANALYSIS - PAGE 2 �/:� Job Number. Job Name: - Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 11:58:34 AM NEW NI I L L E N N I U NI Location: Joist Description: Mark: BUILoING SYSTEMS TIGARD,OR Deep Long Span 68DLH5821390 TJ56 Chord Properties Chord Area _ Rx Rz Ryy Y lx Q Material TC 4.7500 1.5390 0.9829 2.5210 1.4342 11.2503 1.0000 5050=5 x 5 x .500 BC 3.7500 1.2178 0.7823 2.1286 1.1833 5.5615 1.0000 4050=4 x 4 x .500 Axial and Bending Analysis K: Fy: Fb: Morn of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 17,950.36 1,255.09 1,882.64 35-8 5/8 42-6 7/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.04 56.05 81.07 24.27 58.55 1.1250 Min Weld Len 2X: Bending Load _ 655.42 655.42 655.42 655.43 655.43 2.1278 Axial Load 73,365.66 72,196.61 205,899.09 67,466.02 68,111.73_ Max Load Fillers TC: fa 7,722.70 7,599.64 20,787.09 7,101.69 7,169.66 260,615.47 Maximum K Lir 46.84 57.02 39.33 24.69 59.57 Max Load no Fillers TC: Fcr 42,588.92 39,419.50 44,652.59 47,819.73 38,573.34 244,768.86 TC Fa 25,553.35 23,651.70 26,791.55 28,691.84 23,144.00 386.26 yy 86.26 F'e 319,811.19 215,790.95 453,599.22 1,150,777.25 197,743.86 BCOAURyy: Cm 0.9879 0.9824 0.9693 0.9969 0.9819 457.46 Panel Point Moment 9,484.34 28,491.56 45,309.09 31,911.91 19,371.87 BC Stress: Mid Panel Moment 7,520.09 3,245.03 19,579.00 15,451.86 14,347.86 0.91 Panel Pointfb 1,503.04 4,515.22 7,180.39 5,057.26 3,069.97 153.3BC 9 53.3938 Mid Panel f6 479.33 206.84 1,247.98 2,448.74 914.54 TC Shear Stress: Fillers 0 0 0 0 0 11,273.00 Panel Point Stress 9,225.74 12,114.87 27,967.48 _ 12,158.95 10,239.63 BC Shear Stress: Mid Panel Stress 0.3168 0.3277 0.8147 0.3206 0.3381 13,450.64 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 88,982.37 107,333.90 8,558.76 76,707.66 19.14 x 0.313 2 3031 =3 X 3 X.313 V1 S 4,276.36 28,624.38 7,491.11 8,213.89 2.69 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 5,787.61 78,227.12 57,711.96 60,403.51 17.12 x 0.227 2 A48A=3.0625 x.227 W4 63,641.31 67,578.15 6,688.05 44,373.52 20.51 x 0.209 2 A44A=2.8750 x.209 V2 1,571.91 28,624.38 9,291.36 12,383.11 3.34 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W5 2,311.48 67,578.15 41,859.19 43,063.70 15.03 x 0.188 2 A44A=2.8750 x.209 W6 24,610.83 28,624.38 1,863.40 3,891.80 8.84 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 V3 721.80 28,624.38 6,761.72 6,970.75 2.43 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W7 1,730.09 43,005.92 18,375.00 20,041.49 6.60 x 0.188 2 A36B=2.0780 x 0.188 W8 17,713.38 33,466.47 12,537.39 13,754.07 7.55 x 0.158 2 A32B= 1.9060 x 0.158 V4 665.22 16,730.22 3,707.63 3,842.83 2.00 x 0.158 1 C32BA= 1.125 x 1.520 x .158 W9 15,861.59 28,624.38 5,642.63 7,947.34 5.70 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W10 1,425.63 33,466.47 15,141.34 16,197.20 6.45 x 0.158 2 A32B= 1.9060 x 0.158 V5 608.70 24,373.24 4,917.43 5,035.74 2.00 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W11 15,169.89 15,659.90 1,428.31 3,908.18 10.02 x 0.102 2 A16B= 1.3750 x 0.102 W11 15,169.33 28,769.10 9,223.18 11,194.04 6.81 x 0.150 2 A28B= 1.7350 x 0.150 V6 608.72 14,381.54 3,047.45 3,152.68. 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W10 15,141.42 28,624.38 7,064.11 8,241.75 5.44 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W9 7,399.46 37,440.23 15,860.23 17,620.71 6.07 x 0.176 2 A34A= 1.9380 x 0.176 Continued on Next Page... STRESS ANALYSIS - PAGE 2 ,,s Job Number. Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 11:58:34 AM NEW MI L L E N N I U M Location: Joist Description: Mark: PI la[DING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 TJ56 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 665.28 16,730.22 3,648.72 3,841.34 2.00 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 17,711.63 18,714.09 1,667.63 2,849.77 6.78 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W7 1,729.67 43,005.92 18,370.53 20,034.75 6.60 x 0.188 2 A36B=2.0780 x 0.188 V8 721.93 24,373.24 5,521.23 6,078.95 2.00 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 25,632.85 28,624.38 1,862.83 3,889.58 9.21 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W5 2,264.00 61,276.80 35,870.10 36,722.85 12.88 x 0.188 2 A42A=2.6250 x.209 V9 784.61 28,624.38 7,575.04 8,017.73 2.72 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W4 63,637.40 67,578.15 3,709.17 37,610.24 20.51 x 0.209 2 A44A=2.8750 x.209 W3 3,933.89 57,194.49 42,822.14 44,884.41 13.23 x 0.218 2 A40B=2.3750 x 0.218 V1S 4,289.72 24,373.24 6,886.44 7,757.51 2.47 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W2 81,974.77 96,902.01 9,008.59 68,532.91 19.65 x 0.281 2 3028=3 X 3 X.281 STRESS ANALYSIS - PAGE 3 Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 11:58:34 AM NEW MILLENNIUM Location: Joist Description: Mark: aLJILoItir; SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 TJ56 TCX Design TCX Left TCX Right TCX Length 0-11 1/2 TCX Length 0-0 TCX Type S TCX Type R TCX Depth 9 TCX Depth 9 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-10 1/2 Clear Bearing 0-10 5/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 582.00 Total Load 582.00 Reqd TL Def L/80 0.14 Reqd TL Def L/80 0.00 Live Load 390.00 Live Load 390.00 Reqd LL Def L/120 0.10 Reqd LL Def L/120 0.00 Section Modulus 6.3101 Section Modulus 0.0000 Reqd SM 0.1473 Reqd SM 0.0000 Mom of Inertia 22.5006 Mom of Inertia 0.0000 Reqd MI 0.0414 Reqd MI 0.0000 Seat Type:T-Plate 1" Seat Type:T-Plate 1' F Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) + Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX SL) Case 5a:0.6(DL)+WL+AX Case Sc: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:58 PM NEW IV I L L E N N I U 1A Location: Joist Description: Mark: SUILOIMO SYSTEMS 'TIGARD,OR Deep Long Span 68DLH582/390 TJ58 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 81-5 314 81-1 3/4 68.00 65.72 9 Special Double Pitch with Ridge @ 40-8 Variable Left End Right End BC Panel 5-8 5-9 3/4 TC Panel 4-0 4-0 \ V � �\ First Half 3-0 3-0 \' [ i `:��rir�T�i�l��)�r���[ � �� fr�r�� ��,��mll) liihminaTEN,--' First Diag. 8-8 8-9 3/4 Depth 47.50 47.50 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) LL(1) 390.00 390.00 TC + 0-0 81-5 3/4 L-BL Uniform(plf) DL(1) 192.00 192.00 TC + 0-0 81-5 3/4 L-BL Uniform(plf) DL(1) 128.00 128.00 BC + 0-0 81-5 3/4 L-BL Uniform(plf) SM (1) 32.00 32.00 TC + 0-0 81-5 3/4 L-BL Uniform (plf) DL(1) 49.00 49.00 TC + 0-0 81-5 3/4 L-BL Axial (Ibs) SM(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) IP(1) 90.00 90.00 TC + 0-0 81-5 3/4 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Concw/bending (Ibs) LL(1) 1,000.00 0.00 BC + 11-1 11-1 L-OAL Conc w/bending(Ibs) CL(1) 3,000.00 0.00 TC + 13-8 5/8 13-8 5/8 L-OAL Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 24-11 1/2 24-11 1/2 L-OAL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 58-6 1/8 58-6 1/8 L-OAL Concw/bending(Ibs) CL(1) 3,000.00 0.00 TC + 69-1 7/8 69-1 7/8 L-OAL Conc w/bending (Ibs) LL(1) 1,000.00 0.00 BC + 72-2 72-2 L-OAL Gross Uplift(plf) WL(2) 60.00 60.00 TC - 0-0 81-5 3/4 L-BL Conc @ any pp (Ibs) WL(2) 400.00 0.00 TC - Conc @ any pp (Ibs) SM (2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear. Max TC Comp.: Max BC Tension 60.05 120.00 37,112.46 37,055.10 9,278.11 139,924.67 139,317.86 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,461.43 49,712.55 0.00 0.00 59,772.22 4,543.55 80.05 0-2 V1S 3,355.26 48,649.11 0.00 0.00 718.65 3,295.78 51.30 4-0 W3 3,355.26 48,649.11 70,113.76 4,893.83 2,839.00 37,376.21 61.28 5-8 W4 6,936.44 99,817.95 70,113.76 4,893.83 38,435.02 2,915.44 77.84 8-8 V2 6,936.44 99,817.95 70,113.76 4,893.83 731.66 6,251.53 52.11 13-8 W5 6,936.44 99,817.95 118,574.01 8,449.46 2,263.74 25,496.57 81.15 13-8 W6 9,528.04 132,560.56 118,574.01 8,449.46 18,768.30 1,658.29 81.15 18-8 V3 9,528.04 132,560.56 118,574.01 8,449.46 721.54 6,506.95 57.15 23-8 W7 9,528.04 132,560.56 137,428.55 10,123.69 1,064.51 12,517.98 78.55 23-8 W8 10,478.75 139,721.91 137,428.55 10,123.69 12,069.80 856.76 78.55 27-11 1/2 V4 10,478.75 139,721.91 137,428.55 10,123.69 664.96 3,172.61 61.48 32-3 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:58 PM NEW MILLENNIUNI Location: Joist Description: Mark: BLIII-CIING eveTEMS TIGARD, OR Deep Long Span 68DLH582/390 TJ58 Stress Anal sis Summary, Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W9 10,478.75 139,721.91 139,189.97 10,572.14 10,818.54 7,443.80 72.55 32-3 W10 10,583.49 138,049.45 139,189.97 10,572.14 677.63 10,330.59 70.88 35-3 V5 10,583.49 138,049.45 139,189.97 10,572.14 608.45 2,600.66 64.36 37-11 1/2 W11 10,583.49 138,049.45 135,521.05 10,495.75 10,350.70 734.73 73.32 37-11 1/2 W11 10,592.48 138,111.30 135,521.05 10,495.75 10,350.32 734.70 73.32 40-8 V6 10,592.48 138,111.30 135,521.05 10,495.75 608.47 2,600.99 64.36 43-41/2 W10 10,592.48 138,111.31 139,317.86 10,585.09 733.31 10,330.65 70.89 43-4 1/2 W9 10,496.18 139,924.66 139,317.86 10,585.09 10,817.62 7,443.17 72.56 46-1 V7 10,496.18 139,924.66 139,317.86 10,585.09 665.02 3,173.60 61.50 49-1 W8 10,496.18 139,924.67 137,747.73 10,148.17 12,068.63 856.67 78.57 49-1 W7 9,560.25 133,143.73 137,747.73 10,148.17 1,052.94 12,514.97 78.57 53-41/2 V8 9,560.25 133,143.73 137,747.73 10,148.17 721.67 6,662.70 57.18 57-8 W6 9,560.25 133,143.75 119,331.50 8,491.99 18,528.92 1,644.94 81.17 57-8 W5 6,991.05 100,775.84 119,331.50 8,491.99 2,248.20 25,223.00 81.17 62-8 V9 6,991.05 100,775.84 119,331.50 8,491.99 731.90 6,481.16 52.16 67-8 W4 6,991.05 100,775.85 71,039.27 4,962.88 38,483.09 2,898.07 77.88 67-8 W3 3,431.25 49,659.46 71,039.27 4,962.88 2,829.42 37,183.81 61.33 72-8 V1S 3,431.25 49,659.46 0.00 0.00 732.75 3,386.52 52.00 77-5 3/4 W2 3,548.53 50,834.25 0.00 0.00 60,684.70 4,622.31 81.50 75-8 STRESS ANALYSIS - PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:58 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD, OR Deep Long Span 68DLH582/390 TJ58 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 2.8594 1.2346 0.7876 2.1017 1.1383 4.3586 1.0000 4037=4 x 4 x.375 BC 2.8594 1.2346 0.7876 2.1017 1.1383 4.3586 1.0000 4037=4 x 4 x.375 Axial and Bending Analysis K. Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 12,368.80 864.83 1,297.24 29-91/4 42-0 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.04 56.05 60.05 57.80 46.04 1.1250 Min Weld Len 2 : Bending Load 630.44 630.44 630.45 630.45 630.45 1.4346 Axial Load 49,712.55 48,649.11 139,924.67 49,659.46 50,834.25 Max Load Fillers TC: fa 8,692.83 8,506.87 23,281.76 8,683.55 8,888.97 149,271.92 Maximum K L/r 58.46 71.16 38.12 73.39 58.46 Max Load no Fillers TC: Fcr 38,945.64 34,526.46 44,959.08 33,724.54 38,945.77 130,756.91 TC OAL/ Fa 23,367.38 20,715.88 26,975.45 20,234.72 23,367.46 463.3263.32Ryy: F'e 205,811.14 138,870.02 215,062.63 130,582.80 205,813.73 BC DAURyy: Cm 0.9789 0.9694 0.9275 0.9668 0.9784 463.32 Panel Point Moment 11,016.86 20,367.98 15,788.81 18,167.54 13,328.25 BC Stress: Mid Panel Moment 6,202.32 4,938.44 7,894.41 6,192.40 7,930.98 0.81 BC Panel Pointfb 3,616.64 6,686.44 5,183.18 5,964.08 4,375.42 152.36 52.3616 Mid Panel fb 809.90 644.87 1,030.86 808.61 1,035.63 -- TC Shear Stress: Fillers 0 0 2 0 0 12,683.22 Panel Point Stress 12,309.46 15,193.31 28,464.95 14,647.62 13,264.40 BC Shear Stress: Mid Panel Stress 0.3973 0.4313 0.8977 0.4552 0.4128 12,078.72 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 59,772.22 96,902.01 4,543.55 69,266.57. 14.32 x 0.281 2 3028=3 X 3 X.281 V 1 S 718.65 10,742.43 3,295.78 3,448.77 2.00 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 2,839.00 57,194.49 37,376.21 40,139.63 13.42 x 0.188 2 A40B=2.3750 x 0.218 W4 38,435.02 43,005.92 2,915.44 20,219.64 13.80 x 0.188 2 A36B=2.0780 x 0.188 V2 731.66 24,373.24 6,251.53 6,938.67 2.25 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W5 2,263.74 57,194.49 25,496.57 30,740.53 9.16 x 0.188 2 A40B=2.3750 x 0.218 W6 18,768.30 24,373.24 1,658.29 3,381.16 6.74 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V3 721.54 28,624.38 6,506.95 6,906.35 2.34 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W7 1,064.51 33,466.47 12,517.98 13,675.36 5.34 x 0.158 2 A32B= 1.9060 x 0.158 W8 12,069.80 14,381.54 856.76 2,224.79 5.42 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V4 664.96 14,381.54 3,172.61 3,369.57 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W9 10,818.54 28,624.38 7,443.80 7,896.73 3.89 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W10 677.63 28,769.10 10,330.59 11,824.89 4.64 x 0.150 2 A28B= 1.7350 x 0.150 V5 608.45 14,381.54 2,600.66 3,125.49 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W11 10,350.70 15,659.90 734.73 3,875.69 6.83 x 0.102 2 A16B = 1.3750 x 0.102 W11 10,350.32 15,659.90 734.70 3,875.69 6.83 x 0.102 2 A16B= 1.3750 x 0.102 V6 608.47 14,381.54 2,600.99 3,125.09 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W10 733.31 28,769.10 10,330.65 11,822.32 4.64 x 0.150 2 A28B = 1.7350 x 0.150 W9 i 10,817.62 28,624.38 7,443.17 7,895.28 3.89 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 *Continued on Next Page... STRESS ANALYSIS -PAGE 2 �/� Job Number: Job Name: Date Run: vl 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 4:40:58 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILoING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 TJ58 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 665.02 14,381.54 3,173.60 3,368.21 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 12,068.63_ 14,381.54 856.67 2,223.93 5.42 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 1,052.94 33,466.47 12,514.97 13,670.07 5.33 x 0.158 2 A32B= 1.9060 x 0.158 V8 721.67 28,624.38 6,662.70 6,900.60 2.39 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W6 18,528.92 18,714.09 1,644.94 2,675.62 7.09 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W5 2,248.20 57,194.49 25,223.00 30,727.98 9.06 x 0.188 2 A40B=2.3750 x 0.218 V9 731.90 24,373.24 6,481.16 6,929.00 2.33 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 38,483.09 43,005.92 2,898.07 20,205.24 13.82 x 0.188 2 A36B=2.0780 x 0.188 W3 2,829.42 57,194.49 37,183.81 40,117.99 13.36 x 0.188 2 A40B=2.3750 x 0.218 V1S 732.75 14,381.54 3,386.52 4,392.75 2.00 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W2 60,684.70 86,681.16 4,622.31 59,749.65 16.35 x 0.250 2 3025=3 x 3 x.250 STRESS ANALYSIS -PAGE 3 �/� Job Number: Job Name: Date Run: �/� 5618.0007 TIGARD HIGH SCHOOL-SHOPORDERS 1017/2019 4:40:58 PM NEW MILLENNIUM Location: Joist Description: Mark: aLJILoING SYSTFM9 TIGARD, OR Deep Long Span 68DLH582/390 TJ58 TCX Design TCX Left TCX Right TCX Length 0-11 1/2 TCX Length 0-0 TCX Type S TCX Type R TCX Depth 9 TCX Depth 9 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-10 7/8 Clear Bearing 0-11 1/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 582.00 Total Load 582.00 Reqd TL Def L/80 0.14 Reqd TL Def L/80 0.00 Live Load 390.00 Live Load 390.00 Reqd LL Def L/120 0.10 Reqd LL Def L/120 0.00 Section Modulus 3.0462 Section Modulus 0.0000 Reqd SM 0.1473 Reqd SM 0.0000 Mom of Inertia 8.7172 Mom of Inertia 0.0000 Reqd MI 0.0414 Reqd MI 0.0000 Seat Type:T-Plate 1" Seat Type:T-'late r 1 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a:LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 l/� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:31:29 AM NEW MILLENNIUM Location: Joist Description: Mark: RUILOING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 TJ60 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Pane!Length: Shape: 81-5 3/4 81-1 3/4 68.00 65.45 9 Special Double Pitch with Ridge @ 40-8 Variable Left End Right End BC Panel 5-8 5-9 3/4 TC Panel 4-0 5-0 1/2 \ /V i /\ /v ;` 1 - ' First Half 3-0 1-3 1 ; r .i First Diag. 8-8 7-0 3/4 Depth 47.50 47.50 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference,! Uniform (plf) LL(1) 390.00 390.00 TC + 0-0 81-5 3/4 L-BL Uniform (plf) DL(1) 192.00 192.00 TC + 0-0 81-5 3/4 L-BL Uniform (plf) IP(1) 90.00 90.00 TC + 0-0 81-5 3/4 L-BL Uniform (plf) SM(1) 32.00 32.00 TC + 0-0 81-5 3/4 L-BL Uniform (plf) DL(1) 62.00 62.00 TC + 0-0 81-5 3/4 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 128.00 128.00 BC + 0-0 81-5 3/4 L-BL Axial(Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Concw/bending(Ibs) LL(1) 4,000.00 0.00 TC + 9-1 1/2 10-2 1/2 L-OAL Concw/bending(Ibs) LL(1) 1,000.00 0.00 BC + 10-1 1/2 10-1 1/2 L-OAL Conc Load(Ibs) LL(1) 1.00 0.00 TC + 10-8 10-8 L-OAL Concw/bending(Ibs) CL(1) 3,000.00 0.00 TC + 12-9 1/8 12-9 1/8 L-OAL Concw/bending(Ibs) LL (1) 1,000.00 0.00 BC + 20-6 1/2 20-6 1/2 L-OAL Concw/bending(Ibs) CL(1) 3,000.00 0.00 TC + 21-0 3/4 21-0 3/4 L-OAL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Concw/bending (Ibs) LL(1) 1,000.00 0.00 BC + 41-10 41-10 L-OAL Concw/bending(Ibs) CL(1) 3,000.00 0.00 TC + 60-6 3/8 60-6 3/8 L-OAL Concw/bending(Ibs) LL(1) 1,000.00 0.00 BC + 60-9 1/2 60-9 1/2 L-OAL Conc w/bending(Ibs) CL(1) 3,000.00 0.00 TC + 68-2 5/8 68-2 5/8 L-OAL Concw/bending(Ibs) LL(1) 1,000.00 0.00 BC + 71-2 1/2 71-2 1/2 L-OAL Concw/bending(Ibs) LL(1) 4,000.00 0.00 TC + 74-11 1/2 76-0 1/2 L-OAL Gross Uplift(plf) WL(2) 60.00 60.00 TC - 0-0 81-5 3/4 L-BL Conc w/bending (Ibs) LL(2) 4,000.00 0.00 TC - 9-1 1/2 10-2 1/2 L-OAL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Conc w/bending(Ibs) LL(2) 4,000.00 0.00 TC - 74-11 1/2 76-0 1/2 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 96.08 120.00 42,994.41 43,323.28 10,830.82 154,421.09 153,747.00 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 6,567.88 57,628.70 0.00 0.00 69,989.52 8,420.47 79.90 0-2 V1S 6,487.80 56,482.66 0.00 0.00 4,172.25 7,356.56 51.05 4-0 W3 6,487.80 56,482.66 82,450.95 9,613.29 5,784.93 44,546.13 61.06 5-8 *Continued on Next Page... STRESS ANALYSIS -PAGE 1 (0. Job Number:5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:31:29 AM NEW MI L L E N NI UM Location: Joist Description: Mark: 61_I11_01NC. SYSTEMS TIGARD, OR Deep Long Span 68DLH582/390 TJ60 Stress Analysis Summary, Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W4 13,468.51 119,000.05 82,450.95 9,613.29 49,273.20 6,753.75 77.67 8-8 V2 13,468.51 119,000.05 82,450.95 9,613.29 3,734.79 10,763.81 61.88 13-8 W5 11,704.78 113,078.66 134,683.44 12,462.35 2,408.50 30,592.60 80.96 13-8 W6 12,864.95 147,702.34 134,683.44 12,462.35 18,602.55 1,860.78 80.96 18-8 V3 12,864.95 147,702.34 134,683.44 12,462.35 721.75 5,450.22 56.88 23-8 W7 12,864.95 147,702.34 152,257.00 12,980.47 2,261.82 14,643.26 78.35 23-8 W8 12,947.27 154,421.09 152,257.00 12,980.47 14,116.60 2,180.47 78.35 27-11 1/2 V4 12,947.27 154,421.09 152,257.00 12,980.47 665.17 3,406.53 61.21 32-3 W9 12,947.27 154,421.09 153,747.00 12,812.34 12,643.28 8,467.03 72.32 32-3 W10 12,651.83 152,485.20 153,747.00 12,812.34 1,876.83 12,069.93 70.64 35-3 V5 12,651.83 152,485.20 153,747.00 12,812.34 608.65 2,795.57 64.08 37-11 1/2 W 11 12,651.83 152,485.20 149,652.05 12,415.69 12,092.84 1,426.95 73.07 37-11 1/2 W11 12,519.83 152,566.86 149,652.05 12,415.69 12,092.39 1,426.89 73.07 40-8 V6 12,519.83 152,566.86 149,652.05 12,415.69 608.67 2,796.93 64.09 43-41/2 W10 12,519.83 152,566.89 153,692.36 12,538.80 1,876.84 12,070.00 70.65 43-4 1/2 W9 12,508.90 154,206.13 153,692.36 12,538.80 12,642.20 8,466.30 72.33 46-1 V7 12,508.90 154,206.13 153,692.36 12,538.80 665.23 3,408.48 61.22 49-1 W8 12,508.90 154,206.13 151,802.33 12,292.88 14,115.22 1,665.58 78.37 49-1 W7 11,907.91 146,989.00 151,802.33 12,292.88 1,727.47 14,639.71 78.37 53-4 1/2 V8 11,907.91 146,989.00 151,802.33 12,292.88 721.88 5,296.95 56.91 57-8 W6 11,907.91 146,989.02 133,825.77 11,166.74 18,438.27 1,860.21 80.99 57-8 W5 10,113.92 113,918.07 133,825.77 11,166.74 2,257.84 27,895.97 80.99 62-8 V9 10,113.92 113,918.07 133,825.77 11,166.74 784.57 7,395.62 51.89 67-8 W4 10,113.92 113,918.07 69,224.80 8,055.84 53,083.20 3,706.08 94.41 67-8 W3 6,900.62 58,445.33 69,224.80 8,055.84 3,930.04 36,653.77 50.76 74-5 V1S 6,900.62 58,445.33 0.00 0.00 4,289.52 6,799.22 48.38 76-51/4 W2 7,086.14 59,082.13 0.00 0.00 71,178.75 8,993.20 81.35 75-8 STRESS ANALYSIS - PAGE 2 0 Job Number Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:31:29 AM NEW MILLENNIUM Location: Joist Description: Mark: 9LlIlOING SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 TJ60 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 4.1882 1.5476 0.9861 2.5085 1.4117 10.0307 0.9798 5043=5 X 5 X.438 BC 2.8594 1.2346 0.7876 2.1017 1.1383 4.3586 1.0000 4037=4 x 4 x.375 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC; 0.75 50,000.00 30,000.00 14,587.07 1,019.93 1,529.89 35-6 1/2 42-0 3(8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.04 56.05 96.08 24.27 58.55 1.1250 Min Weld Len 2X: Bending Load 643.43 643.43 643.43 643.44 643.44 1.2184 Axial Load 57,628.71 56,482.66 154,421.09 58,445.34 59,082.14 Max Load Fillers TC: fa 6,879.89 6,743.07 13,499.67 6,977.38 7,053.40 185,195.27 Maximum K L/r 46.69 56.84 73.08 24.61 59.38 Max Load no Fillers TC: Fcr 41,905.18 38,866.49 33,414.43 46,907.30 38,054.15 150,180.50 TC Fa 25,143.11 23,319.89 20,048.66 28,144.38 22,832.49 388.18 yy: 88.18 F'e 323,395.41 218,209.39 132,003.20 1,163,674.38 199,960.03 BCCAL/Ryy: Cm 0.9894 0.9845 0.9315 0.9970 0.9824 463.32 Panel Point Moment 16,163.68 16,163.75 82,263.81 31,647.93 19,086.31 BC Stress: Mid Panel Moment 7,241.01 9,688.77 42,074.20 15,225.15 14,062.47 0.90 Panel Point fb 2,891.13 2,891.14 14,714.19 5,660.73 3,413.89 BC uRz: 152.3616 Mid Panel fb 509.54 681.79 2,960.72 2,723.26 989.56 TC Shear Stress: Fillers 0 0 0 0 0 10,153.48 Panel Point Stress 9,771.02 9,634.22 28,213.86 12,638.12 10,467.29 BC Shear Stress: Mid Panel Stress 0.2894 0.3106 0.7739 0.3309 0.3402 14,119.68 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty , Material W2 69,989.52 71,606.18 8,420.47 43,268.26 18.85 x 0.250 2 A46A=2.5938 x.250 V1S 4,172.25 28,624.38 7,356.56 8,199.08 2.64 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W3 5,784.93 61,276.80 44,546.13 45,095.57 14.35 x 0.209 2 A42A=2.6250 x.209 W4 49,273.20 57,194.49 6,753.75 32,384.23 15.22 x 0.218 2 A40B=2.3750 x 0.218 V2 _ 3,734.79 28,597.25 10,763.81 11,335.85 3.87 x 0.188 1 A40B=2.3750 x 0.218 W5 2,408.50 57,194.49 30,592.60 30,827.02 10.99 x 0.188 2 A40B=2.3750 x 0.218 W6 18,602.55 18,714.09 1,860.78 2,687.91 7.12 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V3 721.75 24,373.24 5,450.22 6,072.84 2.00 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W7 2,261.82 37,440.23 14,643.26 15,438.98 5.60 x 0.176 2 A34A= 1.9380 x 0.176 W8 14,116.60 14,381.54 2,180.47 2,235.05 6.34 x 0.150 1 C28BB= 1.125 x 1.344 x .150 V4 665.17 16,730.22 3,406.53 3,836.18 2.00 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W9 12,643.28 28,597.25 8,467.03 9,206.93 4.54 x 0.188 1 A40B=2.3750 x 0.218 W10 1,876.83 31,392.15 12,069.93 13,797.48 5.14 x 0.158 2 A30B= 1.7970 x 0.158 V5 608.65 14,381.54 2,795.57 3,147.58 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W11 12,092.84 15,659.90 1,426.95 3,901.72 7.98 x 0.102 2 A16B= 1.3750 x 0.102 W11 12,092.39 15,659.90 1,426.89 3,901.72 7.98 x 0.102 2 A16B= 1.3750 x 0.102 V6 608.67 14,381.54 2,796.93 3,147.19 2.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W10 1,876.84 31,392.15 12,070.00 13,794.70 5.14 x 0.158 2 A30B= 1.7970 x 0.158 W9 12,642.20 28,597.25 8,466.30 9,205.26 4.54 x 0.188 1 A40B=2.3750 x 0.218 Continued on Next Page... STRESS ANALYSIS - PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:31:29 AM NEW MILLENNIUM Location: Joist Description: Mark: aLM_1711�0 SYSTEMS TIGARD,OR Deep Long Span 68DLH582/390 TJ60 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 665.23 16,730.22 3,408.48 3,834.69 2.00 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 14,115.22 14,381.54 1,665.58 2,234.19 6.34 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 1,727.47 37,440.23 14,639.71 15,432.96 5.60 x 0.176 2 A34A= 1.9380 x 0.176 V8 721.88 24,373.24 5,296.95 6,067.78 2.00 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 18,438.27 18,714.09 1,860.21 2,686.36 7.06 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W5 2,257.84 57,194.49 27,895.97 30,814.50 10.02 x 0.188 2 A40B=2.3750 x 0.218 V9 784.57 28,624.38 7,395.62 8,002.15 2.66 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W4 53,083.20 57,194.49 3,706.08 24,681.55 19.07 x 0.188 2 A408=2.3750 x 0.218 W3 3,930.04 48,746.47 36,653.77 36,863.64 13.16 x 0.188 2 A38B=2.2190 x 0.199 V1S 4,289.52 24,373.24 6,799.22 7,742.13 2.44 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 71,178.75 71,606.18 8,993.20 42,476.53 19.17 x 0.250 2 A46A=2.5938 x.250 STRESS ANALYSIS -PAGE 3 l/� Job Number: Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/8/2019 9:31:29 AM NEW MILLENNIUM Location: Joist Description: Mark: BWLOINO SYSTFMIS TIGARD,OR Deep Long Span 68DLH582/390 TJ60 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 0-0 TCX Type R TCX Type R TCX Depth 9 TCX Depth 9 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-11 Clear Bearing 0-11 5/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x .248 Total Load 582.00 Total Load 582.00 Reqd TL Def L/80 0.00 Reqd TL Def L/80 0.00 Live Load 390.00 Live Load 390.00 Reqd LL Def L/120 0.00 Reqd LL Def LJ120 0.00 Section Modulus 0.0000 Section Modulus 0.0000 Reqd SM 0.0000 Reqd SM 0.0000 Mom of Inertia 0.0000 Mom of Inertia 0.0000 Reqd MI 0.0000 Reqd MI 0.0000 Seat T pe.LPI_t9-4 Seat Type'. -PisWi Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) ' Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 Job Number Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:44:47 PM NEW NI I L L E N N I U NI Location: Joist Description: Mark: 9LI1L01E1G SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ63 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 41-8 5/8 41.4 5/8 24.00 22.29 9 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-11 3/4 2-8 1/8 uurliiuu ffffiiiiiuuiiiii guiirxuuiir ,µu�uiuiiii H[J TC Panel 2-6 2-8 1/8 � ii � � First Half 1-6 1-6 3/4 .. First Diag. 5-5 3/4 4-2 7/8 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) DL(1) 126.00 126.00 TC + 0-0 41-8 5/8 L-BL Uniform(plt) LL(1) 260.00 260.00 TC + 0-0 41-8 5/8 L-BL Uniform(plf) LL(1) 95.00 95.00 TC + 0-0 41-8 5/8 L-BL Uniform(plt) SM (1) 21.00 21.00 TC + 0-0 41-8 5/8 L-BL Uniform(pit) DL(1) 36.00 36.00 TC + 0-0 41-8 5/8 L-BL Uniform (plf) IP(1) 60.00 60.00 TC + 0-0 41-8 5/8 L-BL Uniform (plf) DL(1) 84.00 84.00 BC + 0-0 41-8 5/8 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc Load (Ibs) LL(1) 4,000.00 0.00 TC + 37-7 3/4 38-8 3/4 L-OAL Uniform(plf) LL(1) 0.00 130.00 TC + 38-9 1/2 41-8 5/8 L-OAL Conc @ any pp(Ibs) SM (2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 41-8 5/8 L-BL Conc Load(Ibs) LL (2) 4,000.00 0.00 TC - 37-7 3/4 38-8 3/4 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 12,522.99 16,457.66 4,114.42 72,767.05 73,300.53 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 2,454.84 25,042.49 0.00 0.00 27,211.82 3,087.10 50.89 0-2 V1S 2,397.74 24,041.58 0.00 0.00 640.75 2,372.90 28.50 2-6 W3 2,397.74 24,041.58 31,728.69 3,305.67 1,596.79 13,366.35 28.65 3-11 3/4 W4 4,443.88 41,524.99 31,728.69 3,305.67 14,273.60 1,726.72 32.76 5-5 3/4 W5 4,443.88 41,524.99 49,868.99 5,523.95 1,607.30 12,287.57 32.76 7-5 3/4 W6 6,545.89 57,099.80 49,868.99 5,523.95 10,768.25 1,527.96 32.76 9-5 3/4 W7 6,545.89 57,099.80 62,855.70 7,509.69 1,422.68 8,755.22 32.76 11-5 3/4 W8 8,415.36 67,498.42 62,855.70 7,509.69 7,235.90 1,422.68 32.76 13-5 3/4 W9 8,415.36 67,498.42 70,666.23 9,262.89 1,422.68 6,045.57 32.76 15-53/4 W10 10,052.29 72,720.83 70,666.23 9,262.89 6,045.57 1,422.68 32.76 17-5 3/4 W11 10,052.29 72,720.83 73,300.53 10,683.46 6,045.57 6,045.57 32.76 19-5 3/4 W11 11,033.62 72,767.05 73,300.53 10,683.46 6,045.57 6,045.57 32.76 21-5 3/4 W10 11,033.62 72,767.05 70,758.64 11,325.63 6,045.57 1,422.68 32.76 23-5 3/4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 �/� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:44:47 PM NEW IVI I L L E N N I U PA Location: Joist Description: Mark: al111_17/ING SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ63 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W9 11,559.52 67,637.06 70,758.64 11,325.63 1,422.68 6,045.57 32.76 25-5 3/4 W8 11,559.52 67,637.06 63,040.55 11,735.26 7,235.90 1,422.68 32.76 27-5 3/4 W7 11,852.87 57,330.87 63,040.55 11,735.26 1,422.68 8,755.22 32.76 29-5 3/4 W6 11,852.87 57,330.87 50,146.27 11,912.35 10,768.25 1,527.96 32.76 31-5 3/4 W5 12,450.13 41,848.48 50,146.27 11,912.35 1,607.30 12,287.57 32.76 33-5 3/4 W4 12,450.13 41,848.48 32,095.56 13,155.27 14,273.60 1,726.72 32.76 35-5 3/4 W3 10,700.70 20,727.56 32,095.56 13,155.27 4,175.87 18,085.21 29.13 37-5 3/4 W2 10,700.70 20,727.56 0.00 0.00 25,877.62 13,453.23 37.48 39-01/2 Standard Verticals Member Position Max Tension Max Comp. Length V1 End Panel 8,309.09 4,955.24 28.50 V2 Interior 492.65 1,768.49 22.29 STRESS ANALYSIS - PAGE 2 0 Job Number:5618-0007 Job Name. Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:44:47 PM NEW MILLENNIUM Location: Joist Description: Mark: 6WLDING SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ63 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 BC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 804.14 423.83 635.74 22-01/4 28-91/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 35.75 24.00 18.75 30.13 1.1250 Bending Load 517.00 517.00 517.00 541.94 606.94 Min Weld Len 2X:0.7841 Axial Load 25,042.49 24,041.58 72,767.05 20,727.56 20,727.56 Max Load Fillers TC: fa 4,934.48 7,480.27 22,640.65 6,449.15 3,708.64 92,994.17 Maximum K L/r 47.40 60.52 30.47 31.74 51.00 Max Load no Fillers TC: Fcr 42,424.94 38,252.39 46,717.98 46,448.93 41,340.96 89,552.73 Fa 25,454.96 22,951.43 28,030.79 27,869.36 24,804.58 TC OAURyy: 293.51 F'e 606,108.69 192,029.36 757,486.25 698,099.25 1,228,203.13 BCOAL/Ryy: Cm 0.9959 0.9805 0.9800 0.9954 0.9985 293.51 Panel Point Moment 4,922.50 4,922.50 2,068.00 10,954.69 137,779.89 BC Stress: Mid Panel Moment 2,112.21 2,640.66 1,034.00 9,458.14 109,803.27 0.76 Panel Point fb 1,105.76 3,833.69 1,610.58 3,392.93 16,421.38 BcuR9: 81.2595 Mid Panel fb 402.93 817.88 320.25 2,929.41 13,086.97 TC Shear Stress: Fillers 0 0 0 0 0 9,686.58 Panel Point Stress 6,040.24 11,313.96 24,251.23 9,842.08 20,130.02 BC Shear Stress: Mid Panel Stress 0.1105 0.3513 0.8175 0.3192 0.5125 9,686.58 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 27,211.82 28,624.38 3,087.10 9,686.23 9.77 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 1,596.79 28,624.38 13,366.35 15,354.71 4.80 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 14,273.60 14,381.54 1,726.72 7,485.99 6.41 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,607.30 28,624.38 12,287.57 13,902.98 4.41 x 0.188 1 C40BA= 1.125 x 2.014 x .218 W6 10,768.25 14,381.54 1,527.96 7,485.99 4.83 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W7 1,422.68 18,714.09 8,755.22 9,629.22 3.35 x 0.176 1 C34AA= 1.125 x 1.549 x .176 W8 7,235.90 7,826.93 1,422.68 3,872.25 4.78 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 1,422.68 14,381.54 6,045.57 7,485.99 2.71 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W10 6,045.57 7,826.93 1,422.68 3,872.25 3.99 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W11 6,045.57 14,381.54 6,045.57 7,485.99 2.71 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W11 6,045.57 14,381.54 6,045.57 7,485.99 2.71 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W10 6,045.57 7,826.93 1,422.68 3,872.25 3.99 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 1,422.68 14,381.54 6,045.57 7,485.99 2.71 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 7,235.90 7,826.93 1,422.68 3,872.25 4.78 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W7 1,422.68 18,714.09 8,755.22 9,629.22 3.35 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 10,768.25 14,381.54 1,527.96 7,485.99 4.83 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,607.30 28,624.38 12,287.57 13,902.98 4.41 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W4 14,273.60 14,381.54 1,726.72 7,485.99 6.41 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 4,175.87 28,624.38 18,085.21 18,623.92 6.50 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 0 Job Number: 5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:44:47 PM NEW Nil LLENNIUNt Location: Joist Description: Mark: BUILoING SYSTEMS TIGARD,OR Long Span 24LH3861260 TJ63 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp _ Weld Qty Material W2 25,877.62 29,969.07 13,453.23 19,693.05 5.03 x 0.245 1 WR11A20B=Wrapped R112 with P V1 8,309.09 14,381.54 4,955.24 9,361.40 3.73 x 0.150 1 C28BB = 1.125 x 1.344 x.150 V2 492.65 4,802.89 1,768.49 3,038.10 2.00 x 0.077 1 C10AB = 1.125 x 0.756 x.077 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:44:47 PM NEW MILLENNIUM Location: Joist Description: Mark: a� ti� s�srFMs TIGARD,OR Long Span 24LH386/260 TJ63 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 9-7 5/8 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 5 BPL Length 3-2 BPL Length 12-7 1/2 Clear Bearing 0-11 1/8 Clear Bearing 10-2 3/4 BPL Material:2024 =2 x 2 x.248 BPL Material:302025=3 x 2 x .250 Total Load 386.00 Total Load 956.00 Reqd TL Def L/80 0.00 Reqd TL Def L/120 0.96 Live Load 260.00 Live Load 830.00 Reqd LL Def L/120 0.00 Reqd LL Def L/180 0.64 Section Modulus 4.4517 Section Modulus 8.3903 Reqd SM 0.0000 Reqd SM 4.5927 Mom of Inertia 8.4257 Mom of Inertia 21.7651 Reqd MI 0.0000 Reqd MI 9.0972 Seat Type:Bird Cage(Reinforced) Seat Type:Pegged or Butted(Reinforced) l I Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c:DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 6, Job Number. Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:17:48 PM NEW M I L L E N N I U Nt Location: Joist Description: Mark: 6WloING SYSTEM% TIGARD,OR Long Span 24LH386/260 TJ65 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: ' 41-8 518 41-4 5/8 24.00 22.30 9©4-0 Parallel Chords ;' Variable Left End Right End I' BC Panel 3-11 3/4 2-2 7/8 TC Panel 2-6 2-2 7/8 ram, /. �1�i rrrrarrrrnr rmu> 3 nun i�i annr cur First Half 1-6 _2-0 �,\ � First Diag. 5-5 3/4 4-2 7/8 Depth 24.00 24.00 Loads Load Type Category Load1 I Load2 I Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 260.00 260.00 TC + 0-0 41-8 5/8 L-BL Uniform (plf) DL(1) 126.00_ 126.00 TC + 0-0 41-8 5/8 L-BL Uniform(plf) DL(1) 84.00_ 84.00 BC + 0-0 41-8 5/8 L-BL Uniform(plf) SM(1) 21.00 21.00 TC + 0-0 41-8 5/8 L-BL Uniform (plf) DL(1) 32.00 32.00 TC + 0-0 41-8 5/8 L-BL Uniform (plf) IP(1) 60.00 60.00 TC + 0-0 41-8 5/8 L-BL Axial(Ibs) SM(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) LL(1) 95.00_ 95.00 TC + 0-0 41-8 5/8 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp (Ibs) WL(1) 400.00 0.00 TC + Conc @ any pp (Ibs) SM(1) 400.00 0.00 TC + Uniform(plf) LL(1) 0.00 130.00 TC + 38-9 1/2 41-8 5/8 L-OAL Gross Uplift(plf) WL(2) 36.00_ 36.00 TC - 0-0 41-8 5/8 L-BL Conc @ any pp (Ibs) SM(2) 400.00 0.00 TC - Conc @ any pp (Ibs) WL(2) 400.00 0.00 TC - Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 12,051.83 12,703.06 3,175.77 68,324.77 68,498.56 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,872.79, 24,294.32 0.00 0.00 26,136.26 2,505.82 50.90 0-2 V1S 1,815.71 23,302.38 0.00 0.00 640.63 2,096.32 28.50 2-6 W3 1,815.71 23,302.38 30,433.50 2,494.67 1,222.78. 12,777.90 28.66 3-11 3/4 W4 3,327.62 39,759.03 30,433.50 2,494.67 14,201.84 1,353.07 32.76 5-5 3/4 W5 3,327.62 39,759.03 47,641.56 4,102.45 1,190.32 12,201.11 32.76 7-5 3/4 W6 4,819.19 54,420.10 47,641.56 4,102.45 10,693.95 1,097.31 32.76 9-53/4 W7 4,819.19 54,420.10 59,733.07 5,477.81 975.25 8,693.22 32.76 11-5 3/4 W8 6,078.33 63,942.02 59,733.07 5,477.81 7,186.06 895.92 32.76 13-5 3/4 W9 6,078.33 63,942.02 66,685.40 6,620.75 773.87 5,185.33 32.76 15-5 3/4 W10 7,105.06 68,324.77 66,685.40 6,620.75 4,665.09 694.54 32.76 17-5 3/4 W11 7,105.06 68,324.77 68,498.56 7,431.22 4,665.09 4,665.09 32.76 19-5 3/4 W11 7,476.50 67,568.34 68,498.56 7,431.22_ 4,665.09 4,665.09 32.76 21-5 3/4 W10 7,476.50 67,568.34 65,172.55 7,463.68 4,665.09 694.54 32.76 23-53/4 W9 7,392.75 61,672.75 65,172.55 7,463.68 773.87 5,185.33 32.76 25-53/4 W8 7,392.75 61,672.75 56,707.37 7,263.71 7,186.06 895.92 32.76 27-5 3/4 *Continued on Next Page... STRESS ANALYSIS -PAGE 1 , Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:17:48 PM NEW MI L LE N NI UM Location: Joist Description: Mark: BUILoItiG SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ65 Stress Analysis Summary, Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W7 7,076.57 50,637.98 56,707.37 7,263.71 975.25 8,693.22 32.76 29-5 3/4 W6 7,076.57 50,637.98 43,103.04 6,831.32 10,693.95 1,097.31 32.76 31-5 3/4 W5 6,527.97 34,641.59 43,103.04 6,831.32 1,190.32 12,201.11 32.76 33-5 3/4 W4 6,527.97 34,641.59 24,359.53 6,166.51 14,201.84 1,353.07 32.76 35-5 3/4 W3 5,867.95 14,553.24 24,359.53 6,166.51 1,458.83 15,732.45 32.76 37-53/4 W2 5,867.95 14,553.24 0.00 0.00 17,640.26 7,940.80 33.41 39-5 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V1 End Panel 5,568.23 2,096.32 28.50 ' V2 Interior 492.64 1,566.18 22.30 I STRESS ANALYSIS -PAGE 2 l' Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:17:48 PM NEW MILLENNIUM Location: Joist Description: Mark: SIJIL01NC SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ65 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 BC 1.4375 0.9304 0.5924 1.6850 0.8424 1.2442 0.9613 3025=3 x 3 x.250 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 760.17 400.65 600.98 22-0 1/4 33-8 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 35.75 24.00 24.00 24.88 1.1250 Min Weld Bending Load 513.00 513.00 513.00 544.92 609.92 0.7362 Len 2X: Axial Load 24,294.32 23,302.38 68,324.77 14,553.24 14,553.24 Max Load Fillers TC: fa 4,787.06 7,250.27 21,258.49 4,528.08 2,603.91 93,002.12 Maximum K Ur 47.40 60.52 30.47 40.63 42.11 Max Load no Fillers TC: Fcr 42,424.94 38,252.39 46,717.98 44,314.97 43,919.62 89,560.38 Fa 25,454.96 22,951.43 28,030.79 26,588.98 26,351.77 TC OAL/Ryy: 293.51 Fe 606,108.69 192,029.36 757,486.25 426,085.97 1,801,350.13 BCOAURyy: Cm 0.9961 0.9811 0.9812 0.9947 0.9993 294.73 Panel Point Moment 4,884.41 4,884.41 2,052.00 6,631.92 137,779.89 BC Stress: Mid Panel Moment 2,095.87 2,620.23 1,026.00 6,594.15 111,527.25 0.79 Panel Point fb 1,097.20 3,804.03 1,598.12 2,054.07 16,421.38 81.026263 Mid Panel fb 399.82 811.55 317.78 2,042.37 13,292.45 TC Shear Stress: Fillers 0 0 0 0 0 7,713.96 Panel Point Stress 5,884.26 11,054.30 22,856.60 6,582.15 19,025.29 BC Shear Stress: Mid Panel Stress 0.1075 0.3411 0.7681 0.1541 0.4932 8,659.97 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 26,136.26 28,624.38 2,505.82 9,684.94 9.39 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 1,222.78 24,373.24 12,777.90 13,257.67 4.59 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 14,201.84 14,381.54 1,353.07 7,484.67 6.38 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,190.32 28,624.38 12,201.11 13,900.33 4.38 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W6 10,693.95 10,742.43 1,097.31 5,751.29 5.58 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 975.25 18,714.09 8,693.22 9,627.49 3.33 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 7,186.06 7,826.93 895.92 3,871.51 4.74 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 773.87 10,742.43 5,185.33 5,751.29 2.71 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 4,665.09 4,802.89 694.54 1,953.48 4.08 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W11 4,665.09 8,984.69 4,665.09 4,686.85 2.66 x 0.118 1 C18BB= 1.125 x 1.035 x .118 W11 4,665.09 8,984.69 4,665.09 4,686.85 2.66 x 0.118 1 C18BB= 1.125 x 1.035 x .118 W10 4,665.09 4,802.89 694.54 1,953.48 4.08 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 773.87 10,742.43 5,185.33 5,751.29 2.71 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 7,186.06 7,826.93 895.92 3,871.51 4.74 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 975.25 18,714.09 8,693.22 9,627.49 3.33 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 10,693.95 10,742.43 1,097.31 5,751.29 5.58 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 1,190.32 28,624.38 12,201.11 13,900.33 4.38 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 14,201.84 14,381.54 1,353.07 7,484.67 6.38 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 1,458.83 28,624.38 15,732.45 17,591.44 5.65 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 / Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:17:48 PM NEW M I L LE N N I UM Location: Joist Description: Mark: BU1LO1NG SV5TEM9 TIGARD, OR Long Span 24LH386/260 TJ65 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 17,640.26 18,714.09 7,940.80 10,193.25 6.75 x 0.176 1 C34AA= 1.125 x 1.549 x .176 V1 5,568.23 14,381.54 2,096.32 9,359.28 3.23 x 0.150 1 C28BB= 1.125 x 1.344 x .150 V2 492.64 4,802.89 1,566.18 3,037.30 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 STRESS ANALYSIS - PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:17:48 PM NEW MILLENNIUM Location: Joist Description: Mark: BLnLO1N6 SYSTEMS TIGARD,OR Long Span 24LH3861260 TJ65 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 9-7 5/8 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 5 BPL Length 3-2 BPL Length 12-2 1/4 Clear Bearing 0-11 1/8 Clear Bearing 10-1 5/8 BPL Material:2024=2 x 2 x.248 BPL Material:302025=3 x 2 x.250 Total Load 386.00 Total Load 956.00 Reqd TL Def L/80 0.00 Reqd TL Def L/120 0.96 Live Load 260.00 Live Load 830.00 Reqd LL Def L/120 0.00 Reqd LL Def L/180 0.64 Section Modulus 4.4517 Section Modulus 8.3903 Reqd SM 0.0000 Reqd SM 4.5927 Mom of Inertia 8.4257 Mom of Inertia 21.7651 Reqd MI 0.0000 Reqd MI 9.0972 Seat Type:Bird Cage(Reinforced) Seat Type:Pegged or Butted(Reinforced) ,nI Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:18:23 PM NEW MILLENNIUM Location: Joist Description: Mark: SUILoING SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ67 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 41-8 5/8 41-4 5/8 24.00 22.30 9 @ 4-0 Parallel Chords Variable Left End Right End 7 BC Panel 3-11 3/4 2-2 7/8 TC Panel 2-6 First Half 1-6 2-0 First Diag. 5-5 3/4 4-2 7/8 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform(plf) LL(1) 260.00 260.00 TC + 0-0 41-8 5/8 L-BL Uniform(plf) DL(1) 126.00 126.00 TC + 0-0 41-8 5/8 L-BL Conc @ any pp(Ibs) SM (1) 400.00 0.00 TC + Uniform(plf) DL(1) 84.00 84.00 BC + 0-0 41-8 5/8 L-BL Uniform(plf) DL(1) 32.00 32.00 TC + 0-0 41-8 5/8 L-BL Uniform (plf) SM (1) 21.00 21.00 TC + 0-0 41-8 5/8 L-BL Uniform (plf) IP(1) 60.00 60.00 TC + 0-0 41-8 5/8 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) LL(1) 95.00 95.00 TC + 0-0 41-8 5/8 L-BL Conc @ any pp(Ibs) WL(1) 400.00 0.00 TC + Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform(plf) LL(1) 0.00 130.00 TC + 38-9 1/2 41-8 5/8 L-OAL Conc @ any pp(Ibs) SM(2) 400.00 0.00 TC - Conc @ any pp(Ibs) WL(2) 400.00 0.00 TC - Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 41-8 5/8 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 12,051.83 12,712.58 3,178.14 68,324.77 68,498.56 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,889.38 24,294.32 0.00 0.00 26,136.26 2,505.82 50.90 0-2 V1S 1,832.30 23,302.38 0.00 0.00, 640.63 2,096.32 28.50 2-6 W3 1,832.30 23,302.38 30,433.50 2,517.79 1,230.51 12,777.90 28.66 3-11 3/4 W4 3,359.43 39,759.03 30,433.50 2,517.79 14,215.82 1,353.07 32.76 5-53/4 W5 3,359.43 39,759.03 47,641.56 4,142.97 1,190.32 12,215.09 32.76 7-53/4 W6 4,868.41 54,420.10 47,641.56 4,142.97 10,707.93 1,109.19 32.76 9-53/4 W7 4,868.41 54,420.10 59,733.07 5,535.74 987.13 8,707.20 32.76 11-5 3/4 W8 6,144.96 63,942.02 59,733.07 5,535.74 7,200.04 907.81 32.76 13-5 3/4 W9 6,144.96 63,942.02 66,685.40 6,696.08 785.75 5,199.31 32.76 15-5 3/4 W10 7,189.09 68,324.77 66,685.40 6,696.08 4,668.59 706.42 32.76 17-5 3/4 W11 7,189.09 68,324.77 68,498.56 7,523.95 4,668.59 4,668.59 32.76 19-5 3/4 W11 7,577.94 67,568.34 68,498.56 7,523.95 4,668.59 4,668.59 32.76 21-5 3/4 W10 7,577.94 67,568.34 65,172.55 7,573.82 4,668.59 706.42 32.76 23-5 3/4 W9 7,511.59 61,672.75 65,172.55 7,573.82 785.75 5,199.31 32.76 25-5 3/4 W8 7,511.59 61,672.75 56,707.37 7,391.26 7,200.04 907.81 32.76 27-5 3/4 *Continued on Next Page... STRESS ANALYSIS - PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:18:23 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILOINO SYSTEMS TIGARD, OR Long Span 24LH386/260 TJ67 Stress Analysis Summary, Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W7 7,212.82 50,637.98 56,707.37 7,391.26 987.13 8,707.20 32.76 29-5 3/4 W6 7,212.82 50,637.98 43,103.04 6,976.27 10,707.93 1,109.19 32.76 31-5 3/4 W5 6,681.62 34,641.59 43,103.04 6,976.27 1,190.32 12,215.09 32.76 33-5 3/4 W4 6,681.62 34,641.59 24,359.53 6,328.87 14,215.82 1,353.07 32.76 35-5 3/4 W3 6,069.20 14,553.24 24,359.53 6,328.87 1,458.83 15,746.42 32.76 37-5 3/4 W2 6,069.20 14,553.24 0.00 0.00 17,640.26 8,170.55 33.41 39-5 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V1 End Panel 5,759.20 2,096.32 28.50 V2 Interior 492.64 1,566.18 22.30 STRESS ANALYSIS - PAGE 2 1, 0 Job Number: 5618-0007 Job Name: Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:18:23 PM NEW M I L L E N N I U M Location: Joist Description: Mark: eutt_oitio SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ67 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.6070 0.9260 0.5907 1.6920 0.8536 1.3780 1.0000 3028=3 X 3 X.281 BC 1.4375 0.9304 0.5924 1.6850 0.8424 1.2442 0.9613 3025 =3 x 3 x.250 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 760.17 400.65 600.98 22-0 1/4 33-8 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 35.75 24.00 24.00 24.88 1.1250 Min Weld Len 2X: Bending Load 513.00 513.00 513.00 544.92 609.92 0.7362 Axial Load 24,294.32 23,302.38 68,324.77 14,553.24 14,553.24 Max Load Fillers TC: fa 4,787.06 7,250.27 21,258.49 4,528.08 2,603.91 93,002.12 Maximum K L/r 47.40 60.52 30.47 40.63 42.11 Max Load no Fillers TC: Fcr 42,424.94 38,252.39 46,717.98 44,314.97 43,919.62 89,560.38 Fa 25,454.96 22,951.43 28,030.79 26,588.98 26,351.77 TC OAL'Ryy: 293.51 F'e 606,108.69 192,029.36 757,486.25 426,085.97 1,801,350.13 BCOALJRyy: Cm 0.9961 0.9811 0.9812 0.9947 0.9993 294.73 Panel Point Moment 4,884.41 4,884.41 2,052.00 6,943.05 142,505.14 BC Stress: Mid Panel Moment 2,095.87 2,620.23 1,026.00 6,839.46 115,413.10 0.79 Panel Point fb 1,097.20 3,804.03 1,598.12 2,150.43 16,984.57 BCUR6: 81.0263 Mid Panel fb 399.82 811.55 317.78 2,118.35 13,755.58 TC Shear Stress: Fillers 0 0 0 0 0 7,713.96 Panel Point Stress 5,884.26 11,054.30 22,856.60 6,678.51 19,588.47 BC Shear Stress: Mid Panel Stress 0.1075 0.3411 0.7681 0.1567 0.5087 8,659.97 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 26,136.26 28,624.38 2,505.82 9,684.94 9.39 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 1,230.51 24,373.24 12,777.90 13,257.67 4.59 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 14,215.82 14,381.54 1,353.07 7,484.67 6.38 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,190.32 28,624.38 12,215.09 13,900.33 4.39 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W6 10,707.93 10,742.43 1,109.19 5,751.29 5.59 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 987.13 18,714.09 8,707.20 9,627.49 3.33 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 7,200.04 7,826.93 907.81 3,871.51 4.75 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 785.75 10,742.43 5,199.31 5,751.29 2.71 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 4,668.59 4,802.89 706.42 1,953.48 4.08 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W11 4,668.59 8,984.69 4,668.59 4,686.85 2.66 x 0.118 1 C18BB= 1.125 x 1.035 x .118 W11 4,668.59 8,984.69 4,668.59 4,686.85 2.66 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,668.59 4,802.89 706.42 1,953.48 4.08 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 785.75 10,742.43 5,199.31 5,751.29 2.71 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 7,200.04 7,826.93 907.81 3,871.51 4.75 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 987.13 18,714.09 8,707.20 9,627.49 3.33 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 10,707.93 10,742.43 1,109.19 5,751.29 5.59 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 1,190.32 28,624.38 12,215.09 13,900.33 4.39 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 14,215.82 14,381.54 1,353.07 7,484.67 6.38 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W3 1,458.83 28,624.38 15,746.42 17,591.44 5.66 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 , Job Number: Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:18:23 PM NEW MILLENNIUM Location: Joist Description: Mark: SUILOING SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ67 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 17,640.26 18,714.09 8,170.55 10,193.25 6.75 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V1 5,759.20 14,381.54 2,096.32 9,359.28 3.23 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 492.64 4,802.89 1,566.18 3,037.30 2.00 x 0.077 1 Cl OAB = 1.125 x 0.756 x.077 STRESS ANALYSIS - PAGE 3 G,> Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/7/2019 5:18:23 PM NEW MIL LE N N I ULJ M Location: Joist Description: Mark: SLALOM° SYSTEMS TIGARD,OR Long Span 24LH3861260 TJ67 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 9-9 5/8 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 5 BPL Length 3-2 BPL Length 12-4 1/4 Clear Bearing 0-11 1/8 Clear Bearing 10-3 5/8 BPL Material:2024=2 x 2 x.248 BPL Material:302025=3 x 2 x.250 Total Load 386.00 Total Load 956.00 Reqd TL Def L/80 0.00 Reqd TL Def L/120 0.98 Live Load 260.00 Live Load 830.00 Reqd LL Def L/120 0.00 Reqd LL Def U180 0.65 Section Modulus 4.4517 Section Modulus 8.3903 Reqd SM 0.0000 Reqd SM 4.7502 Mom of Inertia 8.4257 Mom of Inertia 21.7651 Reqd MI 0.0000 Reqd MI 9.5692 Seat Type:Bird Cage(Reinforced) Seat Type:Pegged or Butted(Reinforced) Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a:LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP JOIST SUBSTITUTE 0 Job Number:5618-0007 Job Name. Date Run: TIGARD HIGH SCHOOL-SHOPORDERS 11/8/2019 NEW MILLENNIUM Location: Description: Mark: BUILowG SYS-MAAS TIGARD,OR 4.0JS710/390-2 Angle Box J43 Specifications Length: Fy: Fb: LL Deflection: Live Load: Allow Deflection: Actual Deflection: 9-8 50,000.00 30,000.00 360 390.00 0.3222 0.2038 Properties Area X Y lxx lyy Rxx Ryy Qty Material 5.7188 2.1875 2.0000 12.9636 15.0126 1.5056 1.6202 2 4037=4 x 4 x .375 Axial and Bending Analysis Total Load 710.00 Properties Required Actual Axial Load 3,000.00 Section Modulus 0.0000 6.4818 Moment @ Midspan 99518.34 Moment of Inertia 0.0000 12.9636 fb 15353.55 fa 524.59 Maximum K L/r 77.05 Fa 19596.49 Fie 25156.76 fa/Fa 0.03 Combined Stress(H1-3) 0.5386 JOIST SUBSTITUTE �j� Job Number: Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 11/8/2019 NEW MILLENNIUM Location: Description: Mark: BLELOINC SYSTEMS ,TIGARD,OR 4.0JS710/390-2 Angle Box J44 Specifications Length: Fy: Fb: LL Deflection: Live Load: Allow Deflection: Actual Deflection: 9-111/4 50,000.00 30,000.00 360 390.00 0.3313 0.2276 Properties Area X Y lxx lyy Rxx Ryy Qty Material 5.7188 2.1875 2.0000 12.9636 15.0126 1.5056 1.6202 2 4037=4 x 4 x.375 Axial and Bending Analysis Total Load 710.00 Properties Required Actual Axial Load 3,000.00 Section Modulus 0.0000 6.4818 Moment @ Midspan 105172.91 Moment of Inertia 0.0000 12.9636 fb 16225.92 fa 524.59 Maximum K L/r 79.20 Fa 19170.99 Fe 23804.22 fa/Fa 0.03 Combined Stress(H1-3) 0.5682 JOIST SUBSTITUTE , Job Number: Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 11/8/2019 NEW MI L L E N N I U M Location: Description: Mark: BUILDING SYSTEMS TIGARD,OR 4.0JS710/390-2 Angie Box J45 Specifications Length: Fy: Fb: LL Deflection: Live Load: Allow Deflection: Actual Deflection: 9-8 50,000.00 30,000.00 360 390.00 0.3222 0.2038 Properties Area X Y lxx lyy Rxx Ryy Qty Material 5.7188 2.1875 2.0000 12.9636 15.0126 1.5056 1.6202 2 4037=4 x 4 x.375 Axial and Bending Analysis Total Load 710.00 Properties Required Actual Axial Load 3,000.00 Section Modulus 0.0000 6.4818 Moment @ Midspan 99518.34 Moment of Inertia 0.0000 12.9636 fb 15353.55 fa 524.59 Maximum K L/r 77.05 Fa 19596.49 F'e 25156.76 fa/Fa 0.03 Combined Stress(H1-3) 0.5386