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Report (4) 4000 Sw uUZi-►ickM FIELD MODIFICATION DETAILS RECEIVED MAR 3 2020 GENERAL NOTES. 2 CITY OF TIGARD BUILDING DIVISIOIN 1) All repair materials must meet ASTM requirements. All welding per latest AWS D1.1 2) All work must be done by an AWS certified welder. All welding must be done using E70XX electrodes. 3) The Engineer of Record shall be notified of the proposed field modifications. 4) New Millennium Building Systems (NMBS), LLC will not be responsible for field workmanship or cost. 5) The provisions of the General Specifications pertaining to Contractor's Drawings also govern work in this section. 6) The Procedures for removing and installing members for these modifications are not the responsibility of NMBS. 7) When removing members, care must be taken not to damage the remaining chords and webs. 8) Care must be taken as not to over heat areas where welding or torching are being performed. 9) Where reinforcement of top chords and/ or bottom chords occur at bridging locations, the bridging and/ or bridging clip must be removed. After the joist modifications are complete, all bridging must be reinstalled. 10) All material yield strength minimum (Fy) = 36 k.s.i. U.N.O. 11) Verify all lengths in the field before cutting any material. 12) Support Joists at 1/3 points if necessary in order to prevent joists from sagging or damage during field welding. ®REVIEWED ❑MAKE CORRECTIONS NOTED `tv PROD Fl REJECTED n REVISE AND RESUBMIT (Z71�5 C"�G I N ERR` 'i THIS REVIEW DOES NOT RELIEVE CONTRACTOR FROM COMPLIANCE WITH THE REQUIREMENTS OF THE DRAWINGS AND SPECIFICATIONS. 72501PE THIS REVIEW IS ONLY FOR GENERAL CONFORMANCE WITH THE DESIGN CONCEPT OF THE PROJECT AND GENERAL COMPLIANCE WITH THE 0,-14-19 INFORMATION GIVEN IN THE CONTRACT DOCUMENTS. CONTRACTOR IS RESPONSIBLE FOR CONFIRMING AND CORRELATING ALL QUANTITIES ,, I� AND DIMENSIONS. SELECTING FABRICATION PROCESSES AND TECHNIQUES OF ALL OTHER TRADES.AND PERFORMING DINATING THEIR WORK INRAOFE WITHD p, OREGON�' SATISFACTORY MANNER. y Y 13 14 4 03/02/2020 DAA y/S MOO' DATE CATENA CONSULTING ENGINEERS BY S K-1 Exp. 12-31-20 MEMBER �A �a PEEL OM MEI%IBER wsmure 'fity�° alai NEW MILLENNIUM BUILDING SYSTEMS Phone: (775) 428-0600 8200 WOOLERY WAY I FALLON, NEVADA 89406 I WWW.NEWMILL.COM Fax: (775) 867-2169 Project: TIGARD HIGH SCHOOL Project #: 5618-0007 By: HZ Chk: DLM Location: TIGARD, OR REFERENCE: FIELD MODIFICATION Date: 06/14/19 Sht: 1 of 4 NEW MILLENNIUM BUILDING SYSTEMS October 30, 2018 RECEIVED To: Stuart Holgate MAR 2 3 2020 North Star Industries, Inc. CITY OF TIGARD BUILDING DIVISION Project: Tigard High School—Phase 1 Tigard, OR NMBS Job#5618-0007 Re: Final Joist Design Calculations 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 Construction Documents. New Millennium Building Systems,LLC is a fully approved member company of the Steel Joist Institute. Respectfully, y `-Q� PROFF i�G ii7 � N EeRSS/�2 72501 P � Dennis Montgomery, P.E. Civil Engineer P, ', OREGON e ct•�, *gy1320\ �'� yis MONTV Exp. 12-31- IS ®REVIEWED ❑MAKE CORRECTIONS NOTED n REJECTED n REVISE AND 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:775-867-2130 I Fax:775-867-2169 I www.newmill.com Building a better steel experience. NEW MILLENNIUIV 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 Load') Load2 Poston Direction LOclse9in SplEnd___ Uniform(plf) OL(1) 96.47 96.47 TC + 0-0 30.5 5/8 Uniform(plf) LL(1) 234.22 234.22: TC + 0-0 30-5 5/8 Net DMA(plf) WL(1) 6700 67.00'; TC - 0-0 30-55/8 _ Linden(pa) TL(2) 319.00 319,00'. IC + 0.0 30-5 518 a,dal tiers ----- sM(2) 30000 0.001 l IC + 0-0 Ian Conc Load(Ibs) DL(2) 1,700.00 0.00 IC + 13-0 1/4 I13-0 1/4 1Cdnc Load Ms) DL 1.700.00 0.00 TC + 26-61(4 `26-61/4 Figure 1 (2� (Example only) Load Cantina ono Case 1:OL Case ea.0L+CL+085(TL)+WL+AX Case 2a:LL Case 6b.DL+CL+085(TL).WL-AX Case 2b:5L Case 6c:OL.CL+0.85(TL)+WL.AX.IP Case 3a:OL.CL+TL+LL Case 6d:DL+CL+0.85(1L)+WL-AX.11' Case 36:OL+CL+TL+SL Case 6e:DL+CL+085(TL)+61,.AX Case 3c:OL+CL+TL.LL+FEM Case 6t D1.+CL+0-85(TL)+SM-AX Case 3d:DL+CL+TI+SL+FEM Case 7a''DL+CL+0.a5(TL)+0.75)WL+AX.LL) Case 30:DL+CL+TL+LL Case 7b:01.+CL+0.85(TL)+0.75/WL-AX+LL) Case 31:OL+CL+TL+SL Case 7c:DL+CL+0.85(IL)+075(WL+AX+LL.IP) Case 4a:DL.WL+AX Case 7d:DL+CL.085(f1.).0.75(WL-AX+LL+IP) Case 4b:DL.WL-AX Case 7a.D1.CL+0.85(1L)+0.75(SM+AX+LL) Case 4c:0L.WL+RX+IP Case 71:DL.CL.O-85(TL)+0.75(SM-AX+W Case 4d:DL+WL-AX+IP Case 8a.OL+CL+0,65(11)+075CW L.AX+SL) Case 4e:DL.SM+AX Case 8b:DL+CL+0,85(1L)+0.75(WL-AX.SL) Case 4f:DL+SM-AX Case 8e 01..CL+0.85(TL)+0.75(W L+AX-SL+IP) Case 5a:0.6(D1.1.WL+AX Case 8d:DL.CL+0.85(TL1+0.75(WL•AX.SL+IP) Case 50:0.6(DL1•WL-AX Case 8e:DL+CL+0.85(T1.1.0.78(WL.AX.SL+SM) Case 5c:0.6(DL)+WL+M+IP Case Sf:DL.CL.085(TL)+0.75(WL-AX.SL+S81) Case 5d:0.6(01.).WL.AX+IP Case 9a:1.2(oLN0.51LL)+0.6(TL)+SMAX+FEM Figure 2 Case 5e:0,8(DL)+WL+AX+SM Case 9b:120.)+0.5(LL).0.8(1L)+SMAX+FEM Case 51:0.8(DL)+WL-AX+SM Interior Dimensions: TC PANEL „yr W V2 BC PANEL - { Left End Dimensions: OVERALL LENGTH BASELENGTH = [Hi FIRST DIAGONAL - {. TC PANEL - W2 V 1S W3 NV4 V2 BC PANEL I- - FIRST HALF Right End Dimensions: FIRST DIAGONAL TCX I-r- T C PANEL -i V2 4 W3 1S 2 v i BCX FIRST HAL F - 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 STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/�/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:11:03 AM NEW MILLENNIUM Location: Joist Description: Mark: .WL.MN6 SYSTEM% [TIGARD,OR Long Span 20LH444/300 J1 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: I 28-4 28-0 20.00 18.84 5 0 4-0 Parallel Chords Variable Left End Right End BC Panel 4-2 4-2 -T�- I {T T TI TFFH 1-Ftom TFfFTTi TC Panel 3-2 3-2 �� } �T � First Half 2-0 2-0 I1 T 1Tl SF1'I I l l TTTT7fIT TTTIP tI ---- First Diag. 6-2 6-2 Depth 20.00 20.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 L-BL Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Uniform (plf) IP(1) 66.00 66.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 L-BL Axial (lbs) SM(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) SM(1) 24.00 24.00 TC + 0-0 28-4 L-BL Axial (Ibs) SM (1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Additional Shear(Ibs) LL(1) 700.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 28-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 L-BL Axial (lbs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 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 9,264.07 8,982.00 2,316.02 41,109.22 41,806.68 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 7,421.99 22,132.48 0.00 0.00 24,147.46 7,973.21 51.56 0-2 V1S 5,521.81 21,086.29 0.00 0.00 3,825.37 2,971.50 22.34 3-2 W3 5,521.81 21,086.29 28,690.55 7,847.60 1,407.75 11,650.11 30.51 4-2 W4 5,573.06 34,551.15 28,690.55 7,847.60 9,330.15 1,407.75 30.51 6-2 W5 5,573.06 34,551.15 38,527.64 7,718.27 1,407.75 6,852.29 30.51 8-2 W6 5,283.23 41,109.22 38,527.64 7,718.27 4,996.32 1,407.75 30.51 10-2 W7 5,283.23 41,109.22 41,806.68 7,267.92 2,050.34 3,750.83 30.51 12-2 W7 4,672.36 41,109.21 41,806.68 7,267.92 2,050.34 3,750.83 30.51 14-2 W6 4,672.36 41,109.21 38,527.64 6,496.55 4,996.32 1,407.75 30.51 16-2 W5 3,740.48 34,551.15 38,527.64 6,496.55 1,407.75 6,852.29 30.51 18-2 W4 3,740.48 34,551.15 28,690.55 5,404.15 9,330.15 1,407.75 30.51 20-2 W3 2,467.50 21,086.29 28,690.55 5,404.15 1,407.75 11,650.11 30.51 22-2 V1S 2,467.50 21,086.29 0.00 0.00 3,825.37 2,971.50 22.34 25-2 W2 2,832.24 22,132.48 0.00 0.00 24,147.46 7,973.21 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.84 2,048.09 18.84 STRESS ANALYSIS- PAGE 2 0 Job Number. Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:11:03 AM NEW MILLENNIUM Location: Joist Description: Mark.: NULL.MI1J6 -SYSTEM% TIGARD,OR ,Long Span 20LH444/300 J1 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: �Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 491.22 736.83 17-1 18-111/2 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 22,132.48 21,086.29 41,109.22 21,086.29 22,132.48 Max Load Fillers TC: fa 5,224.85 11,330.62 22,089.86 11,330.62 6,718.21 50,573.97 Maximum K Lir 92.02 92.02 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 257.5857.50 yy: Fe 539,299.88 81,962.00 327,847.97 81,962.00 266,614.72 BC0AURyy: Cm 0.9952 0.9309 0.9549 0.9309 0.9874 260.64 Panel Point Moment 115025.55 5218.23 2292.00 4378.83 20249.96 BC Stress: Mid Panel Moment 91838.84 4281.25 1146.00 3364.69 13307.27 0.97 Panel Point fb 19730.13 10646.52 4676.26 8933.94 8190.10 12188 21.8893 Mid Panel fb 15752.96 3663.79 980.72 2879.43 5382.13 TC Shear Stress: Fillers 0 0 0 0 0 10,750.33 Panel Point Stress - 24,954.99 21,977.14 26,766.12 20,264.56 14,908.31 BC Shear Stress: Mid Panel Stress 0.7956 0.8329 0.8909 0.8048 0.5803 14,110.97 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 24,147.46 25,761.95 7,973.21 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 1 W3 1,407.75 24,373.24 11,650.11 12,698.97 4.18 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 9,330.15 10,742.43 1,407.75 6,045.24 4.87 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 1,407.75 14,381.54 6,852.29 7,876.57 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 4,996.32 5,758.64 1,407.75 2,799.53 3.74 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 4,996.32 5,758.64 1,407.75 2,799.53 3.74 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 1,407.75 14,381.54 6,852.29 7,876.57_ 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 9,330.15 10,742.43 1,407.75 6,045.24 4.87 x 0.129 1 _C22BB= 1.125 x 1.110 x.129 W3 1,407.75 24,373.24 11,650.11 12,698.97 4.18 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 24,147.46 25,761.95 7,973.21 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1 3,825.37 4,802.89 2,971.50 3,034.97 3.35 x 0.077 1 _C10AB= 1.125 x 0.756 x.077 V2 96.84 4,802.89 2,048.09 3,292.50 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: �f 5618 D007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:11:03 AM NEW MILLENNIUM Location: Joist Description: Mark: 9LIIr-rIlhin _,,.4*1,1s TIGARD,OR Long Span 20LH444/300 J1 TCX Design TCX Left TCX Right TCX Length 5-9 1/2 TCX Length 2-4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 9-5 BPL Length 5-11 1/2 Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material:302025=3 x 2 x.250 BPL Material:2018=2 X 2 X.188 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.87 Reqd TL Def L/80 0.35 Live Load 300.00 Live Load 300.00 Reqd LL Def L/180 0.39 Reqd LL Def U180 0.16 Section Modulus 4.6476 Section Modulus 2.4725 Reqd SM 3.8342 Reqd SM 0.6750 Mom of Inertia 10.3441 Mom of Inertia 3.9771 Reqd MI 7.0899 Reqd MI 0.5237 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(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+AX+IP STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:10:48 AM NEW MILLENNIUM li Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 20LH444/300 J10 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 28-4 28-0 20.00 18.84 5 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 4-2 4-2 TC Panel 3-2 3-2 �' _ First Half 2-0 2-0 �-, TRH - - rrriT First Diag. 6-2 6-2 Depth 20.00 20.00 Loads Load Type Category Load1 Load2 Position Direction 1 Loc/Begin Sp/End Reference Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 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 BC + 0-0 0-0 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Additional Shear(Ibs) LL (1) 700.00 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) 24.00 24.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 28-4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(1) _ _ 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 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 8,982.00 9,237.55 2,309.39 41,109.22 41,806.68 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,310.80 22,132.48 0.00 0.00 24,147.46 8,045.79 51.56 0-2 V1S 2,812.07 21,086.29 0.00 0.00 3,825.71 2,971.50 22.34 3-2 W3 2,812.07 21,086.29 28,690.55 5,720.00 1,381.98 11,607.16 30.51 4-2 W4 4,027.62 34,551.15 28,690.55 5,720.00 9,287.21 1,381.98 30.51 6-2 W5 4,027.62 34,551.15 38,527.64 6,754.97 1,381.98 6,809.34 30.51 8-2 W6 4,902.08 41,109.22 38,527.64 6,754.97 4,953.38 1,381.98 30.51 10-2 W7 4,902.08 41,109.22 41,806.68 7,468.92 1,381.98 3,740.09 30.51 12-2 W7 5,455.51 41,109.21 41,806.68 7,468.92 1,381.98 3,740.09 30.51 14-2 W6 5,455.51 41,109.21 38,527.64 7,861.84 4,953.38 1,381.98 30.51 16-2 W5 5,687.92 34,551.15 38,527.64 7,861.84 1,381.98 6,809.34 30.51 18-2 W4 5,687.92 34,551.15 28,690.55 7,933.74 9,287.21 1,381.98 30.51 20-2 W3 5,579.24 21,086.29 28,690.55 7,933.74 1,381.98 11,607.16_ 30.51 22-2 V1S 5,579.24 21,086.29 0.00 0.00 3,825.71 2,971.50 22.34 25-2 W2 7,489.56 22,132.48 0.00 0.00 24,147.46 8,045.79 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.84 2,048.09 18.84 STRESS ANALYSIS- PAGE 2 //� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:10:48 AM NEW MILLENNIUM Location: Joist Description: Mark: 9l Ill-r],Nr sys*FMS 11GARD,OR Long Span 20LH444/300 J10 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 491.22 736.83 17-1 18-101/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 22,132.48 21,086.29 41,109.22 21,086.29 22,132.48 Max Load Fillers TC: fa 6,718.21 11,330.62 22,089.86 11,330.62 5,224.85 50,573.97 Maximum K Ur 92.02 92.02 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 257.58 57.58 yy: F'e 266,614.72 81,962.00 327,847.97 81,962.00 539,299.88 BCOAURyy: Cm 0.9874 0.9309 0.9549 0.9309 0.9952 260.64 Panel Point Moment 29159.99 4605.39 2292.00 5218.23 115025.55 BC stress: Mid Panel Moment 20605.21 3624.63 1146.00 4281.25 91838.84 0.97 Panel Point fb 11793.76 9396.17 4676.26 10646.52 19730.13 BC 121.888893 Mid Panel fb 8333.78 3101.88 980.72 3663.79 15752.96 TC Shear Stress: Fillers 0 0 0 0 0 10,750.33 Panel Point Stress 18,511.97 20,726.79 26,766.12 21,977.14 24,954.99 BC Shear Stress: Mid Panel Stress 0.6705 0.8128 0.8909 0.8329 0.7956 14,110.97 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 24,147.46 25,761.95 8,045.79 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 1,381.98 24,373.24 11,607.16 12,698.97 4.17 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 9,287.21 10,742.43 1,381.98 6,045.24 4.85 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 1,381.98 14,381.54 6,809.34 7,876.57 3.06 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 4,953.38 5,758.64 1,381.98 2,799.53 3.71 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 1,381.98 7,826.93 3,740.09 4,091.27 2.47 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,381.98 7,826.93 3,740.09 4,091.27 2.47 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W6 4,953.38 5,758.64 1,381.98 2,799.53 3.71 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 1,381.98 14,381.54 6,809.34 7,876.57 3.06 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W4 9,287.21 10,742.43 1,381.98 6,045.24 4.85 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W3 1,381.98 24,373.24 11,607.16 12,698.97 4.17 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 24,147.46 25,761.95 8,045.79 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1 3,825.71 4,802.89 2,971.50 3,034.97 3.35 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 96.84 4,802.89 2,048.09 3,292.50 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 10/24/2018 9:10:48 AM NEW MILLENNIUM Location: Joist Description: Mark: 4V4TFM5 TIGARD,OR Long Span 20LH444/300 J10 TCX Design TCX Left TCX Right TCX Length 2-10 TCX Length 5-9 1/2 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 6-4 7/8 BPL Length 9-5 Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material:2018=2 X 2 X.188 BPL Material:302025=3 x 2 x.250 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.43 Reqd TL Def U80 0.87 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.19 Reqd LL Def U180 0.39 Section Modulus 2.4725 Section Modulus 4.6476 Reqd SM 0.9720 Reqd SM 3.8342 Mom of Inertia 3.9771 Mom of Inertia 10.3441 Reqd MI 0.9050 Reqd MI 7.0899 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) J 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(OL)+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 �i 1 Job Number: Job Name: Date Run: w� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/201810:09:11 AM NEW MILLENNIUM Location: Joist Description: Mark: aUI,.oItiG 3VSTEM2 TIGARD,OR Long Span 20LH444l300 J13 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 28-4 28-0 20.00 18.84 5 @ 4-0 Parallel Chords Variable Left End Right End i BC Panel 4-2 4-2 TC Panel 3-2 3-2 k.H - iff ff f tFmTff n- -FF fff TfF-j First Half 2-0 2-0 � -ifil1illatilliiIil1Ll_t_llI LI ll11:1[1 Eflanni t.l rr nth First Diag. 6-2 6-2 Depth 20.00 20.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (pif) LL(1) 300.00 300.00 TC + 0-0 28-4 L-BL Uniform (plf) DL (1) 144.00 144.00 TC + 0-0 28-4 L-BL Uniform (plf) DL (1) 96.00 96.00 BC + 0-0 28-4 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 Uniform (plf) DL (1) 20.00 20.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp (Ibs) WL(1) 100.00 0.00 TC + 14-2 0-0 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) SM (1) 24.00 24.00 TC + 0-0 28-4 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Conc @ any pp(Ibs) SM (1) 100.00 0.00 TC + 14-2 0-0 L-BL Additional Shear(Ibs) LL(1) 700.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(Ibs) SM (2) 100.00 0.00 TC - 14-2 0-0 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp (Ibs) WL(2) 100.00 0.00 TC - 14-2 0-0 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 8,982.00 9,237.55 2,309.39 41,395.85 42,141.08 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,406.35 22,228.03 0.00 0.00 24,147.46 8,120.07 51.56 0-2 V1S 2,907.61 21,181.83 0.00 0.00 3,825.71 2,971.50 22.34 3-2 W3 2,907.61 21,181.83 28,833.86 5,863.32 1,381.98 11,607.16 30.51 4-2 W4 4,218.70 34,742.23 28,833.86 5,863.32 9,287.21 1,381.98 30.51 6-2 W5 4,218.70 34,742.23 38,766.50 6,993.83 1,381.98 6,809.34 30.51 8-2 W6 5,188.70 41,395.85 38,766.50 6,993.83 4,953.38 1,381.98 30.51 10-2 W7 5,188.70 41,395.85 42,141.08 7,803.32 1,381.98 3,740.09 30.51 12-2 W7 5,742.14 41,395.84 42,141.08 7,803.32 1,381.98 3,740.09 30.51 14-2 W6 5,742.14 41,395.84 38,766.50 8,100.70 4,953.38 1,381.98 30.51 16-2 W5 5,879.01 34,742.23 38,766.50 8,100.70 1,381.98 6,809.34 30.51 18-2 W4 5,879.01 34,742.23 28,833.86 8,077.06 9,287.21 1,381.98 30.51 20-2 W3 5,674.79 21,181.83 28,833.86 8,077.06 1,381.98 11,607.16 30.51 22-2 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name Date Run: 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/201810:09:11 AM NEW MILLENNIUM Location: Joist Description: Mark: a„ll rIINt: SVSTFMS TIGARD,OR Long Span 20LH444/300 J13 Stress Anal sis Summary,Continued... Member IC Tension TC Compresion BC Tension _BC Compresion Web Tension Web Comp. Web Length PP Dist. V1S 5,674.79 21,181.83 0.00 0.00 3,825.71 2,971.50 22.34 25-2 W2 7,489.56 22,228.02 0.00 0.00 24,147.46 8,120.07 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 196.84 2,048.09 18.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/201810:09:11 AM NEW MILLENNIUM Location: Joist Description: Mark: nun-n,Nn 4YSTFMS TIGARD,OR Long Span 20LH444/300 J13 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and BendingAnalysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 491.22 736.83 17-1 18-7 7/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 22,228.03 21,181.83 41,395.85 21,181.83 22,228.02 Max Load Fillers TC: fa 6,747.22 11,381.96 22,243.87 11,381.96 5,247.41 50,573.97 Maximum K Ur 92.02 92.02 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 257.5857.58OAL yy: Fe 266,614.72 81,962.00 327,847.97 81,962.00 539,299.88 BCOAURyy: Cm 0.9873 0.9306 0.9545 0.9306 0.9951 260.64 Panel Point Moment 29159.99 4605.39 2292.00 5218.23 115025.55 BC Stress: Mid Panel Moment 20605.21 3624.63 1146.00 4281.25 91838.84 0.98 Panel Point fb 11793.76 9396.17 4676.26 10646.52 19730.13 BCLRz: 121.8893 Mid Panel fb 8333.78 3101.88 980.72 3663.79 15752.96 TC Shear Stress: Fillers 0 0 0 0 0 10,750.33 Panel Point Stress 18,540.98 20,778.13 26,920.14 22,028.48 24,977.54 BC Shear Stress: Mid Panel Stress 0.6723 0.8161 0.8969 0.8362 0.7970 14,110.97 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 24,147.46 25,761.95 8,120.07 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 1,381.98 24,373.24 11,607.16 12,698.97 4.17 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 9,287.21 10,742.43 1,381.98 6,045.24 4.85 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W5 1,381.98 14,381.54 6,809.34 7,876.57 3.06 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 4,953.38 5,758.64 1,381.98 2,799.53 3.71 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W7 1,381.98 7,826.93 3,740.09 4,091.27 2.47 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W7 1,381.98 7,826.93 3,740.09 4,091.27 2.47 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W6 4,953.38 5,758.64 1,381.98 2,799.53 3.71 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 1,381.98 14,381.54 6,809.34 7,876.57 3.06 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 9,287.21 10,742.43 1,381.98 6,045.24 4.85 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,381.98 24,373.24 11,607.16 12,698.97 4.17 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 24,147.46 25,761.95 8,120.07 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1 3,825.71 4,802.89 2,971.50 3,034.97 3.35 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 196.84 4,802.89 2,048.09 3,292.50 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/201810:09:11 AM NEW MILLENNIUM Location: Joist Description: Mark: ,,4111 niNr; SVSTFINS TIGARD,OR Long Span 20LH444/300 J13 TCX Design TCX Left TCX Right TCX Length 2-10 TCX Length 5-9 1/2 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 6-4 7/8 BPL Length 9-5 Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material:2018=2 X 2 X.188 BPL Material:302025=3 x 2 x.250 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.43 Reqd TL Def U80 0.87 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.19 Reqd LL Def U180 0.39 Section Modulus 2.4725 Section Modulus 4.6476 Reqd SM 0.9720 Reqd SM 3.8342 Mom of Inertia 3.9771 Mom of Inertia 10.3441 Reqd MI 0.9050 Reqd MI 7.0899 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) 1 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 10/24/2018 9:39:43 AM NEW NMI I L L E N N I LI AA Location: Joist Description: Mark: awi_oiwa SYSTEMS TIGARD,OR Long Span 20LH444/300 316 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 28-4 28-0 [20.00 18.53 5 Special Parallel Chords Variable Left End Right End BC Panel 4-2 3-6 TC Panel 3-2 3-2 - / I First Half 2-0 2-2 jj.LLYi 11 1 1 1 1 I 1 hJlk1 i ITI rt FJtr I I JI I I i iit-t I I IZ l J I N J--Nh Ill - First Diag. 6-2 5-8 Depth 20.00 20.00 ) Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL (1) 300.00 300.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 L-BL Axial (lbs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Axial (lbs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Additional Shear(Ibs) LL(1) 700.00 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) 96.00 96.00 BC + 0-0 28-4 L-BL Uniform (plf) SM (1) 24.00 24.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Axial (lbs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc Load (Ibs) LL(1) 5,000.00 0.00 TC + 22-3 1/4 22-3 1/4 L-OAL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 36.00 62.00 10,549.16 12,734.39 3,183.60 57,340.95 56,677.91 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,366.65 25,518.41 0.00 0.00 28,852.91 3,608.73 51.45 0-2 V1S 2,859.50 24,454.57 0.00 0.00 1,426.52 3,007.59 22.07 3-2 W3 2,859.50 24,454.57 34,066.87 5,778.53 845.19 13,875.10 30.32 4-2 W4 4,095.55 42,287.64 34,066.87 5,778.53 11,530.85 716.32 30.32 6-2 V2 4,095.55 42,287.64 34,066.87 5,778.53 94.88 2,057.44 18.53 8-2 W5 4,095.55 42,287.64 48,526.46 6,830.96 613.22 9,027.05 30.32 8-2 W6 4,984.76 53,280.77 48,526.46 6,830.96 7,151.65 3,696.43 30.32 10-2 V3 4,984.76 53,280.77 48,526.46 6,830.96 97.06 2,112.40 18.53 12-2 W7 4,984.76 53,280.77 56,053.11 7,556.95 5,209.87 5,209.87 30.32 12-2 W7 5,547.53 57,340.95 56,053.11 7,556.95 5,209.87 5,209.87 30.32 14-2 V4 5,547.53 57,340.95 56,053.11 7,556.95 97.06 2,132.70 18.53 16-2 W6 5,547.53 57,340.95 56,677.91 7,956.50 7,151.65 3,696.43 30.32 16-2 W5 5,772.17 54,464.26 56,677.91 7,956.50 2,084.23 4,509.01 25.83 18-2 V5 5,772.17 54,464.26 56,677.91 7,956.50 105.77 6,497.68 18.53 19-8 W4 5,772.17 54,464.26 38,492.38 8,015.80 20,051.11 642.48 40.49 19-8 1 *Continued on Next Page... I STRESS ANALYSIS- PAGE 1 �/� Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:39:43 AM NEW MILLENNIUM Location: Joist Description: Mark: a,„LM,tin %V%TE1.A5 TIGARD,OR Long Span 20LH444/300 J16 Stress Analysis Summary,Continued... Member IC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 5,656.74 24,745.82 38,492.38 8,015.80 705.64 18,526.22 31.93 22-8 V1S 5,656.74 24,745.82 0.00 0.00 3,300.51 2,453.62 18.95 25-2 W2 6,346.57 25,086.02 0.00 0.00 29,311.82 6,994.30 44.08 24-10 STRESS ANALYSIS- PAGE 2 //� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:39:43 AM NEW MILLENNIUM Location: Joist Description: Mark- fit lit niNr 9V5*FM5 TIGARD,OR Long Span 20LH444/300 J16 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 1.0151 0.7748 0.4934 1.4841 0.7033 0.6093 0.9679 2521 =2 1/2 x 2 1/2 x .212 Axial and BendingAnalysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 378.46 644.09 966.13 20-4 3/8 25-8 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 36.00 30.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5869 Axial Load 25,518.41 24,454.57 57,340.95 24,745.82 25,086.02 Max Load Fillers TC: fa 6,700.56 10,296.66 22,932.32 10,419.29 5,281.27 61,655.50 Maximum K Ur 74.80 74.80 56.10 62.33 74.80 Max Load no Fillers TC: Fcr 33,213.52 33,213.52 39,722.73 37,635.57 33,213.52 54,279.00 Fa 19,928.11 19,928.11 23,833.64 22,581.34 19,928.11 TCOAL/Ryy: 216.10 Fe 263,307.09 142,085.50 252,596.48 204,603.13 485,197.63 BCOAL/Ryy: Cm 0.9873 0.9638 0.9392 0.9745 0.9946 226.40 Panel Point Moment 29159.99 5065.71 5157.00 7066.88 115025.58 BC Stress: Mid Panel Moment 20364.10 4117.84 2578.50 6701.99 90578.06 0'93 BC URz: Panel Point fb 10309.09 6048.82 6157.82 8438.35 21755.95 56 _ 125.6567 Mid Panel fb 7199.43 2074.01 1298.70 3375.56 17131.94 TC Shear Stress: Fillers 0 0 0 0 0 13,359.59 Panel Point Stress 17,009.65 16,345.48 29,090.14 18,857.64 27,037.22 BC Shear Stress: Mid Panel Stress 0.5562 0.5841 1.0048 0.5679 0.7792 13,340.89 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 28,852.91 29,969.07 3,608.73 7,021.91 5.61 x 0.245 1 R112= round 1 1/8 V1 S 1,426.52 4,802.89 3,007.59 3,053.67 2.63 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W3 845.19 28,624.38 13,875.10 14,758.93 4.98 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 11,530.85 14,381.54 716.32 7,910.18 5.18 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 94.88 4,802.89 2,057.44 3,316.48 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W5 613.22 18,714.09 9,027.05 10,184.69 3.45 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 7,151.65 7,826.93 3,696.43 4,110.27 4.72 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V3 97.06 4,802.89 2,112.40 3,316.48 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W7 5,209.87 10,742.43 5,209.87 6,070.36 2.72 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W7 5,209.87 10,742.43 5,209.87 6,070.36 2.72 x 0.129 1 C22BB= 1.125 x 1.110 x .129 V4 97.06 4,802.89 2,132.70 3,316.48 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W6 7,151.65 7,826.93 3,696.43 4,110.27 4.72 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W5 2,084.23 7,826.93 4,509.01 4,569.70 2.98 x 0.102 1 C16BB= 1.125 x 1.025 x .102 V5 105.77 10,742.43 6,497.68 7,669.07 3.39 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W4 20,051.11 24,373.24 642.48 9,822.71 7.20 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 705.64 23,649.64 18,526.22 19,022.54 9.11 x 0.137 2 1513 = 1 1/2 x 1 1/2 x .137 V1 S 3,300.51 4,802.89 2,453.62 3,283.76 2.89 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W2 29,311.82 29,969.07 6,994.30 9,565.79 5.70 x 0.245 1 R112=round 1 1/8 STRESS ANALYSIS- PAGE 3 Job Number: Job Name: Date Run. 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:39:43 AM NEW MILLENNIUM Location: Joist Description: Mark: fainr-MINLI SVSTFMS TIGARD,OR Long Span 20LH444/300 J16 TCX Design TCX Left TCX Right TCX Length 2-10 TCX Length 5-9 1/2 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 6-5 BPL Length 9-3 3/8 Clear Bearing 1-3 1/8 Clear Bearing 1-0 7/8 BPL Material:2018=2 X 2 X.188 BPL Material:2525=2 1/2 x 2 1/2 x.250 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.43 Reqd TL Def U80 0.87 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.19 Reqd LL Def L/180 0.39 Section Modulus 2.8286 Section Modulus 5.1504 Reqd SM 0.9720 Reqd SM 3.8342 Mom of Inertia 4.5406 Mom of Inertia 10.4357 Reqd MI 0.9050 Reqd MI 7.0899 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(W L+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: �j/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: .un.o'ti' vsTerrs TIGARD,OR Long Span 48LH550/370 J18 Geometry - - Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length Shape: 56-4 56-0 48.00 45.86 7 Special Parallel Chords Variable Left End Right End BC Panel 8-0 8-0 � 1-i1Yra ts� r=t rka r-ll ttilitL4,0tf-r r _ +- L__ TC Panel 4-0 4-0 �, / \� . / First Half 0-10 0-10 �1`1j1 �� LEITilII11 fs-�_II11111 I11ITIII'J�fk li i- First Diag. 8-10 8-10 Depth 48.00 48.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL (1) 180.00 180.00 IC + 0-0 56-4 L-BL Uniform (plf) LL(1) 370.00 370.00 TC + 0-0 56-4 L-BL Uniform (plf) DL (1) 43.00 43.00 TC + 0-0 56-4 L-BL Uniform (plf) DL (1) 120.00 120.00 BC + 0-0 56-4 L-BL Axial (lbs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) SM (1) 30.00 30.00 TC + 0-0 56-4 L-BL Axial (Ibs) SM (1) 32,200.00 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 Load (Ibs) SM (1) 21,700.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 5-2 5-2 L-OAL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 9-4 9-4 L-OAL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 23-5 23-5 L-OAL Conc Load (Ibs) CL(1) 500.00 0.00 TC + 28-2 28-2 L-BL Conc Load (lbs) CL(1) 3,000.00 0.00 TC + 34-7 34-7 L-OAL Conc Load (Ibs) SM(1) 21,700.00 0.00 TC + 4-0 4-0 R-BL Uniform (plf) DL(2) 300.00 300.00 TC + 0-0 56-4 L-BL Uniform (plf) SM (2) 30.00 30.00 TC - 0-0 56-4 L-BL Conc Load (Ibs) SM (2) 21,700.00 0.00 TC - 4-0 4-0 L-BL Conc Load (Ibs) SM (2) 21,700.00 0.00 TC - 4-0 4-0 R-BL Gross Uplift(plf) WL(3) 54.00 54.00 TC - 0-0 56-4 L-BL Stress Analysis Summary lnt.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 52.00 72.00 41,919.35 37,258.65 10,479.84 131,623.22 105,509.64 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 36,459.41 115,752.89 0.00 0.00 93,317.13 40,567.03 104.59 0-2 V1S 14,427.09 88,752.74 0.00 0.00 30,654.02 37,921.22 66.39 4-0 W3 14,427.09 88,752.74 65,479.08 13,715.69 1,202.10 21,071.88 46.94 8-0 W4 10,795.92 107,377.66 65,479.08 13,715.69 24,506.36 1,401.49 69.33 8-10 W5 10,795.92 107,377.66 89,676.13 9,206.30 926.78 16,991.21 58.30 13-2 W6 7,969.93 123,542.94 89,676.13 9,206.30 14,729.56 720.83 58.30 16-2 W7 7,969.93 123,542.94 102,812.89 7,086.80 514.88 13,323.10 58.30 19-2 W8 6,556.93 131,623.22 102,812.89 7,086.80 13,323.10 480.55 58.30 22-2 W9 6,556.93 131,623.22 105,509.64 6,380.30 12,644.54 13,323.10 58.30 25-2 Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: r/ 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: Au,Lnwr. SYSTEM. TIGARD,OR Long Span 48LH550/370 J18 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W9 6,556.93 130,571.90 105,509.64 6,380.30 12,644.54 13,323.10 58.30 28-2 W8 6,556.93 130,571.90 100,710.20 7,086.80 13,323.10 480.55 58.30 31-2 W7 7,969.93 120,388.91 100,710.20 7,086.80 514.88 13,323.10 58.30 34-2 W6 7,969.93 120,388.91 85,470.78 9,206.30 14,729.56 720.83 58.30 37-2 W5 10,795.93 102,120.97 85,470.78 9,206.30 926.78 16,991.21 58.30 40-2 W4 10,795.93 102,120.97 58,703.80 13,715.69 24,506.36 1,401.49 69.33 43-2 W3 14,427.09 82,339.58 58,703.80 13,715.69 1,202.10 21,071.88 46.94 47-6 V1S 14,427.09 82,339.58 0.00 0.00 30,654.02 37,921.22 66.39 52-4 W2 36,459.41 106,199.73 0.00 0.00 93,317.13 40,567.03 104.59 48-4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 217.75 2,675.65 45.86 STRESS ANALYSIS- PAGE 2 /�/� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW M I L L E N N I U M Location: Joist Description: Mark: RIM ^unor SYSTEM' TIGARD,OR Long Span 48LH550/370 J18 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 2.2897 1.0781 0.6883 1.8998 1.0018 2.6613 1.0000 3534=3 1/2 x 3 1/2 x.344 Axial and Bendin 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 5,362.37 1,140.76 1,711.14 29-91/4 37-91/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.00 58.00 52.00 58.00 46.00 1.1250 Min Weld Len 2X: Bending Load 593.00 593.00 593.00 593.00 593.00 1.4182 Axial Load 115,752.90 88,752.74 131,623.22 82,339.58 106,199.73 Max Load Fillers TC. fa 20,240.77 15,519.47 23,015.88 14,398.05 18,570.28 163,975.39 Maximum K L/r 58.41 73.64 34.28 73.64 58.41 Max Load no Fillers TC: Fcr 38,962.79 33,632.86 45,883.00 33,632.86 38,962.79 156,334.17 TC Fa 23,377.67 20,179.71 27,529.80 20,179.71 23,377.67 31915 yy. 9.75 F'e 206,174.33 129,686.35 598,442.88 129,686.35 206,174.33 BCOAURyy: Cm 0.9509 0.9402 0.9742 0.9445 0.9550 353.72 Panel Point Moment 12882.84 13474.48 5337.00 13474.48 12882.84 BC Stress: Mid Panel Moment 5124.10 7601.05 2668.50 7601.05 5124.10 0'77 Panel Point fb 4229.21 4423.43 1752.04 4423.43 4229.21 1 URz: 04.6055 Mid Panel fb 669.11 992.55 348.46 992.55 669.11 TC Shear Stress: Fillers 0 0 0 0 0 15,485.15 Panel Point Stress 24,469.97 19,942.90 24,767.92 18,821.48 22,799.49 BC Shear Stress: Mid Panel Stress 0.8884 0.8036 0.8468 0.7476 0.8166 19,302.43 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 93,317.13 107,333.90 40,567.03 63,195.42 20.08 x 0.313 2 3031 =3 X 3 X.313 W3 1,202.10 31,265.52 21,071.88 22,048.74 9.16 x 0.155 2 1715= 1 3/4 x 1 3/4 x.155 W4 24,506.36 28,624.38 1,401.49 5,061.09 8.80 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W5 926.78 31,265.52 16,991.21 18,404.06 7.38 x 0.155 2 1715= 1 3/4 x 1 3/4 x.155 W6 14,729.56 16,730.22 720.83 4,137.66 6.28 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W7 514.88 28,950.00 13,323.10 16,816.88 6.27 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W8 13,323.10 14,381.54 480.55 3,671.49 5.98 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W9 12,644.54 28,950.00 13,323.10 16,816.88 6.27 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W9 12,644.54 28,950.00 13,323.10 16,816.88 6.27 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W8 13,323.10 14,381.54 480.55 3,671.49 5.98 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 514.88 28,950.00 13,323.10 16,816.88 6.27 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W6 14,729.56 16,730.22 720.83 4,137.66 6.28 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W5 926.78 31,265.52 16,991.21 18,404.06 7.38 x 0.155 2 1715= 1 3/4 x 1 3/4 x.155 W4 24,506.36 28,624.38 1,401.49 5,061.09 8.80 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 1,202.10 31,265.52 21,071.88 22,048.74 9.16 x 0.155 2 1715= 1 3/4 x 1 3/4 x.155 W2 93,317.13 107,333.90 40,567.03 63,195.42 20.08 x 0.313 2 3031 =3 X 3 X.313 V1 30,654.02 61,210.47 37,921.22 43,007.39 13.62 x 0.188 2 2521 =2 1/2 x 2 1/2 x.212 V2 217.75 7,826.93 2,675.65 2,689.39 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 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: F1Li niNf SYSTEMS TIGARD,OR Long Span 48LH550/370 J18 TCX Design TCX Left TCX Right TCX Length 0-10 TCX Length 0-10 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 1/2 Clear Bearing 0-8 1/2 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 0.13 Reqd TL Def U80 0.13 Live Load 370.00 Live Load 370.00 Reqd LL Def U120 0.08 Reqd LL Def U120 0.08 Section Modulus 3.0462 Section Modulus 3.0462 Reqd SM 0.1100 Reqd SM 0.1100 Mom of Inertia 8.7172 Mom of Inertia 8.7172 Reqd MI 0.0276 Reqd MI 0.0276 Seat Type:T-Plate Seat Type:T-Plate 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(W L-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 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: ■ui1-owc SYSTEMS TIGARD,OR Long Span 48LH550i370 J20 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 8-0 8-0 -r, , , ,, , , ,, , •1„ , t, , , �,_o , rrr,1„ h,I-l-e„ TC Panel 4-0 4-0 \� N, j\ !\ ��I / v j /�;�,A / --- '', First Half 0-10 0-10 j�H a�J I I I i i I I}T I i I i i I fv,(i I H I I th i I 1 I I IAd I I I I I II l(l I i I I First Diag. 8-10 8-10 Depth 48.00 48.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference 1 Uniform (plf) DL(1) 180.00 180.00 TC + 0-0 56-4 L-BL Uniform (plf) LL(1) 370.00 370.00 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 (plf) DL(1) 35.00 35.00 TC + 0-0 56-4 L-BL Axial (Ibs) SM (1) 3,500.00 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 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 Load (Ibs) WL(1) 2,400.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) SM (1) 2,800.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 4-4 4-4 L-BL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 8-6 8-6 L-BL Conc Load (Ibs) LL(1) 10,000.00 0.00 TC + 26-5 1/2 26-5 1/2 L-OAL Conc Load (Ibs) LL(1) 3,125.00 0.00 TC + 27-0 27-0 L-OAL Conc Load (Ibs) LL(1) 10,000.00 0.00 TC - 27-6 1/2 27-6 1/2 L-OAL Conc Load (Ibs) WL(1) 2,400.00 0.00 TC + 4-0 4-0 R-BL Conc Load (Ibs) SM (1) 2,800.00 0.00 TC + 4-0 4-0 R-BL 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 - 1-0 7-0 L-OAL Conc Load (Ibs) SM (2) 2,800.00 0.00 TC - 1-0 7-0 L-OAL Conc Load (Ibs) WL(2) 2,400.00 0.00 TC - 51-0 57-0 L-OAL Conc Load (Ibs) SM (2) 2,800.00 0.00 TC - 51-0 57-0 L-OAL Axial (Ibs) SM (3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL(3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL(3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(3) 35.00 35.00 TC + 0-0 56-4 L-BL Axial (Ibs) SM(3) 3,500.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) SM (3) 30.00 30.00 TC + 0-0 56-4 L-BL Uniform (plf) DL(3) 120.00 120.00 BC + 0-0 56-4 L-BL Uniform (plf) LL(3) 370.00 370.00 TC + 0-0 56-4 L-BL Uniform (pH) DL (3) 180.00 180.00 TC + 0-0 56-4 L-BL Uniform (plf) IP (3) 84.00 84.00 TC + 0-0 56-4 L-BL *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: AILLnING SY4TLM5 TIGARD,OR Long Span 48LH550/370 J20 Loads,Continued... Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Conc Load (Ibs) WL(3) 2,400.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) SM (3) 2,800.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) CL(3) 3,000.00 0.00 TC + 4-4 4-4 L-BL Conc Load (Ibs) CL(3) 3,000.00 0.00 TC + 8-6 8-6 L-BL Conc Load (Ibs) LL(3) 10,000.00 0.00 TC - 26-5 1/2 26-5 1/2 L-OAL Conc Load (Ibs) LL(3) 3,125.00 0.00 TC + 27-0 27-0 L-OAL Conc Load (Ibs) LL(3) 10,000.00 0.00 TC + 27-6 1/2 27-6 1/2 L-OAL Conc Load(Ibs) WL(3) 2,400.00 0.00 TC + 4-0 4-0 R-BL Conc Load(Ibs) SM (3) 2,800.00 0.00 TC + 4-0 4-0 R-BL 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 26,505.02 21,676.90 6,626.26 87,874.37 88,105.52 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 7,754.72 56,300.59 0.00 0.00 57,710.58 9,195.03 104.72 0-2 V1S 6,134.66 48,806.99 0.00 0.00 4,127.84 10,852.26 66.60 4-0 W3 6,134.66 48,806.99 49,020.44 6,622.12 2,302.55 19,473.04 47.24 8-0 W4 7,666.28 66,630.80 49,020.44 6,622.12 21,789.95 1,792.00 69.54 8-10 V2 7,666.28 66,630.80 49,020.44 6,622.12 480.34 2,465.29 46.1713-2 W5 7,666.28 66,630.80 72,273.77 8,234.76 1,257.61 14,775.35 58.5413-2 W6 8,676.91 80,413.15 72,273.77 8,234.76 12,549.82 1,240.21 58.54 16-2 V3 8,676.91 80,413.15 72,273.77 8,234.76 449.39 2,150.60 46.17 19-2 W7 8,676.91 80,413.15 84,037.79 8,992.73 1,240.21 9,411.25 58.54 19-2 W8 9,182.22 87,874.37 84,037.79 8,992.73 8,402.81 1,240.21 58.54 22-2 V4 9,182.22 87,874.37 84,037.79 8,992.73 3,902.28 8,879.60 46.17 25-2 W9 9,182.22 87,874.37 88,105.52 9,238.37 7,468.19 7,386.43 52.03 25-2 W9 9,182.22 85,742.08 88,105.52 9,238.37 1,410.85 9,558.96 66.60 27-2 V5 9,182.22 85,742.08 88,105.52 9,238.37 478.92 2,472.96 46.17 31-2 W8 9,182.22 85,742.08 80,672.55 8,992.73 8,402.81 1,240.21 58.54 31-2 W7 8,676.91 76,453.18 80,672.55 8,992.73 1,240.21 9,411.25 58.54 34-2 V6 8,676.91 76,453.18 80,672.55 8,992.73 449.39 2,129.43 46.17 37-2 W6 8,676.91 76,453.18 67,167.88 8,234.76 12,549.82 1,240.21 58.54 37-2 W5 7,666.28 60,843.16 67,167.88 8,234.76 1,257.61 14,775.35 58.54 40-2 V7 7,666.28 60,843.16 67,167.88 8,234.76 480.34 2,435.41 46.17 43-2 W4 7,666.28 60,843.16 41,787.11 6,622.12 21,789.95 1,792.00 69.54 43-2 W3 6,134.66 42,095.38 41,787.11 6,622.12 2,302.55 19,473.04 47.24 47-6 V1S 6,134.66 42,095.38 0.00 0.00 4,127.84 10,852.26 66.60 52-4 W2 7,754.72 46,469.74 0.00 0.00 57,710.58 9,195.03 104.72 48-4 STRESS ANALYSIS- PAGE 2 �/� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location Joist Description: Mark: RCM ninon 9V5*FM,i TIGARD,OR Long Span 48LH550/370 J20 Chord Properties Chord Area Rx Rz Ryy Y Ix 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 Bendin 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 33-10 1/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.00 58.00 52.00 58.00 46.00 1'1250 Bending Load 585.00 585.00 585.00 585.00 585.00 Min Weld Len 2X: 0.9239 Axial Load 56,300.59 48,807.00 87,874.37 42,095.38 46,469.74 Max Load Fillers TC: fa 14,611.39 12,666.61 22,252.17 10,924.78 12,060.04 98,179.60 Maximum K L/r 66.53 83.89 52.07 83.89 66.53 Max Load no Fillers TC: Fcr 35,058.03 29,214.88 39,519.82 29,214.88 35,058.03 88'399'72 Fa 21,034.82 17,528.93 23,711.89 17,528.93 21,034.82 TCOALRyy: 356.04 Fe 159,559.14 100,364.79 260,514.80 100,364.79 159,559.14 BCOAL/Ryy: Cm 0.9542 0.9369 0.9428 0.9456 0.9622 397.16 Panel Point Moment 12698.34 13295.76 9360.00 13295.76 12698.34 BC Stress: Mid Panel Moment 5028.86 7502.33 4680.00 7502.33 5028.86 0.91 BC L/Ft Panel Point fb 7037.28 7368.36 5187.21 7368.36 7087.28 121.88: 21.8893 Mid Panel fb 1085.50 1619.41 1010.20 1619.41 1085.50 TC Shear Stress: Fillers 0 0 0 0 0 14,336.60 Panel Point Stress 21,648.67 20,034.98 27,439.38 18,293.15 19,097.32 BC Shear Stress: Mid Panel Stress 0.7326 0.7822 0.9729 0.6813 0.6104 17,106.24 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 57,710.58 71,606.18 9,195.03 33,428.67 15.55 x 0.250 2 2525=2 1/2 x 2 1/2 x.250 V1S 4,127.84 28,950.00 10,852.26 14,457.69 5.11 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W3 2,302.55 28,950.00 19,473.04 19,940.76 9.17 x 0.143 2 1714= 1 3/4 x 1 3/4 x .143 W4 21,789.95 24,373.24 1,792.00 4,396.78 7.83 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V2 480.34 7,826.93 2,465.29 2,664.40 2.00 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W5 1,257.61 28,950.00 14,775.35 16,748.06 6.96 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W6 12,549.82 14,381.54 1,240.21 3,647.35 5.63 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V3 449.39 7,826.93 2,150.60 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,240.21 28,624.38 9,411.25 10,873.92 3.38 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W8 8,402.81 8,984.69 1,240.21 2,126.50 4.80 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V4 3,902.28 28,624.38 8,879.60 9,487.38 3.19 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W9 7,468.19 28,624.38 7,386.43 7,969.28 2.68 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W9 1,410.85 26,592.28 9,558.96 10,448.75 4.15 x 0.155 2 1515= 1 1/2 x 1 1/2 x.155 V5 478.92 7,826.93 2,472.96 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W8 8,402.81 8,984.69 1,240.21 2,126.50 4.80 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 1,240.21 28,624.38 9,411.25 10,873.92 3.38 x 0.188 1 CW4OBA= 1.5 x 1.926 x .218 V6 449.39 7,826.93 2,129.43 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 12,549.82 14,381.54 1,240.21 3,647.35 5.63 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,257.61 28,950.00 14,775.35 16,748.06 6.96 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 Continued on Next Page... STRESS ANALYSIS- PAGE 2 �/� Job Number: Job Name: Date Run: �J 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: MAIL.MIND 4VSTF/4.4G TIGARD,OR Long Span 48LH550/370 J20 Web Design Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 480.34 7,826.93 2,435.41 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W4 21,789.95 24,373.24 1,792.00 4,396.78 7.83 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 2,302.55 28,950.00 19,473.04 19,940.76 9.17 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 V1S 4,127.84 28,950.00 10,852.26 14,457.69 5.11 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W2 57,710.58 71,606.18 9,195.03 33,428.67 15.55 x 0.250 2 2525=2 1/2 x 2 1/2 x.250 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: �/ 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW PAILLENNIUN1 Location: Joist Description: Mark: Null.now-, SVS*FI.AS TIGARD,OR Long Span 48LH550/370 J20 TCX Design TCX Left TCX Right TCX Length 0-10 TCX Length 0-10 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 7/8 Clear Bearing 0-8 7/8 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 U80 0.13 j Reqd TL Def U80 0.13 Live Load 370.00. Live Load 370.00 Reqd LL Def U120 0.08 Reqd LL Def U120 0.08 Section Modulus 1.8044 Section Modulus 1.8044 Reqd SM 0.1100 Reqd SM 0.1100 Mom of Inertia 4.5452 Mom of Inertia 4.5452 Reqd MI 0.0276 Reqd MI 0.0276 Seat Type:T-Plate Seat Type:T-Plate 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)+W L-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+W L-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: �i/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 8:43:22 AM NEW PA IL LEN NI UNt Location: Joist Description: Mark: ®UILOING SYSTEMS TIGARD,OR Long Span 20LH444/300 J3 Geometry Base Length: Working Length: Joist Depth: Effective Depth: IBC Panel Length: Shape: 28-4 28-0 20.00 18.84 5 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 4-2 4-2fffffli-_F(FFF-F _ 1FTF-FfTFf -F iTTj TC Panel 3-2 3-2 , First Half 2-0 2-0 -��, Ilmit. fifTfTTTT.TfTTTTl11i, f1lTT1- t° Lai i��L,1� First Diag. 6-2 6-2 Depth 20.00 20.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 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 BC + 0-0 0-0 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Additional Shear (Ibs) LL(1) 700.00 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) 24.00 24.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 28-4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL (1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 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 9,264.07 8,982.00 2,316.02 41,109.22 41,806.68 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 7,421.99 22,132.48 0.00 0.00 24,147.46 7,973.21 51.56 0-2 V1S 5,521.81 21,086.29 0.00 0.00 3,825.37 2,971.50 22.34 3-2 W3 5,521.81 21,086.29 28,690.55 7,847.60 1,407.75 11,650.11 30.51 4-2 W4 5,573.06 34,551.15 28,690.55 7,847.60 9,330.15 1,407.75 30.51 6-2 W5 5,573.06 34,551.15 38,527.64 7,718.27 1,407.75 6,852.29 30.51 8-2 W6 5,283.23 41,109.22 38,527.64 7,718.27 4,996.32 1,407.75 30.51 10-2 W7 5,283.23 41,109.22 41,806.68 7,267.92 2,050.34 3,750.83 30.51 12-2 W7 4,672.36 41,109.21 41,806.68 7,267.92 2,050.34 3,750.83 30.51 14-2 W6 4,672.36 41,109.21 38,527.64 6,496.55 4,996.32 1,407.75 30.51 16-2 W5 3,740.48 34,551.15 38,527.64 6,496.55 1,407.75 6,852.29 30.51 18-2 W4 3,740.48 34,551.15 28,690.55 5,404.15 9,330.15, 1,407.75 30.51 20-2 W3 2,467.50 21,086.29 28,690.55 5,404.15 1,407.75 11,650.11 30.51 22-2 V1S 2,467.50 21,086.29 0.00 0.00 3,825.37 2,971.50 22.34 25-2 W2 2,832.24 22,132.48 0.00 0.00 24,147.46 7,973.21 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.84 2,048.09 18.84 STRESS ANALYSIS- PAGE 2 l/� Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 8:43:22 AM NEW MILLENNIUM Location: Joist Description: Mark: AInl_CIiN❑ SvsrFnaS TIGARD,OR Long Span 20LH444/300 J3 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 _ 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018= 2 X 2 X .188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 491.22 736.83 17-1 18-11 1/2 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 22,132.48 21,086.29 41,109.22 21,086.29 22,132.48 Max Load Fillers TC: fa 5,224.85 11,330.62 22,089.86 11,330.62 6,718.21 50,573.97 Maximum K Ur 92.02 92.02 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 TC O Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 57.5URyy: 257.58 F'e 539,299.88 81,962.00 327,847.97 81,962.00 266,614.72 BCOAL/Ryy: Cm 0.9952 0.9309 0.9549 0.9309 0.9874 260.64 Panel Point Moment 115025.55 5218.23 2292.00 4378.83 20249.96 BC Stress: Mid Panel Moment 91838.84 4281.25 1146.00 3364.69 13307.27 0.97 Panel Point fb 19730.13 10646.52 4676.26 8933.94 8190.10 BC L/Rz: 121.8893 Mid Panel fb 15752.96 3663.79 980.72 2879.43 5382.13 TC Shear Stress: Fillers 0 0 0 0 0 10,750.33 Panel Point Stress 24,954.99 21,977.14 26,766.12 20,264.56 14,908.31 BC Shear Stress: Mid Panel Stress 0.7956 0.8329 0.8909 0.8048 0.5803 14,110.97 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 24,147.46 25,761.95 7,973.21 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W3 1,407.75 24,373.24 11,650.11 12,698.97 4.18 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 9,330.15 10,742.43 1,407.75 6,045.24 4.87 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 1,407.75 14,381.54 6,852.29 7,876.57 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 4,996.32 5,758.64 1,407.75 2,799.53 3.74 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 4,996.32 5,758.64 1,407.75 2,799.53 3.74 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 1,407.75 14,381.54 6,852.29 7,876.57 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 9,330.15 10,742.43 1,407.75 6,045.24 4.87 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,407.75 24,373.24 11,650.11 12,698.97 4.18 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 24,147.46 25,761.95 7,973.21 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1 3,825.37 4,802.89 2,971.50 3,034.97 3.35 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 96.84 4,802.89 2,048.09 3,292.50 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 10/24/2018 8:43:22 AM NEW MILLENNIUM Location: Joist Description: Mark: aint ow-, •S TPIua TIGARD,OR Long Span 20LH444/300 J3 TCX Design TCX Left TCX Right TCX Length 5-9 1/2 TCX Length 2-4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 9-5 BPL Length 5-10 7/8 Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material:302025=3 x 2 x.250 BPL Material:2018=2 X 2 X.188 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.87 Reqd TL Def L/80 0.35 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.39 Reqd LL Def U180 0.16 Section Modulus 4.6476 Section Modulus 2.4725 Reqd SM 3.8342 Reqd SM 0.6750 Mom of Inertia 10.3441 Mom of Inertia 3.9771 Reqd MI 7.0899 Reqd MI 0.5237 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)+W L+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(W L+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(W L-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(W L+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(W L-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 li/A Job Number: Job Name: Date Hun: �i/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:29:02 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 24LH386/260 J46 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 35-11 35-7 24.00 22.65 8 Special Parallel Chords Variable Left End Right End BC Panel 3-7 1/2 2-9 1/2 TC Panel 2-7 2-0 �� i� � rzrrti- A � First Half 1-0 0-6 TIT. ,ITITITTI TT IT I I.11�fi f TT-.. .. F.TTILII____. T[f Ii�, II LC] � First Diag. 4-7 1/2 3-3 1/2 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position g y _._ Direction Loc/Begin 1 Sp/End Reference Uniform (plf) DL(1) 126.00 126.00 TC + 0-0 35-11 L-BL Uniform (plf) LL(1) 260.00 260.00 TC + 0-0 35-11 L-BL Uniform (plf) IP (1) 60.00 60.00 TC + 0-0 35-11 L-BL Conc @ any pp (Ibs) SM (1) 300.00 0.00 TC + 17-11 1/2 0-0 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 35-11 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 _0-0 L-BL Conc @ any pp (Ibs) WL(1) 300.00 0.00 TC + 17-11 1/2 0-0 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) DL(1) 84.00 84.00 BC + 0-0 35-11 L-BL Uniform (plf) SM(1) 21.00 21.00 TC + 0-0 35-11 L-BL Axial (Ibs) SM(1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp (Ibs) CL(1) 100.00 0.00 TC + 17-11 1/2 0-0 L-BL Additional Shear(Ibs) LL (1) 500.00 0.00 TC + 0-0 0-0 L-BL Conc Load (Ibs) LL (1) 10,000.00 0.00 TC + 10-0 1/2 10-0 1/2 L-OAL Conc Load (Ibs) LL(1) 3,125.00 0.00 TC + 10-7 10-7 L-OAL Conc Load (Ibs) LL(1) 10,000.00 0.00 TC - 11-1 1/2 11-1 1/2 L-OAL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 35-11 L-BL Conc @ any pp (Ibs) WL(2) 300.00 0.00 TC - 17-11 1/2 0-0 L-BL Conc @ any pp (Ibs) SM (2) 300.00 0.00 TC - 17-11 1/2 0-0 L-BL Axial (Ibs) WL(3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp (Ibs) SM (3) 300.00 0.00 TC + 17-11 1/2 0-0 L-BL Conc @ any pp (Ibs) CL(3) 100.00 0.00 TC + 17-11 1/2 0-0 L-BL Axial (Ibs) SM (3) 3,500.00 0.00 BC + 0-0 0-0 L-BL Axial (Ibs) SM (3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(3) 20.00 20.00 TC + 0-0 35-11 L-BL Uniform (plf) IP (3) 60.00 60.00 TC + 0-0 35-11 L-BL Cone @ any pp (Ibs) WL(3) 300.00 0.00 TC + 17-11 1/2 0-0 L-BL Additional Shear(Ibs) LL (3) 500.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(3) 126.00 126.00 TC + 0-0 _35-11 L-BL Uniform (plf) LL (3) 260.00 260.00 TC + 0-0 35-11 L-BL Uniform (plf) SM (3) 21.00 21.00 TC + 0-0 35-11 L-BL Axial (Ibs) WL(3) 3,000.00 0.00 BC + 0-0 0-0 L-BL *Continued on Next Page... STRESS ANALYSIS- PAGE 1 /ice Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:29:02 PM NEW MILLENNIUM Location: Joist Description: Mark: S"M-niNr. 4VSTEM4 TIGARD,OR Long Span 24LH386/260 J46 Loads,Continued... Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(3) 84.00 84.00 BC + 0-0 35-11 L-BL Conc Load (Ibs) LL (3) 10,000.00 0.00 TC - 10-0 1/2 10-0 1/2 L-OAL Conc Load (Ibs) LL (3) 3,125.00 0.00 TC + 10-7 10-7 L-OAL Conc Load (Ibs) LL(3) 10,000.00 0.00 TC + 11-11/2 11-11/2 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 33.00 51.00 11,073.38 9,784.38 2,768.35 53,170.87 53,087.88 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,368.76 19,984.95 0.00 0.00 23,132.50 1,863.63 47.28 0-2 V1S 1,324.47 19,510.06 0.00 0.00 605.81 1,815.09 25.87 2-7 W3 1,324.47 19,510.06 24,115.58 4,677.74 878.88 11,361.93 25.63 3-7 1/2 W4 2,307.18 33,034.77 24,115.58 4,677.74 13,432.71 1,113.94 33.00 4-7 1/2 V2 2,307.18 33,034.77 24,115.58 4,677.74 394.47 1,728.57 22.65 6-7 1/2 W5 2,307.18 33,034.77 43,835.57 6,048.09 1,021.82 14,026.57 40.02 6-71/2 W6 3,391.42 50,360.60 43,835.57 6,048.09 15,931.77 8,171.54 28.93 9-4 1/2 V3 3,391.42 50,360.60 43,835.57 6,048.09 5,851.03 10,642.08 22.6510-101/2 W7 3,391.42 50,360.60 52,048.51 6,737.73 2,309.65 4,015.52 30.89 10-101/2 W8 4,061.99 53,170.87 52,048.51 6,737.73 6,726.52 2,467.67 33.00 12-71/2 V4 4,061.99 53,170.87 52,048.51 6,737.73 386.56 1,675.94 22.65 14-71/2 W9 4,061.99 53,170.87 53,087.88 7,309.95 3,811.73 5,038.47 33.00 14-71/2 W10 4,375.65 52,109.09 53,087.88 7,309.95 4,033.53 4,033.53 33.00 16-71/2 V5 4,375.65 52,109.09 53,087.88 7,309.95 387.07 1,670.28 22.65 18-71/2 W10 4,375.65 52,109.09 49,843.18 7,153.12 4,033.53 4,033.53 33.00 18-71/2 W9 3,854.30 46,716.80 49,843.18 7,153.12 3,811.73 5,038.47 33.00 20-71/2 V6 3,854.30 46,716.80 49,843.18 7,153.12 386.06 1,643.85 22.65 22-71/2 W8 3,854.30 46,716.80 42,373.94 6,479.17 6,726.52 2,467.67 33.00 22-71/2 W7 3,027.75 37,242.59 42,373.94 6,479.17 700.72 7,909.62 33.00 24-71/2 V7 3,027.75 37,242.59 42,373.94 6,479.17 383.51 1,596.64 22.65 26-71/2 W6 3,027.75 37,242.59 31,224.64 5,500.04 9,598.69 854.88 33.00 26-71/2 W5 1,896.03 24,388.63 31,224.64 5,500.04 959.78 10,781.79 33.00 28-71/2 V8 1,896.03 24,388.63 31,224.64 5,500.04 379.44 1,528.67 22.65 30-71/2 W4 1,896.03 24,388.63 16,445.27 4,215.72 13,432.71 1,113.94 33.00 30-71/2 W3 1,029.95 14,291.13 16,445.27 4,215.72 852.20 9,480.51 23.43 32-71/2 V1S 1,029.95 14,291.13 0.00 0.00 542.20 1,403.33 24.56 33-11 W2 1,053.54 14,544.11 0.00 0.00 16,979.60 1,550.93 38.80 33-1 1/2 STRESS ANALYSIS- PAGE 2 �/� Job Number: Job Name. Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:29:02 PM NEW MILLENNIUM Location: Joist Description: Mark- AI I,,.nwr SYSTEMS TIGARD,OR Long Span 24LH386/260 J46 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 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 Axial and Bendin Analysis K: �Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 500.37 414.91 622.36 20-7 22-7 3/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 29.00 24.50 33.00 15.50 22.00 1.1250 Min Weld Len 2X: Bending Load 406.00 406.00 406.00 406.00 406.00 0.5729 Axial Load 19,984.95 19,510.06 53,170.87 14,291.13 14,544.11 Max Load Fillers TC: fa 5,133.03 9,599.52 26,161.62 7,031.65 3,735.58 55,802.79 Maximum K L/r 58.88 49.75 24.37 31.47 44.67 Max Load no Fillers TC: Fcr 37,784.84 40,526.45 46,279.65 45,001.60 41,920.64 52,956.83 TC OAL Fa 22,670.90 24,315.87 27,767.79 27,000.96 25,152.38 274.51 Ryy. 74.51 F'e 2,430,328.50 319,293.94 591,531.44 797,736.50 4,222,947.00 BCOAL/Ryy: Cm 0.9989 0.9850 0.9704 0.9956 0.9996 327.33 Panel Point Moment 1915.93 1915.93 1624.00 1256.27 495.69 BC Stress: Mid Panel Moment 2355.55 877.00 812.00 153.95 1799.04 0.95 Panel Point fb 225.93 2625.26 2225.24 1721.37 58.45 BC uaz: . 130.3681 Mid Panel fb 272.92 490.06 453.74 86.03 208.44 TC Shear Stress: Fillers 0 0 2 0 0 14,393.26 Panel Point Stress 5,358.97 12,224.78 28,386.86 8,753.02 3,794.03 BC Shear Stress: Mid Panel Stress 0.2348 0.4104 0.9568 0.2631 0.0815 12,852.04 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 23,132.50 24,373.24 1,863.63 9,312.64 8.31 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1S 605.81 4,802.89 1,815.09 2,682.66 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W3 878.88 24,373.24 11,361.93 14,195.78 4.08 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 13,432.71 14,381.54 1,113.94 7,443.94 6.03 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 394.47 4,802.89 1,728.57 3,012.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W5 1,021.82 28,624.38 14,026.57 15,614.11 5.04 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W6 15,931.77 24,373.24 8,171.54 13,175.85 5.72 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V3 5,851.03 18,714.09 10,642.08 11,992.74 4.07 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W7 2,309.65 7,826.93 4,015.52 4,054.26 2.65 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W8 6,726.52 7,826.93 2,467.67 3,848.87 4.44 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V4 386.56 4,802.89 1,675.94 3,012.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 3,811.73 10,742.43 5,038.47 5,720.64 2.63 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W 10 4,033.53 8,984.69 4,033.53 4,660.47 2.30 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V5 387.07 4,802.89 1,670.28 3,012.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W 10 4,033.53 8,984.69 4,033.53 4,660.47 2.30 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W9 3,811.73 10,742.43 5,038.47 5,720.64 2.63 x 0.129 1 C22BB= 1.125 x 1.110 x.129 V6 386.06 4,802.89 1,643.85 3,012.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W8 6,726.52 7,826.93 2,467.67 3,848.87 4.44 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 700.72 16,730.22 7,909.62 8,317.95 3.37 x 0.158 1 C32BA= 1.125 x 1.520 x.158 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:29:02 PM NEW NI I L L E N N I LI M Location: Joist Description: Mark: ih nwn SYSTEMS TIGARD,OR Long Span 24LH386/260 J46 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 383.51 4,802.89 1,596.64 3,012.93_ 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W6 9,598.69 10,742.43 854.88 5,720.64 5.01 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 959.78 24,373.24 10,781.79 11,960.98 3.87 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V8 379.44 4,802.89 1,528.67 3,012.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W4 13,432.71 14,381.54 1,113.94 7,443.94 6.03 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 852.20 16,730.22 9,480.51 10,330.92 4.04 x 0.158 1 C32BA= 1.125 x 1.520 x.158 V1S 542.20 4,802.89 1,403.33 2,825.24 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W2 16,979.60 18,714.09 1,550.93 9,140.87 6.50 x 0.176 1 C34AA= 1.125 x 1.549 x.176 STRESS ANALYSIS- PAGE 3 p Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:29:02 PM NEW M I L L E N N I UM Location: Joist Description: Mark: aim-MINIM SVSTFMS TIGARD,OR Long Span 24LH386/260 J46 TCX Design TCX Left TCX Right TCX Length 0-3 1/2 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-5 1/8 BPL Length 2-5 7/8 Clear Bearing 1-1 7/8 Clear Bearing 0-8 7/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 386.00 Total Load 386.00 Reqd TL Def U80 0.04 Reqd TL Def U80 0.00 Live Load 260.00 Live Load 260.00 Reqd LL Def U120 0.03 Reqd LL Def U120 0.00 Section Modulus 8.4801 Section Modulus 8.4801 Reqd SM 0.0162 Reqd SM 0.0000 Mom of Inertia 27.8030 Mom of Inertia 27.8030 Reqd MI 0.0019 Reqd MI 0.0000 Seat Type:Pegged or Butted(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)+W L+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(W L-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 10/25/2018 3:29:45 PM NEW NIILLENNIUNI Location: Joist Description: Mark: BUIL 0ING SVSTEMs TIGARD,OR Long Span 24LH386/260 J48 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 35-9 1/2 35-5 1/2 24.00 22.85 8 @ 4-0 Parallel Chords i Variable Left End Right End BC Panel 3-6 2-9 1/2 TC Panel 2-6 2-0 First Half 1-0 0-6 First Diag. 4-6 3-3 1/2 Depth 24.00 24.00 Loads Load Type Category Load1 - Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL (1) 260.00 260.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 126.00 126.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) IP (1) 60.00 60.00 TC + 0-0 35-9 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) 500.00 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 Uniform (plf) SM(1) 21.00 21.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 84.00 84.00 BC + 0-0 35-9 1/2 L-BL Axial (Ibs) WL (1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) DL (1) 20.00 20.00 TC + 0-0 35-9 1/2 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 35-9 1/2 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 8,414.14 8,461.79 2,115.45 40,797.75 40,508.88 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,043.71 15,566.37 0.00 0.00 17,011.93 1,202.02 46.07 0-2 V1S 1,002.75 15,127.18 0.00 0.00 583.96 1,627.81 25.81 2-6 W3 1,002.75 15,127.18 18,616.73 4,274.90 585.36 8,397.61 25.81 3-6 W4 1,743.58 24,785.03 18,616.73 4,274.90 10,415.38 726.71 33.14 4-6 W5 1,743.58 24,785.03 29,833.74 5,136.65 726.71 8,841.92 33.14 6-6 W6 2,454.09 34,071.63 29,833.74 5,136.65 7,664.36 726.71 33.14 8-6 W7 2,454.09 34,071.63 37,145.82 5,695.92 726.71 5,999.53 33.14 10-6 W8 2,862.13 39,409.20 37,145.82 5,695.92 4,821.97 726.71 33.14 12-6 W9 2,862.13 39,409.20 40,508.88 5,952.71 726.71 3,157.14 33.14 14-6 W10 2,967.68 40,797.75 40,508.88 5,952.71 3,067.82 726.71 33.1416-6 W10 2,967.68 40,797.75 39,922.92 5,907.02 3,067.82 726.71 33.14 18-6 W9 2,770.75 38,237.27 39,922.92 5,907.02 726.71 3,157.14 33.14 20-6 W8 2,770.75 38 237.27 35 387.92 5,558.86 4,821.97 726.71 33.14 22-6 W7 2,271.35 31,727.77 35,387.92 5,558.86 726.71 5,999.53 33.14 24-6 W6 2,271.35 31,727.77 26,903.90 4,908.21 7,664.36 726.71 33.14 26-6 W5 1,469.46 21,269.23 26,903.90 4,908.21 726.71 8,841.92 33.14 28-6 W4 1,469.46 21,269.23 14,537.02 3,955.09 10,415.38 726.71 33.14 30-6 Continued on Next Page... STRESS ANALYSIS- PAGE 1 //� Job Number: Job Name: Date Run: �J 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:29:45 PM NEW M I L L E N N I U N% Location: Joist Description: Mark: Emu 1-11Nel 9ivG*F1..IS TIGARD,OR Long Span 24LH386/260 J48 Stress Analysis Summary, Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 810.94_ 12,687.16 14,537.02 3,955.09 567.61 8,116.35 23.63 32-6 V1S 810.94 12,687.16 0.00 0.00 541.49 1,284.26 24.75 33-91/2 W2 834.33 12,937.90 0.00 0.00 14,628.15 1,030.74 38.92 33-0 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 86.84 1,512.98 22.85 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �//� 561 B 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:29:45 PM NEW MILLENNIUM Location: Joist Description: Mark: Fll,l ntnan s„s*FMS TIGARD,OR Long Span 24LH386/260 J48 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x.216 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 399.95 335.16 502.74 17-1 7/8 21-9 1/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: 1.1250 Length 28.00 24.00 24.00 15.50 22.00 I Min Weld Len 2JC Bending Load 406.00 406.00 406.00 406.00 406.00 0.5000 Axial Load 15,566.37 15,127.18 40,797.75 12,687.16 12,937.90 Max Load Fillers TC: fa 4,453.13 9,254.36 24,958.86 7,761.63 3,701.20 44,789.44 Maximum K Ur 71.36 61.16 45.87 39.50 56.07 Max Load no Fillers TC: Fcr 34,457.82 38,034.96 42,869.89 44,609.14 39,733.42 41,125.26 TC Fa 20,674.69 22,820.98 25,721.93 26,765.48 23,840.05 328.23 28.23 yy: F'e 2,717,857.00 186,966.06 332,384.13 448,251.63 4,402,479.00 eCOAL/Ryy. Cm 0.9992 0.9753 0.9497 0.9913 0.9996 330.06 Panel Point Moment 1664.08 1664.08 1624.00 1269.19 435.53 BC Stress: Mid Panel Moment 2089.51 797.36 812.00 189.75 1828.99 0'94 Panel Point fb 197.15 • 3842.36 3749.82 2930.57 51.60 BCURz: 121.8893 Mid Panel fb 274.35 751.09 764.88 178.74 240.14 TC Shear Stress: Fillers 0 0 0 0 0 10,761.43 Panel Point Stress 4,650.28 13,096.72 28,708.68 10,692.20 3,752.80 BC Shear Stress: Mid Panel Stress 0.2235 0.4292 0.9949 0.2954 0.0856 12,347.99 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 17,011.93 21,935.91 1,202.02 9,601.28 6.11 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 585.36 14,381.54 8,397.61 8,711.84 3.77 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 10,415.38 14,381.54 726.71 7,419.86 4.68 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 726.71 18,714.09 8,841.92 9,542.60 3.38 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 7,664.36 8,984.69 726.71 4,644.87 4.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 726.71 14,381.54 5,999.53 7,419.86 2.69 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 4,821.97 5,758.64 726.71 2,484.76 3.61 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W9 726.71 7,826.93 3,157.14 3,835.49 2.08 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W 10 3,067.82 4,802.89 726.71 1,915.97 2.68 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W10 3,067.82 4,802.89 726.71 1,915.97 2.68 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W9 726.71 7,826.93 3,157.14 3,835.49 2.08 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W8 4,821.97 5,758.64 726.71 2,484.76 3.61 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W7 726.71 14,381.54 5,999.53 7,419.86 2.69 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W6 7,664.36 8,984.69 726.71 4,644.87 4.37 x 0.118 1 C18BB= 1.125 x 1.035 x .118 W5 726.71 18,714.09 8,841.92 9,542.60 3.38 x 0.176 1 C34AA= 1.125 x 1.549 x .176 W4 10,415.38 14,381.54 726.71 7,419.86 4.68 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W3 567.61 14,381.54 8,116.35 9,111.89 3.64 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W2 14,628.15 15,057.20 1,030.74 7,884.31 6.23 x 0.158 1 C32BA= 1.125 x 1.520 x .158 V1 583.96 4,802.89 1,627.81 2,689.05 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 V2 86.84 4,802.89 1,512.98 2,998.68 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 10/25/2018 3:29:45 PM NEW MI L LE N N I U M Location: Joist Description: Mark: Alla MIND SVSTFM5 TIGARD,OR Long Span 24LH386/260 J48 TCX Design TCX Left TCX Right TCX Length 0-5 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-5 1/2 BPL Length 2-5 7/8 Clear Bearing 1-3 1/4 Clear Bearing 0-8 7/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 386.00 Total Load 386.00 Reqd TL Def U80 0.06 Reqd TL Def L/80 0.00 Live Load 260.00 Live Load 260.00 Reqd LL Def U120 0.04 Reqd LL Def U120 0.00 Section Modulus 7.6163 Section Modulus 7.6163 Reqd SM 0.0263 Reqd SM 0.0000 Mom of Inertia 26.0236 Mom of Inertia 26.0236 Reqd MI 0.0038 Reqd MI 0.0000 Seat Type:Pegged or Butted(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+AX+IP STRESS ANALYSIS- PAGE 1 4 Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:30:19 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 24LH386/260 J50 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 1 35-91/2 35-51/2 24.00 22.85 8 @ 4-0 Parallel Chords 1 Variable Left End Right End BC Panel 3-6 2-9 1/2 TC Panel 2-6 2-0 � Jillll(1114 ltII h ill lll1�11111111�i 11111111I111IC\.l I fill lL 111 l l l llllllliil llliA 11111l �� / , First Half 1-0 0-6 �U1 111(1, t(I i I I i)1 ti I I I i I hJ ICI I I I I(Y,IXI I I i I I l I I11 I I I I 11`.1'I 11 I I 113,1411 111✓ First Diag. 4-6 3-3 1/2 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference '. Uniform (plf) LL(1) 260.00 260.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 126.00 126.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) IP (1) 60.00 60.00 TC + 0-0 35-9 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) 500.00 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 Uniform (plf) SM (1) 21.00 21.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 84.00 84.00 BC + 0-0 35-9 1/2 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 35-9 1/2 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 35-9 1/2 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 8,414.14 8,461.79 2,115.45 40,797.75 40,508.88 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,043.71 15,566.37 0.00 0.00 17,011.93 1,202.02 46.07 0-2 V1S 1,002.75 15,127.18 0.00 0.00 583.96 1,627.81 25.81 2-6 W3 1,002.75 15,127.18 18,616.73 4,274.90 585.36 8,397.61, 25.81 3-6 W4 1,743.58 24,785.03 18,616.73 4,274.90 10,415.38 726.71 33.14 4-6 W5 1,743.58 24,785.03 29,833.74 5,136.65 726.71 8,841.92 33.14 6-6 W6 2,454.09 34,071.63 29,833.74 5,136.65 7,664.36 726.71 33.14 8-6 W7 2,454.09 34,071.63 37,145.82 5,695.92 726.71 5,999.53 33.14 10-6 W8 2,862.13 39,409.20 37,145.82 5,695.92 4,821.97 726.71 33.14 12-6 W9 2,862.13 39,409.20 40,508.88 5,952.71 726.71 3,157.14 33.14 14-6 W10 2,967.68 40,797.75 40,508.88 5,952.71 3,067.82 726.71 33.14 16-6 W10 2,967.68 40,797.75 39,922.92 5,907.02 3,067.82 726.71 33.14 18-6 W9 2,770.75 38,237.27 39,922.92 5,907.02 726.71 3,157.14 33.14 20-6 W8 2,770.75 38,237.27 35,387.92 5,558.86 4,821.97 726.71 33.14 22-6 W7 2,271.35 31,727.77 35,387.92 5,558.86 726.71 5,999.53 33.14 24-6 W6 2,271.35 31,727.77 26,903.90 4,908.21 7,664.36 726.71 33.14 26-6 W5 1,469.46 21,269.23 26,903.90 4,908.21 726.71 8,841.92 33.14 28-6 W4 1,469.46 21,269.23 14,537.02 3,955.09 10,415.38 726.71 33.14 30-6 'Continued on Next Page... STRESS ANALYSIS- PAGE 1 �/� Job Number: Job Name: Date Run �f 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:30:19 PM NEW M I L L E N N I U NI Location: Joist Description: Mark: AIM ntNG 9VSTFMS TIGARD,OR Long Span 24LH386/260 J50 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 810.94 12,687.16 14,537.02 3,955.09 567.61 8,116.35 23.63 32-6 V1S 810.94 12,687.16 0.00 0.00 541.49 1,284.26 24.75 33-91/2 W2 834.33 12,937.90 0.00 0.00 14,628.15 1,030.74 38.92 33-0 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 86.84 1,512.98 22.85 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:30:19 PM NEW MILLENNIUM Location: Joist Description: Mark: PIM niWG SVST5M5 TIGARD,OR Long Span 24LH386/260 J50 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x .216 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: y: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 399.95 335.16 502.74 17-17/8 21-91/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 24.00 24.00 15.50 22.00 1.1250 Min Weld Len 2X: Bending Load 406.00 406.00 406.00 406.00 406.00 0.5000 Axial Load 15,566.37 15,127.18 40,797.75 12,687.16 12,937.90 Max Load Fillers TC: fa 4,453.13 9,254.36 24,958.86 7,761.63 3,701.20 44,789.44 Maximum K L/r 71.36 61.16 45.87 39.50 56.07 Max Load no Fillers TC: Fcr 34,457.82 38,034.96 42,869.89 44,609.14 39,733.42 41,125.26 Fa 20,674.69 22,820.98 25,721.93 26,765.48 23,840.05 TC oALmyy: 328.23 Fe 2,717,857.00 186,966.06 332,384.13 448,251.63 4,402,479.00 BCOAURyy: Cm 0.9992 0.9753 0.9497 0.9913 0.9996 330.06 Panel Point Moment 1664.08 1664.08 1624.00 1269.19 435.53 BC Stress: Mid Panel Moment 2089.51 797.36 812.00 189.75 1828.99 0-94 Panel Point fb 197.15 3842.36 3749.82 2930.57 51.60 BCURz: 121.8893 Mid Panel fb 274.35 751.09 764.88 178.74 240.14 TC Shear Stress: Fillers 0 0 0 0 0 10,761.43 Panel Point Stress 4,650.28 13,096.72 28,708.68 10,692.20 3,752.80 BC Shear Stress: Mid Panel Stress 0.2235 0.4292 0.9949 0.2954 0.0856 12,347.93 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 17,011.93 21,935.91 1,202.02 9,601.28 6.11 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 585.36 14,381.54 8,397.61 8,711.84 3.77 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 10,415.38 14,381.54 726.71 7,419.86 4.68 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 726.71 18,714.09 8,841.92 9,542.60 3.38 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 7,664.36 8,984.69 726.71 4,644.87 4.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 726.71 14,381.54 5,999.53 7,419.86 2.69 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 4,821.97 5,758.64 726.71 2,484.76 3.61 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W9 726.71 7,826.93 3,157.14 3,835.49 2.08 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W10 3,067.82 4,802.89 726.71 1,915.97 2.68 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W 10 3,067.82 4,802.89 726.71 1,915.97 2.68 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 726.71 7,826.93 3,157.14 3,835.49 2.08 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W8 4,821.97 5,758.64 726.71 2,484.76 3.61 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 726.71 14,381.54 5,999.53 7,419.86 2.69 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 7,664.36 8,984.69 726.71 4,644.87 4.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 726.71 18,714.09 8,841.92 9,542.60 3.38 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 10,415.38 14,381.54 726.71 7,419.86 4.68 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 567.61 14,381.54 8,116.35 9,111.89 3.64 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W2 14,628.15 15,057.20 1,030.74 7,884.31 6.23 x 0.158 1 C32BA= 1.125 x 1.520 x.158 V1 583.96 4,802.89 1,627.81 2,689.05 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 86.84 4,802.89 1,512.98 2,998.68 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 /ram Job Number: Job Name: Date Run: �f 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:30:19 PM NEW MILLENNIUM Location: Joist Description: Mark: VIIIII fllr,r: SVZTF14.14 TIGARD,OR Long Span 24LH386/260 J50 TCX Design TCX Left TCX Right TCX Length 0-5 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-5 1/2 BPL Length 2-5 7/8 Clear Bearing 1-3 1/4 Clear Bearing 0-8 7/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 386.00 Total Load 386.00 Reqd TL Def L/80 0.06 Reqd TL Def L/80 0.00 Live Load 260.00 Live Load 260.00 Reqd LL Def U120 0.04 Reqd LL Def U120 0.00 Section Modulus 7.6163 Section Modulus 7.6163 Reqd SM 0.0263 Reqd SM 0.0000 Mom of Inertia 26.0236 Mom of Inertia 26.0236 Reqd MI 0.0038 Reqd MI 0.0000 Seat Type:Pegged or Butted(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 STRESS ANALYSIS- PAGE 1 //� Job Number: Job Name. Date Run: �f 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:30:51 PM NEW M I L L E N NI U M Location: Joist Description: Mark: s�1l 011•I� gvq*F^".1 TIGARD,OR Long Span 24LH386/260 J51 Geometry _ Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: I Shape: 35-91/2 35-51/2 24.00 22.47 8 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-6 2-9 1/2 TITTISITI ETT II 7T'LT7TTT1 TI TTT T17 11il 1I113PT TT1T ITIr1:nTrT1TTi$TTBTIT i TC Panel 2 6 2-0 � �. �� First Half 1-0 0-6 FBI IT 1J IJ tUI I_UUk�LL i First Diag. 4-6 3-3 1/2 Depth 24.00 24.00 Loads Load Type Category Load1 Load2 1 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 126.00 126.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) LL(1) 260.00 260.00 TC + 0-0 35-9 1/2 L-BL Axial (Ibs) WL(1) 3,000.00 0.00_ BC + 0-0 0-0 L-BL Uniform (plf) IP (1) 60.00 60.00 TC + 0-0 35-9 1/2 L-BL Additional Shear(Ibs) LL(1) 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 Uniform (plf) DL(1) 84.00 84.00 BC + 0-0 35-9 1/2 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 35-9 1/2 L-BL Axial (Ibs) SM (1) 3,500.00 0.00_ BC + 0-0 0-0 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 35-9 1/2 L-BL Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 5-3 5-3 L-OAL Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 16-5 16-5 L-OAL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 35-9 1/2 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 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 12,679.71 10,196.23 3,169.93 57,303.71 58,862.17 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,061.22 23,381.69 0.00 0.00 25,935.71 1,217.25 45.88 0-2 V1S 1,019.57 22,935.13 0.00 0.00 586.10 1,672.63 25.48 2-6 W3 1,019.57 22,935.13 28,760.81 4,296.29 587.50 13,263.80 25.48 3-6 W4 1,772.83 36,918.01 28,760.81 4,296.29 13,044.87 733.13 32.88 4-6 W5 1,772.83 36,918.01 43,402.89 5,172.49 733.13 11,457.51_ 32.88 6-6 W6 2,495.26 49,063.38 43,402.89 5,172.49 10,269.54 733.13 32.88 8-6 W7 2,495.26 49,063.38 53,540.62 5,741.14 733.13 8,590.01 32.88 10-6 W8 2,910.14 57,193.47 53,540.62 5,741.14 7,402.05 733.13 32.88 12-6 W9 2,910.14 57,193.47 58,862.17 6,002.24 733.13 5,722.52 32.88 14-6 W10 3,017.46 57,303.71 58,862.17 6,002.24 4,637.63 4,637.63 32.88 16-6 W10 3,017.46 57,303.71 54,562.00 5,955.79 4,637.63 4,637.63 32.88 18-6 W9 2,817.23 50,995.90 54,562.00 5,955.79 733.13 5,722.52 32.88 20-6 W8 2,817.23 50,995.90 46,246.58 5,601.78 7,402.05 733.13 32.88 22-6 W7 2,309.45 40,672.84 46,246.58 5,601.78 733.13 8,590.01 32.88 24-6 W6 2,309.45 40,672.84 33,915.87 4,940.23 10,269.54 733.13 32.88 26-6 'Continued on Next Page... STRESS ANALYSIS- PAGE 1 �/� Job Number: Job Name: Date Run: ��/ 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:30:51 PM NEW M I L L E N NI U M Location: Joist Description: Mark: Rini nitir, SYSTEMS TIGARD,OR Long Span 24LH386/260 J51 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W5 1,494.11 26,334.50 33,915.87 4,940.23 733.13 11,457.51 32.88 28-6 W4 1,494.11 26,334.50 17,637.17 3,971.11 13,044.87 733.13 32.88 30-6 W3 824.55 15,293.23 17,637.17 3,971.11 568.23 9,920.38 23.26 32-6 V1S 824.55 15,293.23 0.00 0.00 542.84 1,300.41 24.40 33-91/2 W2 848.32 15,548.18 0.00 0.00 17,775.68 1,042.10 38.70 33-0 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 87.09 2,344.80 22.47 STRESS ANALYSIS- PAGE 2 //� Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:30:51 PM NEW PA ILLENNIUNI Location: Joist Description: Mark: _L,ILMItiL =v5,1-1.1as TIGARD,OR Long Span 24LH386/260 J51 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 1.0151 0.7748 0.4934 1.4841 0.7033 0.6093 0.9679 2521 =2 1/2 x 2 1/2 x.212 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 541.10 453.44 680.16 21-101/4 29-81/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 24.00 24.00 15.50 22.00 1.1250 Min Weld Len 2X: Bending Load 406.00 406.00 406.00 406.00 406.00 0.6174 Axial Load 23,381.69 22,935.13 57,303.71 15,293.23 15,548.18 Max Load Fillers TC: fa 5,699.52 10,232.50 25,566.03 6,823.07 3,790.02 59,849.52 Maximum K Ur 51.51 44.15 33.11 28.51 40.47 Max Load no Fillers TC: For 38,755.03 40,650.88 43,072.44 43,908.75 41,518.74 57,427.07 TC Fa 23,253.02 24,390.53 25,843.46 26,345.25 24,911.25 257.6957.69 yy: F'e 2,563,715.75 401,690.22 714,116.00 963,053.38 4,152,795.75 BCOAURyy: Cm 0.9989 0.9873 0.9760 0.9965 0.9995 286.71 Panel Point Moment 1725.41 1725.41 1624.00 1249.55 526.94 BC Stress: Mid Panel Moment 2058.86 774.95 812.00 135.35 1783.41 0.97 Panel Point fb 201.84 1954.84 1839.95 1415.71 61.64 BCURZ: 97.2841 Mid Panel fb 223.68 351.84 368.66 61.45 193.76 TC Shear Stress: Fillers 0 0 0 0 0 13,863.98 Panel Point Stress 5,901.35 12,187.35 27,405.99 8,238.78 3,851.66 BC Shear Stress: Mid Panel Stress 0.2523 0.4311 1.0015 0.2610 0.0830 13,215.63 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 25,935.71 28,624.38 1,217.25 11,091.20 9.32 x 0.188 _ 1 C4OBA= 1.125 x 2.014 x .218 W3 587.50 24,373.24 13,263.80 14,244.36 4.76 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W4 13,044.87 14,381.54 733.13 7,464.59 5.86 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W5 733.13 24,373.24 11,457.51 11,996.09 4.12 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W6 10,269.54 10,742.43 733.13 5,736.18 5.36 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 733.13 18,714.09 8,590.01 9,601.19 3.29 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 7,402.05 7,826.93 733.13 3,860.34 4.89 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 733.13 10,742.43 5,722.52 5,736.18 2.99 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W 10 4,637.63 8,984.69 4,637.63 4,673.84 2.65 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W 10 4,637.63 8,984.69 4,637.63 4,673.84 2.65 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W9 733.13 10,742.43 5,722.52 5,736.18 2.99 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 7,402.05 7,826.93 733.13 3,860.34 4.89 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 733.13 18,714.09 8,590.01 9,601.19 3.29 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 10,269.54 10,742.43 733.13 5,736.18 5.36 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 733.13 24,373.24 11,457.51 11,996.09 4.12 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 13,044.87 14,381.54 733.13 7,464.59 5.86 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 568.23 16,730.22 9,920.38 10,368.99 4.23 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W2 17,775.68 18,714.09 1,042.10 9,160.58 6.80 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V 1 586.10 4,802.89 1,672.63 2,725.35 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 87.09 4,802.89 2,344.80 3,025.24 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 10/25/2018 3:30:51 PM NEW MILLENNIUM Location: Joist Description: Mark: FIB„ SVS*FNS TIGARD,OR Long Span 24LH386/260 J51 TCX Design TCX Left TCX Right TCX Length 0-5 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-5 1/2 BPL Length 2-5 3/4 Clear Bearing 1-2 7/8 Clear Bearing 0-8 7/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 386.00 Total Load 386.00 Reqd TL Def L/80 0.06 Reqd TL Def U80 0.00 Live Load 260.00 Live Load 260.00 Reqd LL Def U120 0.04 Reqd LL Def U120 0.00 Section Modulus 8.5484 Section Modulus 8.5484 Reqd SM 0.0263 Reqd SM 0.0000 Mom of Inertia 28.8089 Mom of Inertia 28.8089 Reqd MI 0.0038 Reqd MI 0.0000 Seat Type:Pegged or Butted(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+AX+IP STRESS ANALYSIS- PAGE 1 OP Job Number: Job Name Date Run: �j/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:31:16 PM NEW MILLENNIUM Location. Joist Description: Mark: BUILDING SYRTI*/Q TIGARD,OR Long Span 24LH386/260 J53 Geometry Base Length: Working Length: [Joist Depth: Effective Depth: BC Panel Length: Shape: 35-91/2 35.51/2 24.00 22.47 8@4-0 Parallel Chords Variable Left End Right End BC Panel 3-6 2-9 1/2 (TLTTT(rtTT it II prir1TnJur irT T:IIrn-7717T}7TT9,TTr nhr1ITI TTTTITT TII TC Panel 2-6 2-0 �.., ;, ��.}�.�� �, First Half 1-0 0-6_ Cl i l �j�i_I�Iliaili. I I I''1'1 � �'z First Diag. 4-6 3-3 1/2 1 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 35-9 1/2 L-BL Uniform (plf) DL (1) 126.00 126.00 TC + 0-0 35-9 1/2 L-BL Axial (lbs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) DL (1) 20.00 20.00 TC + 0-0 35-9 1/2 L-BL Additional Shear(lbs) LL(1) 500.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL (1) 84.00 84.00 BC + 0-0 35-9 1/2 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) _ SM(1) 21.00 21.00 TC + 0-0 35-9 1/2 L-BL Axial (lbs) SM(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) IP (1) 60.00 60.00 TC + 0-0 35-9 1/2 L-BL Axial (lbs) SM(1) 3,500.00 0.00 BC + 0-0 0-0 L-BL Conc Load (lbs) CL(1) 3,000.00 0.00 TC _ + 5-3 5-3 L-OAL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 16-5 16-5 L-OAL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 35-9 1/2 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 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 12,679.71 10,196.23 3,169.93 57,303.71 58,862.17 Member TC Tension IC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. _ W2 1,061.22 23,381.69 0.00 0.00 25,935.71 1,217.25 45.88 0-2 V1S 1,019.57 22,935.13 0.00 0.00 586.10 1,672.63 25.48 2-6 W3 1,019.57 22,935.13 28,760.81 4,296.29 587.50 13,263.80 25.48 3-6 W4 1,772.83 36,918.01 28,760.81 4,296.29 13,044.87 733.13 32.88 4-6 W5 1,772.83 36,918.01 43,402.89 5,172.49 733.13 11,457.51 32.88 6-6 W6 2,495.26 49,063.38 43,402.89 5,172.49 10,269.54 733.13 32.88 8-6 W7 2,495.26 49,063.38 53,540.62 5,741.14 733.13 8,590.01 32.88 10-6 W8 2,910.14 57,193.47 53,540.62 5,741.14 7,402.05 733.13 32.88 12-6 W9 2,910.14 57,193.47 58,862.17 6,002.24 733.13 5,722.52 32.88 14-6 W10 3,017.46 57,303.71 58,862.17 6,002.24 4,637.63 4,637.63 32.88 16-6 W10 3,017.46 57,303.71 54,562.00 5,955.79 4,637.63 4,637.63 32.88 18-6 W9 2,817.23 50,995.90 54,562.00 5,955.79 733.13 5,722.52 32.88 20-6 W8 2,817.23 50,995.90 46,246.58 5,601.78 7,402.05 733.13 32.88 22-6 W7 2,309.45 40,672.84 46,246.58. 5,601.78 733.13 8,590.01 32.88 24-6 W6 2,309.45 40,672.84 33,915.87 4,940.23 10,269.54 733.13 32.88 26-6 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:31:16 PM NEW MILLENNIUM Location: Joist Description: Mark: Phil nirar, SVSTFMS TIGARD,OR Long Span 24LH386/260 J53 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W5 1,494.11 26,334.50 33,915.87 4,940.23 733.13 11,457.51 32.88 28-6 W4 1,494.11 26,334.50 17,637.17 3,971.11 13,044.87 733.13 32.88 30-6 W3 824.55 15,293.23 17,637.17 3,971.11 568.23 9,920.38 23.26 32-6 V 1 S 824.55 15,293.23 0.00 0.00 542.84 1,300.41 24.40 33-9 1/2 W2 848.32 15,548.18 0.00 0.00 17,775.68 1,042.10 38.70 33-0 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 87.09 2,344.80 22.47 STRESS ANALYSIS- PAGE 2 �/A Job Number Job Name: Date Run: �/�/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:31:16 PM NEW MILLENNIUM Location: Joist Description: Mark: atm.nwr. sv=.reiue TIGARD,OR Long Span 24LH386/260 J53 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 1.0151 0.7748 0.4934 1.4841 0.7033 0.6093 0.9679 2521 =2 1/2 x 2 1/2 x.212 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 541.10 453.44 680.16 21-101/4 29-81/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 24.00 24.00 15.50 22.00 1.1250 Mn Bending Load 406.00 406.00 406.00 406.00 406.00 016174dten2x: Axial Load 23,381.69 22,935.13 57,303.71 15,293.23 15,548.18 Max Load Fillers TC: fa 5,699.52 10,232.50 25,566.03 6,823.07 3,790.02 59,849.52 Maximum K[Jr 51.51 44.15 33.11 28.51 40.47 Max Load no Fillers TC: Fcr 38,755.03 40,650.88 43,072.44 43,908.75 41,518.74 57,427.07 Fa 23,253.02 24,390.53 25,843.46 26,345.25 24,911.25 TC oauRyy: 257.69 Fe 2,563,715.75 401,690.22 714,116.00 963,053.38 4,152,795.75 Bc0AURyy: Cm 0.9989 0.9873 0.9760 0.9965 0.9995 286.71 Panel Point Moment 1725.41 1725.41 1624.00 1249.55 526.94 BC Stress: Mid Panel Moment 2058.86 774.95 812.00 135.35 1783.41 0.97 BC L/RzPanel Point fb 201.84 1954.84 1839.95 1415.71 61.64 97.284: 7.2841 Mid Panel fb 223.68 351.84 368.66 61.45 193.76 -- TC Shear Stress. Fillers 0 0 0 0 0 13,863.98 Panel Point Stress 5,901.35 12,187.35 27,405.99 8,238.78 3,851.66 BC Shear Stress: Mid Panel Stress 0.2523 0.4311 1.0015 0.2610 0.0830 13,215.63 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 25,935.71 28,624.38 1,217.25 11,091.20 9.32 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W3 587.50 24,373.24 13,263.80 14,244.36 4.76 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 13,044.87 14,381.54 733.13 7,464.59 5.86 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 733.13 24,373.24 11,457.51 11,996.09 4.12 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 10,269.54 10,742.43 733.13 5,736.18 5.36 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 733.13 18,714.09 8,590.01 9,601.19 3.29 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 7,402.05 7,826.93 733.13 3,860.34 4.89 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 733.13 10,742.43 5,722.52 5,736.18 2.99 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W 10 4,637.63 8,984.69 4,637.63 4,673.84 2.65 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W 10 4,637.63 8,984.69 4,637.63 4,673.84 2.65 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W9 733.13 10,742.43 5,722.52 5,736.18 2.99 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 7,402.05 7,826.93 733.13 3,860.34 4.89 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 733.13 18,714.09 8,590.01 9,601.19 3.29 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 10,269.54 10,742.43 733.13 5,736.18 5.36 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 733.13 24,373.24 11,457.51 11,996.09 4.12 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 13,044.87 14,381.54 733.13 7,464.59 5.86 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 568.23 16,730.22 9,920.38 10,368.99 4.23 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W2 17,775.68 18,714.09 1,042.10 9,160.58 6.80 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V1 586.10 4,802.89 1,672.63 2,725.35 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 87.09 4,802.89 2,344.80 3,025.24 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:31:16 PM NEW M I L L E N N I U M Location: Joist Description: Mark: AlIII MIND s,.z*FMS TIGARD,OR Long Span 24LH386/260 J53 TCX Design TCX Left TCX Right TCX Length 0-5 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-5 1/2 BPL Length 2-5 3/4 Clear Bearing 1-2 7/8 Clear Bearing 0-8 7/8 BPL Material:2024=2 x 2 x .248 BPL Material:2024=2 x 2 x.248 Total Load 386.00 Total Load 386.00 Reqd TL Def L/80 0.06 Reqd TL Def U80 0.00 Live Load 260.00 Live Load 260.00 Reqd LL Def U120 0.04 Reqd LL Def L/120 0.00 Section Modulus 8.5484 Section Modulus 8.5484 Reqd SM 0.0263 Reqd SM 0.0000 Mom of Inertia 28.8089 Mom of Inertia 28.8089 Reqd MI 0.0038 Reqd MI 0.0000 Seat Type:Pegged or Butted(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 STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/20181:49:25 PM NEW MILLENNIUM Location: Joist Description: Mark: n',,,o"`r; '''' s TIGARD,OR Long Span 24LH386/260 J54 Geometry . ._... .. ... ..__ Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 35-91/2 35-51/2 24.00 22.00 8 Special Parallel Chords Variable Left End Right End BC Panel 3-6 2-9 1/2 11I111111IIf111111111IIIII IIII ILI [III4p jTr MTCI17 III 'ITIry11Tirilifur 11J TC Panel 2-6 2-0 �. �� 1 First Half 1-0 0-6 First Diag. 4-6 3-3 1/2 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 35-9 1/2 L-BL Uniform (plf) LL (1) 260.00 260.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) CL(1) 416.00 416.00 TC + 0-0 35-9 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 Additional Shear(Ibs) LL (1) 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 Axial (Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) DL(1) 84.00 84.00 BC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 38.00 38.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) IP (1) 60.00 60.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) SM(1) 21.00 21.00 TC + 0-0 35-9 1/2 L-BL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 5-3 5-3 L-OAL Conc Load (Ibs) LL(1) 10,000.00 0.00 TC + 10-0 1/2 10-0 1/2 L-OAL Conc Load(Ibs) LL (1) 3,125.00 0.00 TC + 10-7 10-7 L-OAL Conc Load (Ibs) LL(1) 10,000.00 0.00 TC - 11-1 1/2 11-1 1/2 L-OAL Conc Load (Ibs) CL(1) 2,800.00 0.00 TC + 15-3 15-3 L-OAL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 16-5 16-5 L-OAL Conc w/bending (Ibs) CL(1) 2,800.00 0.00 TC + 26-0 26-0 L-OAL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 35-9 1/2 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) LL(3) 260.00 260.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(3) 84.00 84.00 BC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(3) 126.00 126.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) CL(3) 416.00 416.00 TC + 0-0 35-9 1/2 L-BL Axial(Ibs) SM(3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL(3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) SM (3) 3,500.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) IP(3) 60.00 60.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) SM (3) 21.00 21.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(3) 35.00 35.00 TC + 0-0 35-9 1/2 L-BL Axial (Ibs) WL(3) ' 3,000.00 0.00 BC + 0-0 0-0 L-BL Additional Shear (Ibs) LL(3) 500.00 0.00 TC + 0-0 0-0 L-BL Conc Load (Ibs) CL(3) 3,000.00 0.00 TC + 5-3 5-3 L-OAL Continued on Next Page... STRESS ANALYSIS- PAGE 1 110 Job Number: Job Name: Date Run: 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/20181:49:25 PM NEW M I L L EN N I UM Location: Joist Description: Mark: RI III MINIM RVRTRM6 TIGARD,OR Long Span 24LH386/260 J54 Loads, Continued... Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Conc Load (Ibs) LL(3) 10,000.00 0.00 TC - 10-0 1/2 10-0 1/2 L-OAL Conc Load (Ibs) LL(3) 3,125.00 0.00 TC + 10-7 10-7 L-OAL Conc Load (Ibs) LL(3) 10,000.00 0.00 TC + 11-1 1/2 11-1 1/2 L-OAL Conc Load (Ibs) CL(3) 2,800.00 0.00 TC + 15-3 15-3 L-OAL Conc Load (Ibs) CL(3) 3,000.00 0.00 TC + 16-5 16-5 L-OAL Conc w/bending (Ibs) CL(3) 2,800.00 0.00 TC + 26-0 26-0 L-OAL Stress Analysis Summary int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 33.00 51.00 25,358.16 22,189.55 6,339.54 126,102.97 127,802.61 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,084.27 44,816.53 0.00 0.00 51,625.79 1,237.40 45.65 0-2 V1S 1,041.72 43,847.27 0.00 0.00 611.88 2,864.42 25.06 2-6 W3 1,041.72 43,847.27 55,579.24 4,324.44 590.35 26,122.72 25.06 3-6 W4 1,811.34 75,484.34 55,579.24 4,324.44 28,315.72 724.84 32.56 4-6 V2 1,811.34 75,484.34 55,579.24 4,324.44 94.56 3,372.42 22.00 6-6 W5 1,811.34 75,484.34 98,664.33 5,352.56 650.43 28,762.33 39.66 6-6 W6 2,585.16 111,019.45 98,664.33 5,352.56 25,248.36 8,254.61 28.42 9-3 V3 2,585.16 111,019.45 98,664.33 5,352.56 5,851.57 11,547.17 22.00 10-9 W7 2,585.16 111,019.45 118,857.51 5,800.69 2,332.15 12,915.35 30.41 10-9 W8 2,973.35 126,102.97 118,857.51 5,800.69 13,360.07 2,496.56 32.56 12-6 V4 2,973.35 126,102.97 118,857.51 5,800.69 86.87 5,887.85 22.00 14-6 W9 2,973.35 126,102.97 127,802.61 6,067.46 2,496.56 10,385.22 32.56 14-6 W10 3,083.01 124,711.63 127,802.61 6,067.46 9,382.67 9,382.67 32.56 16-6 V5 3,083.01 124,711.63 127,802.61 6,067.46 87.42 2,797.56 22.0018-6 W10 3,083.01 124,711.63 119,427.58 6,019.99 9,382.67 9,382.67 32.56 18-6 W9 2,878.43 112,317.04 119,427.58 6,019.99 2,496.56 10,385.22 32.56 20-6 V6 2,878.43 112,317.04 119,427.58 6,019.99 86.39 2,735.59 22.00 22-6 W8 2,878.43 112,317.04 103,013.41 5,658.30 13,360.07 2,496.56 32.56 22-6 W7 2,359.61 90,483.08 103,013.41 5,658.30. 405.16 17,737.00 32.56 24-6 V7 2,359.61 90,483.08 103,013.41 5,658.30 83.80 4,143.08 22.00 26-6 W6 2,359.61 90,483.08 74,104.84 4,982.37 22,956.55 511.72 32.56 26-6 W5 1,526.57 56,472.47 74,104.84 4,982.37 618.28 25,434.11 32.56 28-6 V8 1,526.57 56,472.47 74,104.84 4,982.37 79.63 2,453.50 22.00.30-6 W4 1,526.57 56,472.47 36,764.00 3,992.21 28,315.72 724.84 32.56 30-6 W3 842.46 31,470.10 36,764.00 3,992.21 569.06 21,258.80 22.80 32-6 V1S 842.46 31,470.10 0.00 0.00 544.64 2,123.69 23.96 33-9 1/2 W2 866.75 32,021.43 0.00 0.00 38,290.52 1,057.16 38.42,33-0 STRESS ANALYSIS- PAGE 2 0 Job Number: 5618 0007 Job Name: Date Run TIGARD HIGH SCHOOL-SHOPORDERS 10/24i2018 1:49:25 PM NEW NIILLENNIUN1 Location: Joist Description: Mark: BULL-111�01 4VSTEM4 TIGARD,OR Long Span 24LH386/260 J54 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 2.2897 1.0781 0.6883 1.8998 1.0018 2.6613 1.0000 3534=3 1/2 x 3 1/2 x.344 BC 2.2897 1.0781 0.6883 1.8998 1.0018 2.6613 1.0000 3534=3 1/2 x 3 1/2 x.344 Axial and Bendin 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 1,118.50 937.30 1,405.96 25-13/4 38-0 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 24.00 33.00 15.50 22.00 1.1250 Min Weld Len 2X: Bending Load 840.00 840.00 840.00 840.00 840.00 1.3588 Axial Load 44,816.53 43,847.27 126,102.97 31,470.10 32,021.43 Max Load Fillers TC: fa 9,786.55 9,574.89 27,537.01 6,872.10 6,992.49 133,456.02 Maximum K L/r 40.68 34.87 26.15 22.52 31.96 Max Load no Fillers TC: Fcr 44,301.76 45,746.99 47,561.25 48,180.00 46,401.18 129,926.73 Fa 26,581.05 27,448.20 28,536.75 28,908.00 27,840.71 223.9723.97Ryy: F'e 424,326.09 577,555.00 1,026,764.50 1,384,689.50 687,338.13 BCOALJRyy: Cm 0.9885 0.9917 0.9820 0.9975 0.9949 223.97 Panel Point Moment 5241.51 5241.51 3360.00 2899.48 2899.48 BC Stress: Mid Panel Moment 3845.21 1192.22 1680.00 1614.44 2797.95 0'93 Panel Point fb 2460.14 2460.14 1577.04 1360.89 1360.89 BCURz 74.0956 Mid Panel fb 723.73 224.39 316.20 757.75 526.62 TC Shear Stress: Fillers 0 0 0 0 0 11,450.71 Panel Point Stress 12,246.69 12,035.04 29,114.05 8,232.99 8,353.39 BC Shear Stress: Mid Panel Stress 0.3902 0.3556 0.9746 0.2603 0.2670 11,450.71 Web Design Member Web Tension Allow Tension Web Camp Allow Comp Weld Qty Material W2 51,625.79 56,109.09 1,237.40 43,745.85 14.02 x 0.248 2 2024=2 x 2 x.248 V1 S 611.88 5,758.64 2,864.42 3,475.06 2.14 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W3 590.35 31,265.52 26,122.72 27,973.00 11.35 x 0.155 2 1715= 1 3/4 x 1 3/4 x .155 W4 28,315.72 28,624.38 724.84 13,972.95 10.17 x 0.188 1 C40BA= 1.125 x 2.014 x.218 V2 94.56 5,758.64 3,372.42 3,769.64 2.52 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 650.43 37,711.59 28,762.33 30,148.34 11.88 x 0.163 2 2016=2 x 2 x .163 W6 25,248.36 28,624.38 8,254.61 15,437.67 9.07 x 0.188 1 C40BA= 1.125 x 2.014 x.218 V3 5,851.57 18,714.09 11,547.17 12,153.26 4.42 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W7 2,332.15 28,624.38 12,915.35 14,726.32 4.64 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W8 13,360.07 14,381.54 2,496.56 7,520.78 6.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V4 86.87 8,984.69 5,887.85 5,930.70 3.36 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W9 2,496.56 24,373.24 10,385.22 12,091.68 3.73 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W 10 9,382.67 18,714.09 9,382.67 9,674.79 3.59 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V5 87.42 4,802.89 2,797.56 3,059.20 2.45 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W10 9,382.67 18,714.09 9,382.67 9,674.79 3.59 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W9 2,496.56 24,373.24 10,385.22 12,091.68 3.73 x 0.188 1 C38BA= 1.125 x 1.845 x .199 V6 86.39 4,802.89 2,735.59 3,059.20 2.39 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W8 13,360.07 14,381.54 2,496.56 7,520.78 6.00 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 405.16 23,649.64 17,737.00 18,862.49 8.72 x 0.137 2 1513 = 1 1/2 x 1 1/2 x.137 *Continued on Next Page... STRESS ANALYSIS - PAGE 2 ' Job Number: Job Name: Date Run: �/! 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/20181:49:25 PM NEW MILLENNIUM Location: Joist Description: Mark: 91,1I nitir SYSTEMS TIGARD,OR Long Span 24LH386/260 J54 Web Design Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 83.80_ 7,826.93 4,143.08 4,991.37 2.74 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 22,956.55 24,373.24 511.72 12,091.68 8.25 x 0.188 1 _C38BA= 1.125 x 1.845 x .199 W5 618.28 31,265.52 25,434.11 26,205.67 11.05 x 0.155 2 1715= 1 3/4 x 1 3/4 x.155 V8 79.63 4,802.89 2,453.50 3,059.20 2.15 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W4 28,315.72 28,624.38 724.84 13,972.95 10.17 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W3 569.06 26,592.28 21,258.80 23,834.47 9.24 x 0.155 2 1515= 1 1/2 x 1 1/2 x.155 V1S 544.64 4,802.89 2,123.69 2,890.53 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W2 38,290.52 43,216.97 1,057.16 36,315.48 13.75 x 0.188 2 2018=2 X 2 X.188 STRESS ANALYSIS- PAGE 3 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/20181:49:25 PM NEW MILLENNIUM Location: Joist Description: Mark: TIGARD,OR Long Span 24LH386/260 J54 TCX Design TCX Left TCX Right TCX Length 0-5 TCX Length 0-0 TCX Type S TCX Type R TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 0-6 BPL Length 0-6 Clear Bearing 0-9 5/8 Clear Bearing 0-8 1/8 BPL Material:2024=2 x 2 x.248 BPL Material:2024=2 x 2 x.248 Total Load 386.00 Total Load 386.00 Reqd TL Def U80 _ 0.06 Reqd TL Def U80 0.00 Live Load 260.00 Live Load 260.00 Reqd LL Def L/120 0.04 Reqd LL Def U120 0.00 Section Modulus 2.1306 Section Modulus 0.0000 Reqd SM 0.0263 Reqd SM 0.0000 Mom of Inertia 5.3226 Mom of Inertia 0.0000 Reqd MI 0.0038 Reqd MI 0.0000 Seat Type:T-Plate Seal Type:T-Plate 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)+W L-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 10/24/2018 9:04:11 AM NEW M I L L E N N I UNt Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 20LH444/300 J8 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 28-1 3/4 27-9 3/4 1 20.00 , 18.84 5 0 4-0 Parallel Chords 1 Variable Left End Right End BC Panel 3-11 3/4 4-2 TC Panel 3 0 3-2 '�� �\ j „'�� �� First Half 2-0 2-0 t-rf 11 Ill I I N.. 11 1 1 1 11 I f t_1'(l 111 1 11 I'N.i�f 1 11 1 1 1 i'Hull 11 I I I I ft First Diag. 5-11 3/4 6-2 Depth 20.00 20.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-1 3/4 L-BL Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-1 3/4 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 BC + 0-0 0-0 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-1 3/4 L-BL Additional Shear(Ibs) LL(1) 700.00 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) 24.00 24.00 TC + 0-0 28-1 3/4 L-BL Uniform (plf) _ DL(1) 96.00 96.00 BC + 0-0 28-1 3/4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-1 3/4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-1 3/4 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 _0-0 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-1 3/4 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 8,934.75 8,982.48 2,245.62 40,667.42 41,291.26 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,273.84 21,202.36 0.00 0.00 23,171.17 1,933.96 49.48 0-2 V1S 1,197.71 20,209.97 0.00 0.00 150.23 2,886.23 22.20 3-0 W3 1,197.71 20,209.97 27,880.60: 4,710.46 1,192.62 11,281.10 30.51 3-11 3/4 W4 2,090.00 33,814.84 27,880.60 4,710.46 8,970.81 1,192.62 30.51 5-113/4 W5 2,090.00 33,814.84 37,864.96 5,362.54 1,192.62 6,492.95 30.51 7-113/4 W6 2,528.07 40,520.17 37,864.96 5,362.54 4,636.99 1,192.62 30.51 9-113/4 W7 2,528.07 40,520.17 41,291.26 5,586.58 1,192.62 3,636.82 30.51 11-113/4 W7 2,538.10 40,667.42 41,291.26 5,586.58 1,192.62 3,636.82 30.51 13-113/4 W6 2,538.10 40,667.42 38,159.49 5,382.60 4,636.99 1,192.62 30.51 15-113/4 W5 2,240.91 34,256.63 38,159.49 5,382.60 1,192.62 6,492.95 30.51 17-113/4 W4 2,240.91 34,256.63 28,469.65 4,750.58 8,970.81 1,192.62 30.51 19-113/4 W3 1,717.72 20,939.02 28,469.65 4,750.58 1,192.62 11,281.10 30.51 21-113/4 V1S 1,717.72 20,939.02 0.00 0.00 1,233.92 2,970.74 22.34 24-11 3/4 W2 2,082.45 21,985.22 0.00 0.00 23,982.72 2,740.03 51.56 23-11 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.69 2,045.79 18.84 STRESS ANALYSIS- PAGE 2 //� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:04:11 AM NEW PAIL L E N N I U M Location: Joist Description: Mark: Al ilt nttin SYSTffMs TIGARD,OR Long Span 20LH444/300 J8 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 501.22 751.83 17-11/4 22-55/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 34.00 35.75 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 21,202.36 20,209.97 40,667.42 20,939.02 21,985.22 Max Load Fillers TC: fa 6,435.88 10,859.74 21,852.46 11,251.49 6,673.51 50,573.97 Maximum K L/r 86.91 91.39 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 28,781.03 27,150.58 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 17,268.62 16,290.35 25,697.63 16,151.33 16,151.33 255.85 55.85 yy: Fe 298,903.69 83,112.33 327,847.97 81,962.00 266,614.72 BCOAURyy: Cm 0.9892 0.9347 0.9553 0.9314 0.9875 258.89 Panel Point Moment 5890.23 5890.23 2292.00 4378.83 20249.96 BC Stress: Mid Panel Moment 4169.83 2778.38 1146.00 3364.69 13307.27 0'96 BC Panel Point fb 2382.30 12017.57 4676.26 8933.94 8190.10 121.88 21.8893 Mid Panel fb 1458.88 2377.67 980.72 2879.43 5382.13 TC Shear Stress: Fillers 0 0 0 0 0 10,676.98 Panel Point Stress 8,818.18 22,877.30 26,528.72 20,185.43 14,863.61 BC Shear Stress: Mid Panel Stress 0.4170 0.7509 0.8816 0.7997 0.5775 14,014.70 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 23,171.17 25,761.95 1,933.96 10,068.69 8.32 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W3 1,192.62 24,373.24 11,281.10 12,698.97 4.05 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W4 8,970.81 10,742.43 1,192.62 6,045.24 4.68 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W5 1,192.62 14,381.54 6,492.95 7,876.57 2.92 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W6 4,636.99 4,802.89 1,192.62 2,184.64 4.06 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W7 1,192.62 7,826.93 3,636.82 4,091.27 2.40 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,192.62 7,826.93 3,636.82 4,091.27 2.40 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W6 4,636.99 4,802.89 1,192.62 2,184.64 4.06 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W5 1,192.62 14,381.54 6,492.95 7,876.57 2.92 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 8,970.81 10,742.43 1,192.62 6,045.24 4.68 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,192.62 24,373.24 11,281.10 12,698.97 4.05 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 23,982.72 25,761.95 2,740.03 9,511.41 8.61 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1 1,233.92 5,758.64 2,970.74 3,742.51 2.22 x 0.090 1 C12BB= 1.125 x 0.799 x.090 V2 96.69 4,802.89 2,045.79 3,292.50 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 10/24/2018 9:04:11 AM NEW N{I L L E N N I U M Location: Joist Description: Mark: Rt11l.t]INC; GVSTFM4 TIGARD,OR Long Span 20LH444/300 J8 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 2-4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-4 7/8 BPL Length 5-10 7/8 Clear Bearing 1-0 3/4 Clear Bearing 1-1 1/2 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 444.00 Total Load 540.00 Reqd TL Def L/80 0.00 Reqd TL Def U80 0.35 Live Load 300.00 Live Load 300.00 Reqd LL Def U120 0.00 Reqd LL Def U180 0.16 Section Modulus 2.4725 Section Modulus 2.4725 Reqd SM 0.0000 Reqd SM 0.6750 Mom of Inertia 3.9771 Mom of Inertia 3.9771 Reqd MI 0.0000 Reqd MI 0.5237 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+W L-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: 5618-0007 Job Name: Date Run TIGARD HIGH SCHOOL-SHOPORDERS 10/24;;2018 9:06:10 AM NEW MILLENNIUM Location: Joist Description: Mark: aME, IING SYSTEMS TIGARD,OR Long Span 20LH444/300 J9 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 28-1 3/4 27-9 3/4 20.00 18.84 5 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-11314 4-2 IIWIIIILI_illlllttllil_Illilll�lILJIITJII1IliLI IUIIIJIIIIIIIIIII!IIIIIII1JII111l111, . TC Panel 3-0 3-2 < ---, First Half 2-0 2-0 �JkfITTTI I II TT IXITITTT['1171:1>`TTTTM i ,11, TTTTITT'TT1fH11Tl TTTTTE/ First Diag. 5-11 3/4 6-2 Depth 20.00 20.00 Loads Load Type Category Load1 Load2 Position Direction I Loc/Begin Sp/End Reference Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-1 3/4 L-BL Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-1 3/4 L-BL Uniform (plf) SL(1) 110.00 110.00 TC + 0-0 28-1 3/4 L-BL Uniform (plf) IP(1) 66.00 66.00 TC + 0-0 28-1 3/4 L-BL Uniform (plf) SL(1) 114.00 114.00 TC + 0-0 28-1 3/4 L-BL Conc @ any pp(Ibs) SM (1) 200.00 0.00 TC + 14-0 7/8 0-0 L-BL Additional Shear(Ibs) LL (1) 700.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(Ibs) CL(1) 100.00 0.00 TC + 14-0 7/8 0-0 L-BL Uniform (plf) SM (1) 24.00 24.00 TC + 0-0 28-1 3/4 L-BL Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 28-1 3/4 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-1 3/4 L-BL Conc @ any pp(Ibs) WL(1) 200.00 0.00 TC + 14-0 7/8 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) 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) 20.00 20.00 TC + 0-0 28-1 3/4 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-1 3/4 L-BL Conc @ any pp(Ibs) SM (2) 200.00 0.00 TC - 14-0 7/8 0-0 L-BL Conc @ any pp(Ibs) WL (2) 200.00 0.00 TC - 14-0 7/8 0-0 L-BL Axial (Ibs) WL (2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Stress Analysis Summary lnt.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 9,032.95 9,081.58 2,270.40 41,622.86 42,391.00 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,516.68 21,505.90 0.00 0.00 23,429.06 1,893.40 49.48 0-2 V1S 1,440.55 20,513.52 0.00 0.00 385.94 3,004.09 22.20 3-0 W3 1,440.55 20,513.52 28,343.38 5,080.69 902.81 11,406.58 30.51 3-113/4 W4 2,587.62 34,436.86 28,343.38 5,080.69 9,096.29 733.47 30.51 5-113/4 W5 2,587.62 34,436.86 38,646.22 5,987.55 553.66 6,596.54 30.51 7-113/4 W6 3,280.47 41,460.67 38,646.22 5,987.55 4,740.58 417.62 30.51 9-113/4 W7 3,280.47 41,460.67 42,391.00 6,466.38 804.90 3,676.94 30.51 11-113/4 W7 3,302.44 41,622.86 42,391.00 6,466.38 804.90 3,676.94 30.51 13-113/4 j W6 3,302.44 41,622.86 38,955.68 6,019.55 4,740.58 417.62 30.51 15-113/4 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 �/� Job Number: Job Name. Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:06:10 AM NEW MILLENNIUM Location: Joist Description: Mark: a(,.E cowl sys.FMs TIGARD,OR Long Span 20LH444/300 J9 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W5 2,629.66 34,893.58 38,955.68 6,019.55 553.66 6,596.54 30.51 17-113/4 W4 2,629.66 34,893.58 28,947.37 5,132.76 9,096.29 733.47 30.51 19-113/4 W3 1,908.80 21,257.50 28,947.37 5,132.76 902.81 11,406.58 30.51 21-113/4 V1S 1,908.80 21,257.50 0.00 0.00 867.18 3,089.30 22.34 24-11 3/4 W2 2,273.54 22,303.69 0.00 0.00 24,253.95 2,643.97 51.56 23-11 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 296.69 2,145.79 18.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run.- �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:06:10 AM NEW MILLENNIUM Location: Joist Description: Mark: SIM ruNr sVsTEMS TIGARD,OR Long Span 20LH444/300 J9 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024-2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 501.22 751.83 17-11/4 20-105/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 34.00 35.75 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 21,505.90 20,513.52 41,622.86 21,257.50 22,303.69 Max Load Fillers TC: fa 6,528.02 11,022.85 22,365.86 11,422.62 6,770.18 50,573.97 Maximum K Ur 86.91 91.39 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 28,781.03 27,150.58 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 17,268.62 16,290.35 25,697.63 16,151.33 16,151.33 255.85 55.85 yy: F'e 298,903.69 83,112.33 327,847.97 81,962.00 266,614.72 BCOAURyy: Cm 0.9891 0.9337 0.9543 0.9303 0.9873 258.89 Panel Point Moment 5890.23 5890.23 2292.00 4378.83 20249.96 BC Stress: Mid Panel Moment 4169.83 2778.38 1146.00 3364.69 13307.27 0.99 Panel Point fb 2382.30 12017.57 4676.26 8933.94 8190.10 BC URz: 121.8893 Mid Panel fb 1458.88 2377.67 980.72 2879.43 5382.13 TC Shear Stress: j Fillers 0 0 0 0 0 10,797.73 j Panel Point Stress 8,910.32 23,040.42 27,042.12 20,356.56 14,960.28 BC Shear Stress: Mid Panel Stress 0.4224 0.7611 0.9016 0.8107 0.5836 14,173.20 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 23,429.06 25,761.95 1,893.40 10,068.69 8.41 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 902.81 24,373.24 11,406.58 12,698.97 4.10 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 9,096.29 10,742.43 733.47 6,045.24 4.75 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W5 553.66 14,381.54 6,596.54 7,876.57 2.96 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W6 4,740.58 4,802.89 417.62 2,184.64 4.15 x 0.077 1 C10AB = 1.125 x 0.756 x.077 W7 804.90 7,826.93 3,676.94 4,091.27 2.43 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 804.90 7,826.93 3,676.94 4,091.27 2.43 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 4,740.58 4,802.89 417.62 2,184.64 4.15 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W5 553.66 14,381.54 6,596.54 7,876.57 2.96 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 9,096.29 10,742.43 733.47 6,045.24 4.75 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 902.81 24,373.24 11,406.58 12,698.97 4.10 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 24,253.95 25,761.95 2,643.97 9,511.41 8.71 x 0.188 1 C40BA= 1.125 x 2.014 x.218 V1 867.18 5,758.64 3,089.30 3,742.51 2.31 x 0.090 1 C12BB= 1.125 x 0.799 x.090 V2 296.69 4,802.89 2,145.79 3,292.50 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 10/24/2018 9:06:10 AM NEW MILLENNIUM Location: Joist Description: Mark; ar, ^�� sys*aMs TIGARD,OR Long Span 20LH444/300 J9 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 2-4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-4 7/8 BPL Length 5-10 7/8 Clear Bearing 1-0 3/4 Clear Bearing 1-1 1/2 BPL Material:2018=2 X 2 X .188 BPL Material:2018=2 X 2 X.188 Total Load 444.00 Total Load 540.00 Reqd TL Def L/80 0.00 Reqd TL Def U80 0.35 Live Load 300.00 Live Load 300.00 Reqd LL Def U120 0.00 Reqd LL Def U180 0.16 Section Modulus 2.4725 Section Modulus 2.4725 Reqd SM 0.0000 Reqd SM 0.6750 Mom of Inertia 3.9771 Mom of Inertia 3.9771 Reqd MI 0.0000 Reqd MI 0.5237 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)+W L+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: �J 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:22:23 AM NEW MILLENNIUM Location: Joist Description: Mark: M LL.01NG SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ11 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: i 28-4 28-0 20.00 18.84 5 @ 4-0 Parallel Chords Variable Left End Right End 1 BC Panel 4-2 4-2 - TT i{=F- T-t�fiTfFH-H ji- tI 11 T t T�t-T1TT TTHiji tftf TyTif-fTT-fT3l TC Panel 3-2 3-2 �.� ?�... / First Half 2-0 2-0 --- ‘-,J.TT_TTITIIiiii161111FTh1`ilil-T1717_LLIIFI.Lti1TTITLti -'(TTTT1Ii - First Diag. 6-2 6-2 Depth 20.00 20.00 j Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 L-BL Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 28-4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Axial (Ibs) SM(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) SM (1) 24.00 24.00 TC + 0-0 28-4 L-BL 'Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 L-BL Stress Analysis Summary Inf.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 8,982.00 9,237.55 2,309.39 41,109.22 41,148.43 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,310.80 22,132.48 0.00 0.00 22,231.54 8,045.79 51.56 0-2 V1S 2,812.07 21,086.29 0.00 0.00 3,825.71 2,141.56 22.34 3-2 W3 2,812.07 21,086.29 27,512.54 3,470.00 836.43 10,473.50 30.51 4-2 W4 4,027.62 34,551.15 27,512.54 3,470.00 8,153.54 708.89 30.51 6-2 W5 4,027.62 34,551.15 37,739.45 4,504.97 606.86 5,675.68 30.51 8-2 W6 4,902.08 41,109.22 37,739.45 4,504.97 3,819.72 504.84 30.51 10-2 W7 4,902.08 41,109.22 41,148.43 5,218.92 413.87 3,740.09 30.51 12-2 W7 5,455.51 41,109.21 41,148.43 5,218.92 413.87 3,740.09 30.51 14-2 W6 5,455.51 41,109.21 37,739.45 5,611.84 3,819.72 504.84 30.51 16-2 W5 5,687.92 34,551.15 37,739.45 5,611.84 606.86 5,675.68 30.51 18-2 W4 5,687.92 34,551.15 27,512.54 5,683.74 8,153.54 708.89 30.51 20-2 W3 5,579.24 21,086.29 27,512.54 5,683.74 836.43 10,473.50 30.51 22-2 V1S 5,579.24 21,086.29 0.00 0.00 3,825.71 2,141.56 22.34 25-2 W2 7,489.56 22,132.48 0.00 0.00 22,231.54 8,045.79 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.84 1,348.09 18.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:22:23 AM NEW IVIILLENNIUNI Location: Joist Description: Mark: At111 ent^+r SVSTF.MS TIGARD,OR Long Span 20LH444/300 TJ11 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 491.22 736.83 17-1 22-31/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 22,132.48 21,086.29 41,109.22 21,086.29 22,132.48 Max Load Fillers TC: fa 6,718.21 11,330.62 22,089.86 11,330.62 5,224.85 50,573.97 Maximum K L/r 92.02 92.02 46.01 92.02 92.02 Max Load no Firers TC: Fcr 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 257.58 57.58 yy: Fe 266,614.72 81,962.00 327,847.97 81,962.00 539,299.88 BCOAL/Ryy: Cm 0.9874 0.9309 0.9549 0.9309 0.9952 260.64 Panel Point Moment 29159.99 4605.39 2292.00 5218.23 115025.55 BC Stress: Mid Panel Moment 20605.21 3624.63 1146.00 4281.25 91838.84 "6 Panel Point fb 11793.76 9396.17 4676.26 10646.52 19730.13 BC uFz. 121.8893 Mid Panel fb 8333.78 3101.88 980.72 3663.79 15752.96 TC Shear Stress: Fillers 0 0 0 0 0 9897.37 Panel Point Stress 18,511.97 20,726.79 26,766.12 21,977.14 24,954.99 BC Shear Stress: Mid Panel Stress 0.6705 0.8128 0.8909 0.8329 0.7956 12,991.37 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 22,231.54 25,761.95 8,045.79 9,511.41 7.98 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W3 836.43 24,373.24 10,473.50 12,698.97 3.76 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W4 8,153.54 10,742.43 708.89 6,045.24 4.26 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W5 606.86 14,381.54 5,675.68 7,876.57 2.55 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W6 3,819.72 5,758.64 504.84 2,799.53 2.86 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W7 413.87 7,826.93 3,740.09 4,091.27 2.47 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W7 413.87 7,826.93 3,740.09 4,091.27 2.47 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W6 3,819.72 5,758.64 504.84 2,799.53 2.86 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W5 606.86 14,381.54 5,675.68 7,876.57 2.55 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W4 8,153.54 10,742.43 708.89 6,045.24 4.26 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W3 836.43 24,373.24 10,473.50 12,698.97 3.76 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 22,231.54 25,761.95 8,045.79 9,511.41 7.98 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1 3,825.71 4,802.89 2,141.56 3,034.97 3.35 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 96.84 4,802.89 1,348.09 3,292.50 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 10/24/2018 9:22:23 AM NEW MILLENNIUM Location: Joist Description: Mark: FULL-1ANC SVSTFMS TIGARD,OR Long Span 20LH444/300 TJ11 TCX Design TCX Left TCX Right TCX Length 2-10 TCX Length 5-9 1/2 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 6-4 7/8 BPL Length 9-5 Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material:2018=2 X 2 X.188 BPL Material:302025=3 x 2 x.250 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.43 Reqd TL Def L/80 0.87 Live Load 300.00 Live Load 300.00 Reqd LL Def L/180 0.19 Reqd LL Def U180 0.39 Section Modulus 2.4725 Section Modulus 4.6476 Reqd SM 0.9720 Reqd SM 3.8342 Mom of Inertia 3.9771 Mom of Inertia 10.3441 Reqd MI 0.9050 Reqd MI 7.0899 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(W L-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 rim Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/201810:10:20 AM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS. TIGARD,OR Long Span 20LH444/300 TJ12 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Pane!Length: Shape: 28-4 28-0 20.00 18.84 5 Q 4-0 Parallel Chords Variable Left End Right End BC Panel 4-2 4-2 tjlitflTifT illifJti(tf t tt ti tf[THf FFf Tfifffff tf I I II I I TC Panel 3-2 3-2 ��flfttf� tI III I l First Half 2-0 2-0 11fi lTTTTI t IECI ITTTT TTIII�TTTfTl71T3 ritrilimm ttTCI-f ITThIlt-- - First Diag. 6-2 6-2 Depth 20.00 ,20.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 L-BL Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 28-4 L-BL Uniform (plf) SM (1) 24.00 24.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 BC + 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 TC + 0-0 0-0 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Additional Shear(Ibs) LL(1) 700.00 0.00 TC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 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 8,982.00 9,237.55 2,309.39 41,109.22 41,806.68 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,310.80 22,132.48 0.00 0.00 24,147.46 8,045.79 51.56 0-2 V1S 2,812.07 21,086.29 0.00 0.00 3,825.71 2,971.50 22.34 3-2 W3 2,812.07 21,086.29 28,690.55 5,720.00 1,381.98 11,607.16 30.51 4-2 W4 4,027.62 34,551.15 28,690.55 5,720.00 9,287.21 1,381.98 30.51 6-2 W5 4,027.62 34,551.15 38,527.64 6,754.97 1,381.98 6,809.34 30.51 8-2 W6 4,902.08 41,109.22 38,527.64 6,754.97 4,953.38 1,381.98 30.51 10-2 W7 4,902.08 41,109.22 41,806.68 7,468.92 1,381.98 3,740.09 30.51 12-2 W7 5,455.51 41,109.21 41,806.68 7,468.92 1,381.98 3,740.09 30.51 14-2 W6 5,455.51 41,109.21 38,527.64 7,861.84 4,953.38 1,381.98 30.51 16-2 W5 5,687.92 34,551.15 38,527.64 7,861.84 1,381.98 6,809.34 30.51 18-2 W4 5,687.92 34,551.15 28,690.55 7,933.74 9,287.21 1,381.98 30.51 20-2 W3 5,579.24 21,086.29 28,690.55 7,933.74 1,381.98 11,607.16 30.51 22-2 V1S 5,579.24 21,086.29 0.00 0.00 3,825.71 2,971.50 22.34 25-2 W2 7,489.56 22,132.48 0.00 0.00 24,147.46 8,045.79 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.84 2,048.09 18.84 STRESS ANALYSIS - PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/201810:10:20 AM NEW MILLENNIUM Location: Joist Description: Mark: RIM ['ENE SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ12 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x .248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and BendingAnalysis K: Fy: FL': Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 491.22 736.83 17-1 18-101/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 22,132.48 21,086.29 41,109.22 21,086.29 22,132.48 Max Load Fillers TC: fa 6,718.21 11,330.62 22,089.86 11,330.62 5,224.85 50,573.97 Maximum K Ur 92.02 92.02 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 57.5URyy: _ 257.58 F'e 266,614.72 81,962.00 327,847.97 81,962.00 539,299.88 BCOALIRyy: Cm 0.9874 0.9309 0.9549 0.9309 0.9952 260•64 Panel Point Moment 29159.99 4605.39 2292.00 5218.23 115025.55 BC Stress: Mid Panel Moment 20605.21 3624.63 1146.00 4281.25 91838.84 0.97 BC Panel Point fb 11793.76 9396.17 4676.26 10646.52 19730.13 121 88: 121.8893 Mid Panel fb 8333.78 3101.88 980.72 3663.79 15752.96 TC Shear Stress: Fillers 0 0 0 0 0 10,750.33 Panel Point Stress 18,511.97 20,726.79 26,766.12 21,977.14 24,954.99 BC Shear Stress: Mid Panel Stress 0.6705 0.8128 0.8909 0.8329 0.7956 14,110.97 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 24,147.46 25,761.95 8,045.79 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 1,381.98 24,373.24 11,607.16 12,698.97 4.17 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 9,287.21 10,742.43 1,381.98 6,045.24 4.85 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 1,381.98 14,381.54 6,809.34 7,876.57 3.06 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 4,953.38 5,758.64 1,381.98 2,799.53 3.71 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 1,381.98 7,826.93 3,740.09 4,091.27 2.47 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,381.98 7,826.93 3,740.09 4,091.27 2.47 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 4,953.38 5,758.64 1,381.98 2,799.53 3.71 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 1,381.98 14,381.54 6,809.34 7,876.57 3.06 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 9,287.21 10,742.43 1,381.98 6,045.24 4.85 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,381.98 24,373.24 11,607.16 12,698.97 4.17 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 24,147.46 25,761.95 8,045.79 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1 3,825.71 4,802.89 2,971.50 3,034.97 3.35 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 96.84 4,802.89 2,048.09 3,292.50 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 10/24/201810:10:20 AM NEW MILLENNIUM Location: Joist Description: Mark: eiru.nwc SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ12 TCX Design TCX Left TCX Right TCX Length 2-10 TCX Length 5-9 1/2 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 6-4 7/8 BPL Length 9-5 Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material:2018=2 X 2 X.188 BPL Material: 302025=3 x 2 x.250 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.43 Reqd TL Def L/80 0.87 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.19 Reqd LL Def L/180 0.39 Section Modulus 2.4725 Section Modulus 4.6476 Reqd SM 0.9720 Reqd SM 3.8342 Mom of Inertia 3.9771 Mom of Inertia 10.3441 Reqd MI 0.9050 Reqd MI 7.0899 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) tLi 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(W L+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(W L-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 10/24/2018 9:27:08 AM NEW MILLENNIUM Location: Joist Description: Mark: ■LIILDING SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ14 Geometry Base Length: Working Length: Joist Depth Effective Depth: BC Panel Length: Shape: 28-4 28-0 20.00 18.84 5 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 4-2 4-2 TO Panel 3-2 3-2 . ., It FiFF1 t�i T f iFTIF TilTI IIItI ltllif fNFTfFFFTTTF {f - First Half 2-0 2-0 _ �GFrFTI TT ITI i ITT fT I T F1ILTTT I T TTfTil�"�l l Tt I TTTT YTTTTT[T7 %� First Diag. 6-2 6-2 Depth 20.00 '20.00 j Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference I' Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Axial(Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 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 Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 28-4 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) SM(1) 24.00 24.00 TC + 0-0 28-4 L-BL Additional Shear(Ibs) LL (1) 700.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Gross Uplift (plf) WL(2) 42.00 42.00 TC - 0-0 28-4 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 8,982.00 9,237.55 2,309.39 41,109.22 41,806.68 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,310.80 22,132.48 0.00 0.00 24,147.46 8,045.79 51.56 0-2 V1S 2,812.07 21,086.29 0.00 0.00 3,825.71 2,971.50 22.34 3-2 W3 2,812.07 21,086.29 28,690.55 5,720.00 1,381.98 11,607.16 30.51 4-2 W4 4,027.62 34,551.15 28,690.55 5,720.00 9,287.21 1,381.98 30.51 6-2 W5 4,027.62 34,551.15 38,527.64 6,754.97 1,381.98 6,809.34 30.51 8-2 W6 4,902.08 41,109.22 38,527.64 6,754.97 4,953.38 1,381.98 30.51 10-2 W7 4,902.08 41,109.22 41,806.68 7,468.92 1,381.98 3,740.09 30.51 12-2 W7 5,455.51 41,109.21 41,806.68 7,468.92 1,381.98 3,740.09 30.51 14-2 W6 5,455.51 41,109.21 38,527.64 7,861.84 4,953.38 1,381.98 30.51 16-2 W5 5,687.92 34,551.15 38,527.64 7,861.84 1,381.98. 6,809.34 30.51 18-2 W4 5,687.92 34,551.15 28,690.55 7,933.74 9,287.21 1,381.98 30.51 20-2 W3 5,579.24 21,086.29 28,690.55 7,933.74 1,381.98 11,607.16 30.51 22-2 V1S 5,579.24 21,086.29 0.00 0.00 3,825.71 2,971.50 22.34 25-2 W2 7,489.56 22,132.48 0.00 0.00 24,147.46 8,045.79 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.84 2,048.09 18.84 STRESS ANALYSIS- PAGE 2 �/� Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:27:08 AM NEW NI I L L E N N I U N% Location: Joist Description: Mark: A,t11 ninAn SVS*FEAB TIGARD,OR Long Span 20LH444/300 TJ14 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 491.22 736.83 17-1 18-101/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00, 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 22,132.48 21,086.29 41,109.22 21,086.29 22,132.48 Max Load Fillers TC: fa 6,718.21 11,330.62 22,089.86 11,330.62 5,224.85 50,573.97 Maximum K Ur 92.02 92.02 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 257.58 yy: 57.56 F'e 266,614.72 81,962.00 327,847.97 81,962.00 539,299.88 BCOAURyy: Cm 0.9874 0.9309 0.9549 0.9309 0.9952 260.E Panel Point Moment 29159.99 4605.39 2292.00 5218.23 115025.55 BC Stress: Mid Panel Moment 20605.21 3624.63 1146.00 4281.25 91838.84 0.97 Panel Point fb 11793.76 9396.17 4676.26 10646.52 19730.13 12188 21.8893 Mid Panel fb 8333.78 3101.88 980.72 3663.79 15752.96 TC Shear Stress: Fillers 0 0 0 0 0 10,750.33 Panel Point Stress 18,511.97 20,726.79 26,766.12 21,977.14 24,954.99 BC Shear Stress: Mid Panel Stress 0.6705 0.8128 0.8909 0.8329 0.7956 14,110.97 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 24,147.46 25,761.95 8,045.79 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 1,381.98 24,373.24 11,607.16 12,698.97 4.17 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W4 9,287.21 10,742.43 1,381.98 6,045.24 4.85 x 0.129 1 C22BB= 1.125 x 1.110 x .129 W5 1,381.98 14,381.54 6,809.34 7,876.57 3.06 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W6 4,953.38 5,758.64 1,381.98 2,799.53 3.71 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W7 1,381.98 7,826.93 3,740.09 4,091.27 2.47 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W7 1,381.98 7,826.93 3,740.09 4,091.27 2.47 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W6 4,953.38 5,758.64 1,381.98 2,799.53 3.71 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W5 1,381.98 14,381.54 6,809.34 7,876.57 3.06 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W4 9,287.21 10,742.43 1,381.98 6,045.24 4.85 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,381.98 24,373.24 11,607.16 12,698.97 4.17 x 0.188 1 C38BA- 1.125 x 1.845 x.199 W2 24,147.46 25,761.95 8,045.79 9,511.41 8.67 x 0.188 1 C4OBA- 1.125 x 2.014 x.218 V1 3,825.71 4,802.89 2,971.50 3,034.97 3.35 x 0.077 1 C10AB- 1.125 x 0.756 x.077 V2 96.84 4,802.89 2,048.09 3,292.50 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 10/24/2018 9:27:08 AM NEW MILLENNIUM Location: Joist Description Mark: F111!niniG SVSTF.MS TIGARD,OR Long Span 20LH444/300 TJ14 TCX Design TCX Left TCX Right TCX Length 2-10 TCX Length 5-9 1/2 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 6-4 7/8 BPL Length 9-5 Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material: 2018 =2 X 2 X.188 BPL Material: 302025=3 x 2 x.250 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.43 Reqd TL Def L/80 0.87 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.19 Reqd LL Def U180 0.39 Section Modulus 2.4725 Section Modulus 4.6476 Reqd SM 0.9720 Reqd SM 3.8342 Mom of Inertia 3.9771 Mom of Inertia 10.3441 Reqd MI 0.9050 Reqd MI 7.0899 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(W L+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 10/24/2018 9:37:30 AM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ15 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Pane!Length: Shape.' 28-4 28-0 20.00 18.53 5 Special Parallel Chords Variable Left End Right End 8C Panel 4-2 3-6 IIIlIllIIIllIlIIlIIIiIIiiIIIi A((TTTTITTTT TTT- I TTT TIllIt T1ITTTTIIITITIiiI!II TC Panel 3-2 3-2 " , i First Half 2-0 2-2 \\�r�trr rrrl Itx�i>T u u I l rT[Ir�rn l l nt hlltK I n u n>v�rr(r[rrlT�;./ First Diag. 6-2 5-8 Depth 20.00 20.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (pif) DL (1) 144.00 144.00 TC + 0-0 28-4 L-BL Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (pif) SM (1) 24.00 24.00 TC + 0-0 28-4 L-BL Uniform (plf) CL (1) 109.00 109.00 TC + 0-0 28-4 L-BL Additional Shear(Ibs) LL(1) 700.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL (1) 96.00 96.00 BC + 0-0 28-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 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 Conc Load (Ibs) LL(1) 5,000.00 0.00 TC + 22-3 1/4 22-3 1/4 L-OAL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 36.00 62.00 10,549.16 12,734.39 3,183.60 57,340.95 56,677.91 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,366.65 25,518.41 0.00 0.00 28,852.91 3,608.73 51.45 0-2 V1S 2,859.50 24,454.57 0.00 0.00 1,426.52 3,007.59 22.07 3-2 W3 2,859.50 24,454.57 34,066.87 5,778.53 845.19 13,875.10 30.32 4-2 W4 4,095.55 42,287.64 34,066.87 5,778.53 11,530.85 716.32 30.32 6-2 V2 4,095.55 42,287.64 34,066.87 5,778.53 94.88 2,057.44 18.53 8-2 W5 4,095.55 42,287.64 48,526.46 6,830.96 613.22 9,027.05 30.32 8-2 W6 4,984.76 53,280.77 48,526.46 6,830.96 7,151.65 3,696.43 30.32 10-2 V3 4,984.76 53,280.77 48,526.46 6,830.96 97.06 2,112.40 18.5312-2 W7 4,984.76 53,280.77 56,053.11 7,556.95 5,209.87 5,209.87 30.32 12-2 W7 5,547.53 57,340.95 56,053.11 7,556.95 5,209.87 5,209.87 30.32 14-2 V4 5,547.53 57,340.95 56,053.11 7,556.95 97.06 2,132.70 18.53 16-2 W6 5,547.53 57,340.95 56,677.91 7,956.50 7,151.65 3,696.43 30.32I16-2 W5 5,772.17 54,464.26 56,677.91 7,956.50 2,084.23 4,509.01 25.8318-2 V5 5,772.17 54,464.26 56,677.91 7,956.50 105.77 6,497.68 18.5319-8 W4 5,772.17 54,464.26 38,492.38 8,015.80 20,051.11 642.48 40.49 19-8 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 �/� Job Number: Name: Date Run: �f� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:37:30 AM NEW MILLENNIUM Location: Joist Description: Mark. auu_nndc BVSTFMS TIGARD,OR Long Span 20LH444/300 TJ15 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 5,656.74 24,745.82 38,492.38 8,015.80 705.64 18,526.22 31.93 22-8 V1S 5,656.74 24,745.82 0.00 0.00 3,300.51 2,453.62 18.95 25-2 W2 6,346.57 25,086.02 0.00 0.00 29,311.82 6,994.30 44.08 24-10 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:37:30 AM NEW MILLENNIUM Location: Joist Description: Mark: A„I,nitin SVSTFMS TIGARD,OR Long Span 20LH444/300 TJ15 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 1.0151 0.7748 0.4934 1.4841 0.7033 0.6093 0.9679 2521 =2 1/2 x 2 1/2 x.212 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 378.46 644.09 966.13 20-4 3/8 25-8 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 36.00 30.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5869 Axial Load 25,518.41 24,454.57 57,340.95 24,745.82 25,086.02 Max Load Fillers TC: fa 6,700.56 10,296.66 22,932.32 10,419.29 5,281.27 61,655.50 Maximum K Ur 74.80 74.80 56.10 62.33 74.80 Max Load no Fillers TC: 54 Fcr 33,213.52 33,213.52 39,722.73 37,635.57 33,213.52 ,279.00 Fa 19,928.11 19,928.11 23,833.64 22,581.34 19,928.11 TC oaURyy: 21s.1a re 263,307.09 142,085.50 252,596.48 204,603.13 485,197.63 BCOAL/Ryy: Cm 0.9873 0.9638 0.9392 0.9745 0.9946 226.40 Panel Point Moment 29159.99 5065.71 5157.00 7066.88 115025.58 BC Stress: Mid Panel Moment 20364.10 4117.84 2578.50 6701.99 90578.06 0.93 Panel Point fb 10309.09 6048.82 6157.82 8438.35 21755.95 125.6587 Mid Panel fb 7199.43 2074.01 1298.70 3375.56 17131.94 TC Shear Stress: Fillers 0 0 0 0 0 13,359.59 Panel Point Stress 17,009.65 16,345.48 29,090.14 18,857.64 27,037.22 BC Shear Stress: Mid Panel Stress 0.5562 0.5841 1.0048 0.5679 0.7792 13,340.89 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 28,852.91 29,969.07 3,608.73 7,021.91 5.61 x 0.245 1 R112 =round 1 1/8 V1 S 1,426.52 4,802.89 3,007.59 3,053.67 2.63 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W3 845.19 28,624.38 13,875.10 14,758.93 4.98 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W4 11,530.85 14,381.54 716.32 7,910.18 5.18 x 0.150 1 C28BB= 1.125 x 1.344 x .150 V2 94.88 4,802.89 2,057.44 3,316.48 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W5 613.22 18,714.09 9,027.05 10,184.69 3.45 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 7,151.65 7,826.93 3,696.43 4,110.27 4.72 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V3 97.06 4,802.89 2,112.40 3,316.48 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W7 5,209.87_ 10,742.43 5,209.87 6,070.36 2.72 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 5,209.87 10,742.43 5,209.87 6,070.36 2.72 x 0.129 1 C22BB= 1.125 x 1.110 x.129 V4 97.06 4,802.89 2,132.70 3,316.48 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W6 7,151.65 7,826.93 3,696.43 4,110.27 4.72 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 2,084.23 7,826.93 4,509.01 4,569.70 2.98 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V5 105.77 10,742.43 6,497.68 7,669.07 3.39 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W4 20,051.11 24,373.24 642.48 9,822.71 7.20 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 705.64 23,649.64 18,526.22 19,022.54 9.11 x 0.137 2 1513= 1 1/2 x 1 1/2 x.137 V1S 3,300.51 4,802.89 2,453.62 3,283.76 2.89 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W2 29,311.82 29,969.07 6,994.30 9,565.79 5.70 x 0.245 1 R112=round 1 1/8 STRESS ANALYSIS- PAGE 3 �,/� Job Number: Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:37:30 AM NEW MILLENNIUM Location: Joist Description: Mark: Ai III.,[]IWr: 4V4TFM4 TIGARD,OR Long Span 20LH444/300 TJ15 TCX Design TCX Left TCX Right TCX Length 2-10 TCX Length 5-9 1/2 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 6-5 BPL Length 9-3 3/8 Clear Bearing 1-3 1/8 Clear Bearing 1-0 7/8 BPL Material:2018=2 X 2 X.188 BPL Material:2525= 2 1/2 x 2 1/2 x.250 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.43 Reqd TL Def L/80 0.87 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.19 Reqd LL Def L/180 0.39 Section Modulus 2.8286 Section Modulus 5.1504 Reqd SM 0.9720 Reqd SM 3.8342 Mom of Inertia 4.5406 Mom of Inertia 10.4357 Reqd MI 0.9050 Reqd MI 7.0899 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 7 : DL+CL+0.85 TL +0.75 SM+AX+LL Case 4c: DL+WL+AX+IP g ( ) ( ) 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: j/i/ 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: ■u,Lo,wic SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ17 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 56-4 56-0 48.00 46.14 7 Special Parallel Chords Variable Left End Right End BC Panel 8-0 8-0 411 t1i41111 tall TC Panel 4-0 4-0 V \ ,V / ,,' First Half 0-10 0-10 �� 1111 1..41 11 1 I 4(I 1 1 1 111./1 1 I,I I' d1 1111 1 i4Xl 1 111 I(1t1 t i n t V First Diag. 8-10 8-10 Depth 48.00 48.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 180.00 180.00 TC + 0-0 56-4 L-BL Uniform (plf) LL(1) 370.00 370.00 TC + 0-0 56-4 L-BL Uniform (plf) IP (1) 84.00 84.00 TC + 0-0 56-4 L-BL Axial (lbs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 35.00 35.00 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) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) SM (1) 3,500.00 0.00 TC + 0-0 0-0 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 Conc Load (lbs) WL(1) 2,400.00 0.00 TC + 4-0 4-0 L-BL Conc Load (lbs) SM (1) 2,800.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 23-5 23-5 L-OAL Conc Load (lbs) LL(1) 10,000.00 0.00 TC + 26-5 1/2 26-5 1/2 L-OAL Conc Load (lbs) LL(1) 3,125.00 0.00 TC + 27-0 27-0 L-OAL Conc Load (Ibs) LL(1) 10,000.00 0.00 TC - 27-6 1/2 27-6 1/2 L-OAL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 34-7 34-7 L-OAL Conc Load (Ibs) WL(1) 2,400.00 0.00 TC + 4-0 4-0 R-BL Conc Load (lbs) SM(1) 2,800.00 0.00 TC + 4-0 4-0 R-BL 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 - 1-0 7-0 L-OAL Conc Load (Ibs) SM(2) 2,800.00 0.00 TC - 1-0 7-0 L-OAL Conc Load (Ibs) SM(2) 2,800.00 0.00 TC - 51-0 57-0 L-OAL Conc Load (Ibs) WL(2) 2,400.00 0.00 TC - 51-0 57-0 L-OAL Uniform (plf) LL (3) 370.00 370.00 TC + 0-0 56-4 L-BL Uniform (plf) SM (3) 30.00 30.00 TC + 0-0 56-4 L-BL Uniform (plf) IP (3) 84.00 84.00 TC + 0-0 56-4 L-BL Uniform (plf) DL(3) 180.00 180.00 TC + 0-0 56-4 L-BL Uniform (plf) DL(3) 35.00 35.00 TC + 0-0 56-4 L-BL Axial (Ibs) SM(3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL(3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL(3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(3) 120.00 120.00 BC + 0-0 56-4 L-BL Axial (Ibs) SM(3) 3,500.00 0.00 TC + 0-0 0-0 L-BL *Continued on Next Page... STRESS ANALYSIS- PAGE 1 /,/X Job Number: Job Name: Dale Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW Nt I L L E N N l LI M Location: Joist Description: Mark: AIM L t],NO Svs.FMs TIGARD,OR Long Span 48LH550/370 TJ17 Loads,Continued... Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Conc Load (Ibs) SM (3) 2,800.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) WL(3) 2,400.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) CL(3) 3,000.00 0.00 TC + 23-5 23-5 L-OAL Conc Load(Ibs) LL(3) 10,000.00 0.00 TC - 26-5 1/2 26-5 1/2 L-OAL Conc Load (Ibs) LL(3) 3,125.00 0.00 TC + 27-0 27-0 L-OAL Conc Load (Ibs) LL(3) 10,000.00 0.00 TC + 27-6 1/2 27-6 1/2 L-OAL Conc Load (abs) CL(3) 3,000.00 0.00 TC + 34-7 34-7 L-OAL Conc Load (Ibs) SM(3) 2,800.00 0.00 TC + 4-0 4-0 R-BL Conc Load (Ibs) WL(3) 2,400.00 0.00 TC + 4-0 4-0 R-BL 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 24,174.67 24,007.26 6,043.67 100,002.50 100,584.07 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 7,758.25 51,577.03 0.00 0.00 52,443.46 9,198.40 104.72 0-2 V1S 6,137.45 47,200.68 0.00 0.00 4,128.81 6,502.35 66.58 4-0 W3 6,137.45 47,200.68 47,561.37 6,625.13 2,302.60 20,158.62 47.22 8-0 W4 7,669.77 69,313.02 47,561.37 6,625.13 25,642.76 1,792.46 69.52 8-10 V2 7,669.77 69,313.02 47,561.37 6,625.13 480.35 2,478.71 46.14 13-2 W5 7,669.77 69,313.02 77,823.51 8,238.50 1,257.83 18,016.65 58.53 13-2 W6 8,680.86 88,827.47 77,823.51 8,238.50 15,790.74 1,240.42 58.53 16-2 V3 8,680.86 88,827.47 77,823.51 8,238.50 449.40 2,192.68 46.14 19-2 W7 8,680.86 88,827.47 95,318.73 8,996.82 1,240.42 12,651.63 58.53 19-2 W8 9,186.40 100,002.50 95,318.73 8,996.82 7,665.34 1,240.42 58.53 22-2 V4 9,186.40 100,002.50 95,318.73 8,996.82 3,902.30 9,356.92 46.14 25-2 W9 9,186.40 100,002.50 100,584.07 9,242.57 6,812.24 7,332.04 52.01 25-2 W9 9,186.40 98,914.10 100,584.07 9,242.57 1,411.19 8,720.59 66.58 27-2 V5 9,186.40 98,914.10 100,584.07 9,242.57 478.93 2,955.49 46.14 31-2 W8 9,186.40 98,914.10 94,041.66 8,996.82 7,665.34 1,240.42 58.53 31-2 W7 8,680.86 88,000.30 94,041.66 8,996.82 1,240.42 12,651.63 58.53 34-2 V6 8,680.86 88,000.30 94,041.66 8,996.82 449.40 2,187.17 46.14 37-2 W6 8,680.86 88,000.30 76,894.75 8,238.50 15,790.74 1,240.42 58.53 37-2 W5 7,669.77 68,747.05 76,894.75 8,238.50 1,257.83 18,016.65 58.53 40-2 V7 7,669.77 68,747.05 76,894.75 8,238.50 480.35 2,474.93 46.14 43-2 W4 7,669.77 68,747.05 47,058.29 6,625.13 25,642.76 1,792.46 69.52 43-2 W3 6,137.45 46,859.64 47,058.29 6,625.13 2,302.60 20,158.62 47.22 47-6 V1S 6,137.45 46,859.64 0.00 0.00 4,128.81 6,502.35 66.58 52-4 W2 7,758.25 51,236.00 0.00 0.00 52,443.46 9,198.40 104.72 48-4 STRESS ANALYSIS- PAGE 2 �/� Job Number: Job Name: Date Run: /// 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW NI I L L E N N I U M Location: Joist Description: Mark: NUR nimr: SVFMR TIGARD,OR Long Span 48LH550/370 TJ17 Chord Properties Chord Area Rx Rz Ryy Y Ix 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 1.7800 0.9216 0.5891 1.6993 0.8652 1.5119 1.0000 3031 =3 X 3 X.313 Axial and Bendin, 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 4,104.38 873.14 1,309.71 26-93/4 33-117/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.00 58.00 52.00 58.00 46.00 1.1250 Min Weld Len 2X: Bending Load 585.00 585.00 585.00 585.00 585.00 1.0658 Axial Load 51,577.03 47,200.68 100,002.50 46,859.64 51,236.00 Max Load Fillers TC: fa 12,321.32 11,275.84 23,629.74 11,194.37 12,239.85 110,272.38 Maximum K Ur 66.68 84.07 52.18 84.07 66.68 Max Load no Fillers TC: Fcr 35,808.61 29,634.50 40,549.95 29,634.50 35,808.61 98,891.67 Fa 21,485.17 17,780.70 24,329.97 17,780.70 21,485.17 rcoauayy: 354.99 F'e 158,473.86 99,682.13 258,742.78 99,682.13 158,473.86 BcoAL/Ryy: Cm 0.9611 0.9434 0.9388 0.9438 0.9614 395.45 Panel Point Moment 12698.34 13295.76 9360.00 13295.76 12698.34 BC Stress: Mid Panel Moment 5028.86 7502.33 4680.00 7502.33 5028.86 "4 Panel Point fb 6497.53 6803.22 4789.36 6803.22 6497.53 122.2203 Mid Panel fb 1015.64 1515.18 945.18 1515.18 1015.64 TC Shear Stress: Fillers 0 0 0 0 0 11,952.96 Panel Point Stress 18,818.85 18,079.06 28,419.10 17,997.59 18,737.38 BC Shear Stress: Mid Panel Stress 0.6072 0.6871 1.0026 0.6824 0.6033 13,969.47 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 52,443.46 56,109.09 9,198.40 16,948.74 14.24 x 0.248 2 2024=2 x 2 x.248 V1S 4,128.81 28,624.38 6,502.35 9,013.02 2.34 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 W3 2,302.60 31,265.52 20,158.62 21,961.75 8.76 x 0.155 2 1715= 1 3/4 x 1 3/4 x.155 W4 25,642.76 28,624.38 1,792.46 5,038.30 9.21 x 0.188 1 C40BA= 1.125 x 2.014 x.218 V2 480.35 7,826.93 2,478.71 2,666.11 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 1,257.83 31,265.52 18,016.65 18,331.46 7.83 x 0.155 2 1715= 1 3/4 x 1 3/4 x.155 W6 15,790.74 16,730.22 1,240.42 4,113.27 6.73 x 0.158 1 C32BA= 1.125 x 1.520 x.158 V3 449.40 7,826.93 2,192.68 2,666.11 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,240.42 26,592.28 12,651.63 12,925.39 5.50 x 0.155 2 1515= 1 1/2 x 1 1/2 x.155 W8 7,665.34 7,826.93 1,240.42 1,861.97 5.06 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V4 3,902.30 28,624.38 9,356.92 9,493.51 3.36 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W9 6,812.24 28,624.38 7,332.04 7,973.55 2.63 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W9 1,411.19 28,624.38 8,720.59 9,013.02 3.13 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 V5 478.93 8,984.69 2,955.49 3,239.61 2.00 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 7,665.34 7,826.93 1,240.42 1,861.97 5.06 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,240.42 26,592.28 12,651.63 12,925.39 5.50 x 0.155 2 1515= 1 1/2 x 1 1/2 x.155 V6 449.40 7,826.93 2,187.17 2,666.11 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W6 15,790.74 16,730.22 1,240.42 4,113.27 6.73 x 0.158 1 C32BA= 1.125 x 1.520 x .158 W5 1,257.83 31,265.52 18,016.65 18,331.46 7.83 x 0.155 2 1715= 1 3/4 x 1 3/4 x.155 Continued on Next Page... STRESS ANALYSIS- PAGE 2 ' Job Number: Job Name: Date Run: �/�/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: Buu.niNr. S„STFMS TIGARD,OR Long Span 48LH550/370 TJ17 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 480.35 7,826.93 2,474.93 2,666.11 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W4 25,642.76 28,624.38 1,792.46 5,038.30 9.21 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 2,302.60 31,265.52 20,158.62 21,961.75 8.76 x 0.155 2 1715= 1 3/4 x 1 3/4 x.155 V1S 4,128.81 28,624.38 6,502.35 9,013.02 2.34 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W2 52,443.46 56,109.09 9,198.40 16,948.74 14.24 x 0.248 2 2024=2 x 2 x.248 STRESS ANALYSIS- PAGE 3 �i4s Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: PIM clINr SVSTFMS TIGARD,OR Long Span 48LH550/370 TJ17 TCX Design TCX Left TCX Right TCX Length 0-10 TCX Length 0-10 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 0-10 1/2 Clear Bearing 0-10 1/2 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 U80 0.13 Reqd TL Def U80 0.13 Live Load 370.00 Live Load 370.00 Reqd LL Def U120 0.08 Reqd LL Def U120 0.08 Section Modulus 1.9543 Section Modulus 1.9543 Reqd SM 0.1100 Reqd SM 0.1100 Mom of Inertia 4.9044 Mom of Inertia 4.9044 Reqd MI 0.0276 Reqd MI 0.0276 Seat Type:T-Plate Seat Type:T-Plate 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 //A Job Number: Job Name: Date Run: ��/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ19 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 56-4 56-0 48.00 146.17 7 Special Parallel Chords Variable Left End Right End BC Panel 8-0 8-0 � ,.....E ,r �•aearr,mil, n,e6ee Tj r� I . n i ,rrn, , , � , ,..,,,_ TC Panel 4-0 4-0 w v, /vy /v 7N v / ",..--- First Half 0-10 0-10 �J1111 11111.1/ 111 11 I414(111[6 41 I 11111,14I 1 1114144111 l 4111 7 11 11 First Diag. 8-10 8-10 Depth 48.00 48.00 i Loads Load Type Category Load1 , Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 180.00 180.00 TC + 0-0 56-4 L-BL Uniform (plf) LL(1) 370.00 370.00 TO + 0-0 56-4 L-BL Axial (Ibs) SM(1) 3,500.00 0.00 TO + 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) 30.00 30.00 TC + 0-0 56-4 L-BL Uniform (plf) IP (1) 84.00 84.00 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) 35.00 35.00 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) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc Load (Ibs) SM (1) 2,800.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) WL(1) 2,400.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 5-2 5-2 L-OAL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 9-4 9-4 L-OAL Conc Load (Ibs) LL(1) 10,000.00 0.00 TC + 26-5 1/2 26-5 1/2 L-OAL Conc Load (Ibs) LL(1) 3,125.00 0.00 TC + 27-0 27-0 L-OAL Conc Load (Ibs) LL(1) 10,000.00 0.00 TC - 27-6 1/2 27-6 1/2 L-OAL Conc w/bending (Ibs) CL(1) 500.00 0.00 TC + 29-0 29-0 L-OAL Cone Load (Ibs) SM (1) 2,800.00 0.00 TC + 4-0 4-0 R-BL Conc Load (Ibs) WL(1) 2,400.00 0.00 TC + 4-0 4-0 R-BL 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 - 1-0 7-0 L-OAL Conc Load (Ibs) WL(2) 2,400.00 0.00 TC - 1-0 7-0 L-OAL Conc Load (Ibs) SM(2) 2,800.00 0.00 TO - 51-0 57-0 L-OAL Conc Load (Ibs) WL(2) 2,400.00 0.00 TC - 51-0 57-0 L-OAL Uniform (plf) DL(3) 180.00 180.00 TC + 0-0 56-4 L-BL Axial (Ibs) WL (3) 3,000.00 0.00 TO + 0-0 0-0 L-BL Axial (Ibs) SM(3) 3,500.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) LL(3) 370.00 370.00 TC + 0-0 56-4 L-BL Uniform (plf) SM (3) 30.00 30.00 TC + 0-0 56-4 L-BL Axial (Ibs) WL(3) 3,000.00 0.00 TO + 0-0 0-0 L-BL Uniform (plf) DL (3) 120.00 120.00 BC + 0-0 56-4 L-BL Uniform (plf) IP (3) 84.00 84.00 TC + 0-0 56-4 L-BL Axial (Ibs) SM (3) 3,000.00 0.00 TC + 0-0 0-0 L-BL *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW Nt I L L E N N I U Nt Location: Joist Description: Mark: RI III ^iN r SVGTFI.AS TIGARD,OR Long Span 48LH550/370 TJ19 Loads,Continued... Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL (3) 35.00 35.00 TC + 0-0 56-4 L-BL Conc Load (Ibs) WL(3) 2,400.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) SM (3) 2,800.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) CL (3) 3,000.00 0.00 TC + 5-2 5-2 L-OAL Conc Load (Ibs) CL (3) 3,000.00 0.00 TC + 9-4 9-4 L-OAL Conc Load (Ibs) LL(3) 10,000.00 0.00 TC - 26-5 1/2 26-5 1/2 L-OAL Conc Load (Ibs) LL(3) 3,125.00 0.00 TC + 27-0 27-0 L-OAL Conc Load (Ibs) LL(3) 10,000.00 0.00 TC + 27-6 1/2 27-6 1/2 L-OAL Conc w/bending (Ibs) CL(3) 500.00 0.00 TC + 29-0 29-0 L-OAL Conc Load (Ibs) SM(3) 2,800.00 0.00 IC + 4-0 4-0 R-BL Conc Load (Ibs) WL(3) 2,400.00 0.00 TC + 4-0 4-0 R-BL 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 26,755.02 21,926.90 6,688.76 89,498.96 89,860.09 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 7,754.72 56,809.63 0.00 0.00 58,277.70 9,195.03 104.72 0-2 V1S 6,134.66 49,316.03 0.00 0.00 4,127.84 10,854.80 66.60 4-0 W3 6,134.66 49,316.03 49,583.64 6,622.12 2,302.55 19,728.84 47.24 8-0 W4 7,666.28 67,475.59 49,583.64 6,622.12 22,166.51 1,792.00 69.54 8-10 V2 7,666.28 67,475.59 49,583.64 6,622.12 480.34 2,469.52 46.17 13-2 W5 7,666.28 67,475.59 73,313.51 8,234.76 1,257.61 15,092.38 58.54 13-2 W6 8,676.91 81,647.84 73,313.51 8,234.76 12,866.84 1,240.21 58.54 16-2 V3 8,676.91 81,647.84 73,313.51 8,234.76 449.39 2,156.78 46.17 19-2 W7 8,676.91 81,647.84 85,467.44 8,992.73 1,240.21 9,728.28 58.54 19-2 W8 9,182.22 89,498.96 85,467.44 8,992.73 8,482.07 1,240.21 58.54 22-2 V4 9,182.22 89,498.96 85,467.44 8,992.73 3,902.28 8,887.72 46.17 25-2 W9 9,182.22 89,498.96 89,860.09 9,238.37 7,538.63 7,456.87 52.03 25-2 W9 9,182.22 87,366.67 89,860.09 9,238.37 1,410.85, 9,649.13 66.60 27-2 V5 9,182.22 87,366.67 89,860.09 9,238.37 478.92 2,606.08 46.17 31-2 W8 9,182.22 87,366.67 82,102.20 8,992.73 8,482.07 1,240.21 58.54 31-2 W7 8,676.91 77,687.88 82,102.20 8,992.73 1,240.21 9,728.28 58.54 34-2 V6 8,676.91 77,687.88 82,102.20 8,992.73 449.39 2,135.60 46.17 37-2 W6 8,676.91 77,687.88 68,207.63 8,234.76 12,866.84 1,240.21 58.54 37-2 W5 7,666.28 61,687.95 68,207.63 8,234.76 1,257.61 15,092.38 58.54 40-2 V7 7,666.28 61,687.95 68,207.63 8,234.76 480.34 2,439.63 46.17 43-2 W4 7,666.28 61,687.95 42,350.30 6,622.12 22,166.51 1,792.00 69.54 43-2 W3 6,134.66 42,604.41 42,350.30 6,622.12 2,302.55 19,728.84 47.24 47-6 V1S 6,134.66 42,604.41 0.00 0.00 4,127.84 10,854.80 66.60 52-4 W2 7,754.72 46,978.78 0.00 0.00 58,277.70 9,195.03 104.72 48-4 STRESS ANALYSIS- PAGE 2 �,/, Job Number: Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description:. Mark: SUM MING 4V4TRMS TIGARD,OR Long Span 48LH550/370 TJ19 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 BendingAnalysis 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 26-87/8 33-101/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.00 58.00 52.00 58.00 46.00 1.1250 Bending Load 585.00 585.00 585.00 585.00 585.00 Min Weld Len 2X:0.9414 Axial Load 56,809.63 49,316.04 89,498.96 42,604.41 46,978.78 Max Load FiilersTC: fa 14,743.49 12,798.72 22,673.80 11,056.89 12,192.15 96,803.91 Maximum K Ur 66.53 83.89 52.07 83.89 66.53 Max Load no Fillers TC: Fcr 35,058.03 29,214.88 39,519.82 29,214.88 35,058.03 87,169.07 TC Fa 21,034.82 17,528.93 23,711.89 17,528.93 21,034.82 356.0456.04 yy: F'e 159,559.14 100,364.79 260,514.80 100,364.79 159,559.14 BCOAURyy: Cm 0.9538 0.9362 0.9417 0.9449 0.9618 397.16 Panel Point Moment 12698.34 13295.76 12735.00 13295.76 12698.34 BC Stress: Mid Panel Moment 5028.86 7502.33 6367.50 7502.33 5028.86 0.93 BC Panel Point fb 7037.28 7368.36 7057.60 7368.36 7037.28 121.889.813 3 Mid Panel fb 1085.50 1619.41 1374.45 1619.41 1085.50 TC Shear Stress: Fillers 0 0 0 0 0 14,477.48 Panel Point Stress 21,780.78 20,167.08 29,731.39 18,425.25 19,229.43 BC Shear Stress: Mid Panel Stress 0.7389 0.7899 1.0032 0.6889 0.6167 17,274.34 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 58,277.70 71,606.18 9,195.03 33,428.67 15.70 x 0.250 2 2525=2 1/2 x 2 1/2 x.250 V1S 4,127.84 28,950.00 10,854.80 14,457.69 5.11 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W3 2,302.55 28,950.00 19,728.84 19,940.76 9.29 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W4 22,166.51 24,373.24 1,792.00 4,396.78 7.96 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V2 480.34 7,826.93 2,469.52 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 1,257.61 28,950.00 15,092.38 16,748.06 7.11 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W6 12,866.84 14,381.54 1,240.21 3,647.35 5.78 x 0.150 1 C28BB= 1.125 x 1.344 x .150 V3 449.39 7,826.93 2,156.78 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W7 1,240.21 28,624.38 9,728.28 10,873.92 3.49 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W8 8,482.07 8,984.69 1,240.21 2,126.50 4.84 x 0.118 1 C18BB = 1.125 x 1.035 x.118 V4 3,902.28 28,624.38 8,887.72 9,487.38 3.19 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W9 7,538.63 28,624.38 7,456.87 7,969.28 2.71 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W9 1,410.85 26,592.28 9,649.13 10,448.75 4.19 x 0.155 2 1515= 1 1/2 x 1 1/2 x .155 V5 478.92 7,826.93 2,606.08 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W8 8,482.07 8,984.69 1,240.21 2,126.50 4.84 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 1,240.21 28,624.38 9,728.28 10,873.92 3.49 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 V6 449.39 7,826.93 2,135.60 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 12,866.84 14,381.54 1,240.21 3,647.35 5.78 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,257.61 28,950.00 15,092.38 16,748.06 7.11 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 'Continued on Next Page... STRESS ANALYSIS- PAGE 2 /� Job Number: Job Name: Date Run: �// 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24i2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: Bull rIltif: SVSTPFAS TIGARD,OR Long Span 48LH550/370 TJ19 Web Design Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 480.34 7,826.93 2,439.63 2,664.40 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W4 22,166.51 24,373.24 1,792.00 4,396.78 7.96 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 2,302.55 28,950.00 19,728.84 19,940.76 9.29 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 V 1 S 4,127.84 28,950.00 10,854.80 14,457.69 5.11 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W2 58,277.70 71,606.18 9,195.03 33,428.67 15.70 x 0.250 2 2525=2 1/2 x 2 1/2 x.250 STRESS ANALYSIS- PAGE 3 Job Number: Job Name. Date Run: 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: BUIL.OWr 6v8TFM5 TIGARD,OR Long Span 48LH550/370 TJ19 TCX Design TCX Left TCX Right TCX Length 0-10 TCX Length 0-10 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 7/8 Clear Bearing 0-8 7/8 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 0.13 Reqd TL Def U80 0.13 Live Load 370.00 Live Load 370.00 Reqd LL Def U120 0.08 Reqd LL Def L/120 0.08 Section Modulus 1.8044 Section Modulus 1.8044 Reqd SM 0.1100 Reqd SM 0.1100 Mom of Inertia 4.5452 Mom of Inertia 4.5452 Reqd MI 0.0276 Reqd MI 0.0276 Seat Type:T-Plate Seat Type:T-Plate 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)+W L+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 /�i� Job Number Job Name: Date Run: �i� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 8:38:05 AM NEW MILLENNIUM Location: Joist Description: Mark: BULL OINIS SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ2 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 28-4 28-0 20.00 18.84 5 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 4-2 4-2 1 TC Panel 3-2 3-2 First Half 2-0 2-0 ITII1 TI fITYtIfl IIIII LITIITTIITII TTTTTJ1 it 11 fT1TII 1 ICl'(lI[I I7fITIZ---- I First Diag. 6-2 6-2 Depth 20.00 20.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference 1 Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 L-BL Uniform (plf) LL (1) 300.00 300.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 28-4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Axial (Ibs) SM(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) SM(1) 24.00 24.00 TC + 0-0 28-4 L-BL Axial (lbs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 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 9,264.07 8,982.00 2,316.02 41,109.22 41,148.43 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 7,421.99 22,132.48 0.00 0.00 22,231.54 7,973.21 51.56 0-2 V1S 5,521.81 21,086.29 0.00 0.00 3,825.37 2,141.56 22.34 3-2 W3 5,521.81 21,086.29 27,512.54 5,597.60 872.94 10,516.45 30.51 4-2 W4 5,573.06 34,551.15 27,512.54 5,597.60 8,196.49 745.40 30.51 6-2 W5 5,573.06 34,551.15 37,739.45 5,468.27 643.37 5,718.63 30.51 8-2 W6 5,283.23 41,109.22 37,739.45 5,468.27 3,862.66 541.34 30.51 10-2 W7 5,283.23 41,109.22 41,148.43 5,017.92 2,050.34 3,750.83 30.51 12-2 W7 4,672.36 41,109.21 41,148.43 5,017.92 2,050.34 3,750.83 30.51 14-2 W6 4,672.36 41,109.21 37,739.45 4,246.55 3,862.66 541.34 30.51 16-2 W5 3,740.48 34,551.15 37,739.45 4,246.55 643.37 5,718.63 30.51 18-2 W4 3,740.48 34,551.15 27,512.54 3,154.15 8,196.49 745.40 30.51 20-2 W3 2,467.50 21,086.29 27,512.54 3,154.15 872.94 10,516.45 30.51 22-2 V1S 2,467.50 21,086.29 0.00 0.00 3,825.37 2,141.56 22.34 25-2 W2 2,832.24 22,132.48 0.00 0.00 22,231.54 7,973.21 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.84 1,348.09 18.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �// 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 8:38:05 AM NEW NtILLENNIunit Location: Joist Description: Mark: AIM_nttio SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ2 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 491.22 736.83 17-1 22-5 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 22,132.48 21,086.29 41,109.22 21,086.29 22,132.48 Max Load Fillers TC: fa 5,224.85 11,330.62 22,089.86 11,330.62 6,718.21 50,573.97 Maximum K Ur 92.02 92.02 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 257.5857.58 yy: F'e 539,299.88 81,962.00 327,847.97 81,962.00 266,614.72 BC OAURyy: Cm 0.9952 0.9309 0.9549 0.9309 0.9874 260.64 Panel Point Moment 115025.55 5218.23 2292.00 4378.83 20249.96 BC Stress: Mid Panel Moment 91838.84 4281.25 1146.00 3364.69 13307.27 0.96 BC Panel Point fb 19730.13 10646.52 4676.26 8933.94 8190.10 121.88 21.8893 Mid Panel fb 15752.96 3663.79 980.72 2879.43 5382.13 TC Shear Stress: Fillers 0 0 0 0 0 9,897.37 Panel Point Stress 24,954.99 21,977.14 26,766.12 20,264.56 14,908.31 BC Shear Stress: Mid Panel Stress 0.7956 0.8329 0.8909 0.8048 0.5803 12,991.37 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 22,231.54 25,761.95 7,973.21 9,511.41 7.98 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W3 872.94 24,373.24 10,516.45 12,698.97 3.78 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 8,196.49 10,742.43 745.40 6,045.24 4.28 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 643.37 14,381.54 5,718.63 7,876.57 2.57 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 3,862.66 5,758.64 541.34 2,799.53 2.89 x 0.090 1 C12BB = 1.125 x 0.799 x.090 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 3,862.66 5,758.64 541.34 2,799.53 2.89 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 643.37 14,381.54 5,718.63 7,876.57 2.57 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 8,196.49 10,742.43 745.40 6,045.24 4.28 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 872.94 24,373.24 10,516.45 12,698.97 3.78 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 22,231.54 25,761.95 7,973.21 9,511.41 7.98 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1 3,825.37 4,802.89 2,141.56 3,034.97 3.35 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 96.84 4,802.89 1,348.09 3,292.50 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 10/24/2018 8:38:05 AM NEW MILLENNIUM Location: Joist Description: Mark: Ar, ^lKin RV4TRM4 TIGARD,OR Long Span 20LH444/300 TJ2 TCX Design TCX Left TCX Right TCX Length 5-9 1/2 TCX Length 2-4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 9-5 BPL Length 5-10 7/8 Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material:302025=3 x 2 x .250 BPL Material:2018=2 X 2 X.188 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.87 Reqd TL Def L/80 0.35 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.39 Reqd LL Def U180 0.16 Section Modulus 4.6476 Section Modulus 2.4725 Reqd SM 3.8342 Reqd SM 0.6750 Mom of Inertia 10.3441 Mom of Inertia 3.9771 Reqd MI 7.0899 Reqd MI 0.5237 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(W L+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/� i Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark SLIILOING SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ21 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 8-0 8-0 , TC Panel 4-0 4-0 n� /� I ^� % �, First Half 0-10 0-10 Jilll l 1N 141 I I I L I xl11-111K41 I11 I I L d J I I I I IJ,1(I I I I I II I'f(I I I I16%" First Diag. 8-10 8-10 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) 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 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 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 (plf) DL(1) 35.00 35.00 TC + 0-0 56-4 L-BL Conc Load (Ibs) SM (1) 2,800.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) WL(1) 2,400.00 0.00 TC + 4-0 4-0 L-BL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 5-2 5-2 L-OAL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 9-4 9-4 L-OAL Conc Load (Ibs) CL(1) 500.00 0.00 TC + 29-0 29-0 L-OAL Conc Load (Ibs) WL (1) 2,400.00 0.00 TC + 4-0 4-0 R-BL Conc Load (Ibs) SM (1) 2,800.00 0.00 TC + 4-0 4-0 R-BL 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 - 1-0 7-0 L-OAL Conc Load (Ibs) SM (2) 2,800.00 0.00 TC - 1-0 7-0 L-OAL Conc Load (Ibs) WL(2) 2,400.00 0.00 TC - 51-0 57-0 L-OAL Conc Load (Ibs) SM (2) 2,800.00 0.00 TC - 51-0 57-0 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 25,354.35 20,693.64 6,338.59 80,378.45 77,412.95 Member IC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 7,752.84 53,945.64 0.00 0.00 55,089.55 9,193.23 104.73 0-2 V1S 6,133.17 46,453.86 0.00 0.00 4,127.32 10,839.15 66.61 4-0 W3 6,133.17 46,453.86 45,586.12 6,620.51 2,302.53 17,817.78 47.25 8-0 W4 7,664.42 62,728.37 45,586.12 6,620.51 19,687.06 1,791.76 69.54 8-10 W5 7,664.42 62,728.37 65,530.48 8,232.76 1,257.50 13,005.97 58.5513-2 W6 8,674.80 74,713.21 65,530.48 8,232.76 10,780.65 1,240.10 58.55 16-2 W7 8,674.80 74,713.21 74,769.51 8,990.55 1,240.10 8,037.28 58.55 19-2 W8 9,179.99 80,378.45 74,769.51 8,990.55 8,037.28 1,240.10 58.55 22-2 Continued on Next Page... STRESS ANALYSIS - PAGE 1 �/� Job Number: Job Name: Date Run: �j/i/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: 6lnl-^IN LI SVS*F,..14 TIGARD,OR Long Span 48LH55O370 TJ21 Stress Mali sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W9 9,179.99 80,378.45 77,412.95 9,243.14 5,598.30 8,037.28 58.55 25-2 W9 9,179.99 79,334.33 77,412.95 9,243.14 5,598.30 8,037.28 58.55 28-2 W8 9,179.99 79,334.33 72,681.25 8,990.55 8,037.28 1,240.10 58.55 31-2 W7 8,674.80 71,580.81 72,681.25 8,990.55 1,240.10 8,037.28 58.55 34-2 W6 8,674.80 71,580.81 61,353.96 8,232.76 10,780.65 1,240.10 58.55 37-2 W5 7,664.42 57,507.72 61,353.96 8,232.76 1,257.50 13,005.97 58.55 40-2 W4 7,664.42 57,507.72 38,857.28 6,620.51 19,687.06 1,791.76 69.54 43-2 W3 6,133.17 40,084.67 38,857.28 6,620.51 2,302.53 17,817.78 47.25 47-6 V1S 6,133.17 40,084.67 0.00 0.00 4,127.32 10,839.15 66.61 52-4 W2 7,752.84 44,457.98 0.00 0.00 55,089.55 9,193.23 104.73 48-4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 480.33 2,437.89 46.18 STRESS ANALYSIS- PAGE 2 �/� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: ALM nintr, SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ21 Chord Properties Chord Area Rx Rz Ryy Y Ix 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 Bendin 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 32-4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 46.00 58.00 52.00 58.00 46.00 1.1250 Min Weld Len 2X: Bending Load 585.00 585.00 585.00 585.00 585.00 0.8661 Axial Load 53,945.64 46,453.86 80,378.45 40,084.67 44,457.98 Max Load Fillers TC: fa 14,000.22 12,055.92 20,860.18 10,402.96 11,537.94 103,657.98 Maximum K L/r 66.53 83.89 39.05 83.89 66.53 Max Load no Fillers TC: Fcr 35,058.03 29,214.88 42,932.89 29,214.88 35,058.03 97,707.06 TC Fa 21,034.82 17,528.93 25,759.73 17,528.93 21,034.82 356.04 yy: 6.04 Fe 159,559.14 100,364.79 463,137.34 100,364.79 159,559.14 BCOALRyy: Cm 0.9561 0.9399 0.9698 0.9482 0.9638 398.81 Panel Point Moment 12698.34 13295.76 5265.00 13295.76 12698.34 BC Stress: Mid Panel Moment 5028.86 7502.33 2632.50 7502.33 5028.86 0.90 BC URz: Panel Point fb 7037.28 7368.36 2917.81 7368.36 7037.28 121.535395 Mid Panel fb 1085.50 1619.41 568.24 1619.41 1085.50 -" TC Shear Stress: Fillers 0 0 0 0 0 13,687.42 Panel Point Stress 21,037.50 19,424.28 23,777.99 17,771.32 18,575.22 BC Shear Stress: Mid Panel Stress 0.7033 0.7468 0.8283 0.6511 0.5854 18,334.76 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 55,089.55 56,109.09 9,193.23 16,944.15 14.96 x 0.248 2 2024=2 x 2 x.248 W3 2,302.53 28,950.00 17,817.78 19,937.76 8.39 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W4 19,687.06 24,373.24 1,791.76 4,396.00 7.07 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W5 1,257.50 28,950.00 13,005.97 16,745.54 6.12 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W6 10,780.65 14,381.54 1,240.10 3,646.46 4.84 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W7 1,240.10 28,624.38 8,037.28 10,871.78 2.89 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W8 8,037.28 8,984.69 1,240.10 2,125.86 4.59 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W9 5,598.30 28,624.38 8,037.28 10,871.78 2.89 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W9 5,598.30 28,624.38 8,037.28 10,871.78 2.89 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W8 8,037.28 8,984.69 1,240.10 2,125.86 4.59 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 1,240.10 28,624.38 8,037.28 10,871.78 2.89 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W6 10,780.65 14,381.54 1,240.10 3,646.46 4.84 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,257.50 28,950.00 13,005.97 16,745.54 6.12 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W4 19,687.06 24,373.24 1,791.76 4,396.00 7.07 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 2,302.53 28,950.00 17,817.78 19,937.76 8.39 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 W2 55,089.55 56,109.09 9,193.23 16,944.15 14.96 x 0.248 2 2024=2 x 2 x.248 V1 4,127.32 28,950.00 10,839.15 14,455.51 5.10 x 0.143 2 1714= 1 3/4 x 1 3/4 x.143 V2 480.33 7,826.93 2,437.89 2,663.49 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 STRESS ANALYSIS- PAGE 3 G� Job Number: Job Name: Date Run: 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 2:51:25 PM NEW MILLENNIUM Location: Joist Description: Mark: at m_eiNc SYSTEMS TIGARD,OR Long Span 48LH550/370 TJ21 TCX Design TCX Left TCX Right TCX Length 0-10 TCX Length 0-10 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 0-10 3/8 Clear Bearing 0-10 1/2 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 0.13 Reqd TL Def U80 0.13 Live Load 370.00 Live Load 370.00 Reqd LL Def L/120 0.08 Reqd LL Def U120 0.08 Section Modulus 1.8044 Section Modulus 1.8044 Reqd SM 0.1100 Reqd SM _ 0.1100 Mom of Inertia 4.5452 Mom of Inertia 4.5452 Reqd MI 0.0276 Reqd MI 0.0276 Seat Type:T-Plate Seat Type:T-Plate • 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)+W L-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 10/24/2018 9:11:28 AM NEW MILLENNIUM Location: Joist Description: Mark: aLJE_EENG SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ4 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: 28-4 28-0 20.00 18.84 5 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 4-2 4-2 - T I J fi TFrrf --FTff F HTJf f1 TC Panel 3-2 3-2 �� � First Half 2-0 2-0 ���� jJIL1 T I�•�fiI-T1T[T I f T 1'N1L1'I Lf Tm�;YfTLLLLTI]3;1L '- First Diag. 6-2 6-2 Depth 20.00 20.00 Loads Load Type Category _ Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 L-BL Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-4 L-BL Additional Shear(Ibs) LL(1) _ 700.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 28-4 L-BL Uniform (plf) SM (1) 24.00 24.00 TC + 0-0 28-4 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 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) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 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 9,264.07 8,982.00 2,316.02 41,109.22 41,806.68 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 7,421.99 22,132.48 0.00 0.00 24,147.46 7,973.21 51.56 0-2 V1S 5,521.81 21,086.29 0.00 0.00 3,825.37 2,971.50 22.34 3-2 W3 5,521.81 21,086.29 28,690.55 7,847.60 1,407.75 11,650.11 30.51 4-2 W4 5,573.06 34,551.15 28,690.55 7,847.60 9,330.15 1,407.75 30.51 6-2 W5 5,573.06 34,551.15 38,527.64 7,718.27 1,407.75 6,852.29 30.51 8-2 W6 5,283.23 41,109.22 38,527.64 7,718.27 4,996.32 1,407.75 30.51 10-2 W7 5,283.23 41,109.22 41,806.68 7,267.92 2,050.34 3,750.83 30.51 12-2 W7 4,672.36 41,109.21 41,806.68 7,267.92 2,050.34 3,750.83 30.51 14-2 W6 4,672.36 41,109.21 38,527.64 6,496.55 4,996.32 1,407.75 30.51 16-2 W5 3,740.48 34,551.15 38,527.64 6,496.55 1,407.75 6,852.29 30.51 18-2 W4 3,740.48 34,551.15 28,690.55 5,404.15 9,330.15 1,407.75 30.51 20-2 W3 2,467.50 21,086.29 28,690.55 5,404.15 1,407.75 11,650.11 30.51 22-2 V1S 2,467.50 21,086.29 0.00 0.00 3,825.37 2,971.50 22.34 25-2 W2 2,832.24 22,132.48 0.00 0.00 24,147.46, 7,973.21 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.84 2,048.09 18.84 STRESS ANALYSIS - PAGE 2 �/� Job Number: Job Name: Date Run: �// 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:11:28 AM NEW MILLENNIUM Location: Joist Description: Mark: AIM-mina: SVSTFM^. TIGARD,OR Long Span 20LH444/300 TJ4 Chord Properties Chord Area _ Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.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 30,000.00 288.64 491.22 736.83 17-1 18-111/2 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00_ 36.00 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 22,132.48 21,086.29 41,109.22 21,086.29 22,132.48 Max Load Fillers TC: fa 5,224.85 11,330.62 22,089.86 11,330.62 6,718.21 50,573.97 Maximum K Ur 92.02 92.02 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 257O 'Ryy: 57.58 F'e 539,299.88 81,962.00 327,847.97 81,962.00 266,614.72 BC OAL/Ryy: Cm 0.9952 0.9309 0.9549 0.9309 0.9874 260.64 Panel Point Moment 115025.55 5218.23 2292.00 4378.83 20249.96 BC Stress: Mid Panel Moment 91838.84 4281.25 1146.00 3364.69 13307.27 0.97 Panel Point fb 19730.13 10646.52 4676.26 8933.94 8190.10 BC Linz: 121.8893 Mid Panel fb 15752.96 3663.79 980.72 2879.43 5382.13 TC Shear Stress: Fillers 0 0 0 0 0 10,750.33 Panel Point Stress 24,954.99 21,977.14 26,766.12 20,264.56 14,908.31 BC Shear Stress: Mid Panel Stress 0.7956 0.8329 0.8909 0.8048 0.5803 14,110.97 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 24,147.46 25,761.95 7,973.21 9,511.41 8.67 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W3 1,407.75 24,373.24 11,650.11 12,698.97 4.18 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W4 9,330.15 10,742.43 1,407.75 6,045.24 4.87 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 1,407.75 14,381.54 6,852.29 7,876.57 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W6 4,996.32 5,758.64 1,407.75 2,799.53 3.74 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W6 4,996.32 5,758.64 1,407.75 2,799.53 3.74 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W5 1,407.75 14,381.54 6,852.29 7,876.57 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W4 9,330.15 10,742.43 1,407.75 6,045.24 4.87 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,407.75 24,373.24 11,650.11 12,698.97 4.18 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W2 24,147.46 25,761.95 7,973.21 9,511.41 8.67 x 0.188 1 C40BA= 1.125 x 2.014 x .218 V1 3,825.37 4,802.89 2,971.50 3,034.97 3.35 x 0.077 1 C10AB= 1.125 x 0.756 x .077 V2 96.84 4,802.89 2,048.09 3,292.50 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 10/24/2018 9:11:28 AM NEW Nt I L L E N N I U Nt Location: Joist Description: Mark: eun..n .in 5v51-FM9 TIGARD,OR Long Span 20LH444/300 TJ4 TCX Design TCX Left TCX Right TCX Length 5-9 1/2 TCX Length 2-4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 9-5 BPL Length 5-10 7/8 Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material:302025=3 x 2 x.250 BPL Material: 2018=2 X 2 X.188 Total Load 540.00 Total Load 540.00 Reqd TL Def L/80 0.87 Reqd TL Def L/80 0.35 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.39 Reqd LL Def U180 0.16 Section Modulus 4.6476 Section Modulus 2.4725 Reqd SM 3.8342 Reqd SM 0.6750 Mom of Inertia 10.3441 Mom of Inertia 3.9771 Reqd MI 7.0899 Reqd MI 0.5237 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 lid Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:32:06 PM NEW N1 I L L E N N I U IVl Location: Joist Description: Mark: BUROVJG SVSTenas TIGARD,OR Long Span 24LH386/260 TJ47 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 35-91/2 35-51/2 24.00 22.65 8 Special Parallel Chords Variable Left End Right End BC Panel 3-6 2-9 1/2 l+-rFI8 I I I I-T=F 1�H4--13-1 r ref- 1-1-l114 F1141�rT TC Panel 2-6 2-0 1- First Half 1-0 0-6 �� TTTtfiaTfTTTTT TTTIhITT ITT.1 111141 I 1 I I I ffTlifTTT(T ITTTTIT1�Il1i z First Diag. 4-6 3-3 1/2 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 35-9 1/2 L-BL Uniform (plf) LL (1) 260.00 260.00 TC + 0-0 35-9 1/2 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 84.00 84.00 BC + 0-0 35-9 1/2 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) IP (1) 60.00 60.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) SM (1) 21.00 21.00 TC + 0-0 35-9 1/2 L-BL Conc Load (Ibs) LL (1) 10,000.00 0.00 TC + 10-0 1/2 10-0 1/2 L-OAL Conc Load (Ibs) LL (1) 3,125.00 0.00 TC + 10-7 10-7 L-OAL Conc Load (Ibs) LL (1) 10,000.00 0.00 TC - 11-11/2 11-11/2 L-OAL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 35-9 1/2 L-BL Uniform (plf) SM(3) 21.00 21.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(3) 20.00 20.00 TC + 0-0 35-9 1/2 L-BL Axial (Ibs) WL(3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) SM(3) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(3) 84.00 84.00 BC + 0-0 35-9 1/2 L-BL Uniform (plf) IP (3) 60.00 60.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) LL(3) 260.00 260.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(3) 126.00 126.00 TC + 0-0 35-9 1/2 L-BL Conc Load (Ibs) LL(3) 10,000.00 0.00 TC - 10-0 1/2 10-0 1/2 L-OAL Conc Load (Ibs) LL(3) 3,125.00 0.00 TC + 10-7 10-7 L-OAL Conc Load (Ibs) LL(3) 10,000.00 0.00 TC + 11-11/2 11-11/2 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 33.00 51.00 10,963.35 9,648.63 2,740.84 52,379.88 52,282.52 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,053.05 19,062.13 0.00 0.00 21,285.79 1,210.13 45.97 0-2 V1S 1,011.72 18,619.01 0.00 0.00 97.42 1,088.12 25.63 2-6 W3 1,011.72 18,619.01 23,080.59 1,286.30 586.50 10,732.97 25.63 3-6 W4 1,759.18 32,268.09 23,080.59 1,286.30 12,635.27 713.57 33.00 4-6 V2 1,759.18 32,268.09 23,080.59 1,286.30 94.30 1,125.59 22.65 6-6 W5 1,759.18 32,268.09 43,052.28 2,284.81 637.52 13,083.01 40.02 6-6 W6 2,510.72 49,596.53 43,052.28 2,284.81 15,247.01 7,521.43 28.93 9-3 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 �i� Job Number: Job Name: Date Run: �/� 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:32:06 PM NEW MILLENNIUM Location: Joist Description: Mark: A.m.notic. 6V6TRM9 TIGARD,OR Long Span 24LH386/260 TJ47 Stress Analysls Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. V3 2,510.72 49,596.53 43,052.28 2,284.81 5,350.44 10,039.68 22.6510-9 W7 2,510.72 49,596.53 51,271.87 2,720.04 1,618.51 3,737.72 30.89 10-9 W8 2,887.73 52,379.88 51,271.87 2,720.04 5,845.38 2,385.45 33.00 12-6 V4 2,887.73 52,379.88 51,271.87 2,720.04 86.44 1,073.90 22.65 14-6 W9 2,887.73 52,379.88 52,282.52 2,979.12 3,770.87 4,172.72 33.00 14-6 W10 2,994.22 51,324.70 52,282.52 2,979.12 3,993.44 3,993.44 33.00 16-6 V5 2,994.22 51,324.70 52,282.52 2,979.12 86.97 1,068.62 22.6518-6 W10 2,994.22 51,324.70 49,150.38 2,933.03 3,993.44 3,993.44 33.00 18-6 W9 2,795.54 46,115.63 49,150.38 2,933.03 3,770.87 4,172.72 33.00 20-6 V6 2,795.54 46,115.63 49,150.38 2,933.03 85.98 1,042.58 22.65 22-6 W8 2,795.54 46,115.63 41,864.37 2,581.75 5,845.38 2,385.45 33.00 22-6 W7 2,291.66 36,752.64 41,864.37 2,581.75 398.86 7,028.47 33.00 24-6 V7 2,291.66 36,752.64 41,864.37 2,581.75 83.46 995.76 22.65 26-6 W6 2,291.66 36,752.64 30,424.44 1,925.28 8,701.13 503.76 33.00 26-6 W5 1,482.61 23,856.41 30,424.44 1,925.28 608.67 9,884.22 33.00 28-6 V8 1,482.61 23,856.41 30,424.44 1,925.28 79.41 928.18 22.65 30-6 W4 1,482.61 23,856.41 14,897.37 963.64 12,635.27 713.57 33.00 30-6 W3 818.20 14,018.53 14,897.37 963.64 567.94 8,831.58 23.43 32-6 V1S 818.20 14,018.53 0.00 0.00 65.21 752.43 24.56 33-9 1/2 W2 841.79 14,271.51 0.00 0.00 15,890.57 1,036.79 38.80 33-0 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:32:06 PM NEW Nil L L E N N I U PA Location: Joist Description: Mark: BIMInINO SYSTE.An TIGARD,OR Long Span 24LH386/260 TJ47 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 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 500.37 419.31 628.97 20-71/8 26-11/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 24.00 33.00 15.50 22.00 1.1250 Min Weld Len 2X: Bending Load 406.00 406.00 406.00 406.00 406.00 0.5644 Axial Load 19,062.13 18,619.01 52,379.88 14,018.53 14,271.51 Max Load Fillers TC: fa 4,325.03 9,161.09 25,772.43 6,897.53 3,238.08 55,802.79 Maximum K L/r 56.85 48.73 36.55 31.47 44.67 Max Load no Fillers TC: Fcr 38,416.70 40,813.40 43,918.29 45,001.60 41,920.64 52,956.83 Fa 23,050.02 24,488.04 26,350.97 27,000.96 25,152.38 273.543.54 yy: F'e 2,517,583.50 332,736.44 591,531.44 797,736.50 4,078,069.00 BCOAUFyy: Cm 0.9991 0.9862 0.9708 0.9957 0.9996 326.19 Panel Point Moment 1804.18 1804.18 1624.00 1258.33_ 486.08 BC Stress: Mid Panel Moment 2019.60 843.72 812.00 159.67 1803.84 "4 BC Panel Point fb 180.05 2472.13 2225.24 1724.19 48.51 130.36 30.3681 Mid Panel fb 230.36 471.46 453.74 89.22 205.75 Fillers 0 0 0 0 0 TC Shear Stress: 13,774.62 Panel Point Stress 4,505.07 11,633.22 27,997.67 8,621.72 3,286.59 BC Shear Stress: Mid Panel Stress 0.1018 0.3891 0.9926 0.2582 0.0715 12,299.65 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 21,285.79 24,373.24 1,210.13 9,625.27 7.65 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V1 S 97.42 4,802.89 1,088.12 2,708.57 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W3 586.50 18,714.09 10,732.97 11,275.32 4.11 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 12,635.27 14,381.54 713.57 7,443.94 5.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 94.30 4,802.89 1,125.59 3,012.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W5 637.52 28,624.38 13,083.01 15,614.11 4.70 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W6 15,247.01 18,714.09 7,521.43 10,504.40 5.83 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V3 5,350.44 16,730.22 10,039.68 10,508.45 4.28 x 0.158 1 C32BA- 1.125 x 1.520 x.158 W7 1,618.51 7,826.93 3,737.72 4,054.26 2.47 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W8 5,845.38 7,826.93 2,385.45 3,848.87 3.86 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V4 86.44 4,802.89 1,073.90 3,012.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 3,770.87 8,984.69 4,172.72 4,660.47 2.38 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 3,993.44 8,984.69 3,993.44 4,660.47 2.28 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V5 86.97 4,802.89 1,068.62 3,012.93 2.00 x 0.077 i 1 C10AB= 1.125 x 0.756 x.077 W10 3,993.44 8,984.69 3,993.44 4,660.47 2.28 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W9 3,770.87 8,984.69 4,172.72 4,660.47 2.38 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V6 85.98 4,802.89 1,042.58 3,012.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W8 5,845.38 7,826.93 2,385.45 3,848.87 3.86 x 0.102 i 1 C16BB= 1.125 x 1.025 x.102 W7 398.86 14,381.54 7,028.47 7,443.94 3.16 x 0.150 1 C28BB= 1.125 x 1.344 x.150 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �// 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:32:06 PM NEW MILLENNIUM Location: Joist Description: Mark. RI lit nitir. =,a*FMG TIGARD,OR Long Span 24LH386/260 TJ47 Web Design, Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 83.46 4,802.89 995.76 3,012.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W6 8,701.13 8,984.69 503.76 4,660.47 4.97 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 608.67 24,373.24 9,884.22 11,960.98 3.55 x 0.188 1 C38BA= 1.125 x 1.845 x.199 V8 79.41 4,802.89 928.18 3,012.93 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W4 12,635.27 14,381.54 713.57 7,443.94 5.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 567.94 14,381.54 8,831.58 9,148.27 3.96 x 0.150 1 C28BB= 1.125 x 1.344 x .150 V1S 65.21 4,802.89 752.43 2,825.24 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W2 15,890.57 16,730.22 1,036.79 7,904.25 6.77 x 0.158 1 C32BA= 1.125 x 1.520 x .158 STRESS ANALYSIS- PAGE 3 Job Number: Job Name: Date Run: 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:32:06 PM NEW MILLENNIUM Location: Joist Description: Mark: SOIL.rLNG SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ47 TCX Design TCX Left TCX Right TCX Length 0-5 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-5 1/2 BPL Length 2-5 7/8 Clear Bearing 1-3 1/4 Clear Bearing 0-8 7/8 _ BPL Material:2525=2 1/2 x 2 1/2 x.250 BPL Material:2525=2 1/2 x 2 1/2 x.250 Total Load 386.00 Total Load 386.00 Reqd TL Def U80 0.06 Reqd TL Def U80 0.00 Live Load 260.00 Live Load 260.00 Reqd LL Def L/120 0.04 Reqd LL Def U120 0.00 Section Modulus 8.7670 Section Modulus 8.7670 Reqd SM 0.0263 Reqd SM 0.0000 Mom of Inertia 30.3938 Mom of Inertia 30.3938 Reqd MI 0.0038 Reqd MI 0.0000 Seat Type:Pegged or Butted(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 STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:33:05 PM NEW MILLENNIUM Location: Joist Description: Mark. BUILDING SYSTEMS TIGARD,OR Long Span 24LH3861260 TJ49 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 35-9 1/2 35-5 1/2 24.00 22.85 8 @ 4-0 Parallel Chords Variable Left End Right End 1 BC Panel 3-6 2-9 1/2 �. - -t iii�tiiifiili�i ltjl lltJ TC Panel 2-6 2-0 ��i i i t�t� First Half 1-0 0-6 i[`I.Ih1 1111 I i f 11 I l I 1 1 i ,1'fl 1 I 1 I`o('t ii,v First Diag. 4-6 3-3 1/2 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 35-9 1/2 L-BL Uniform (plf) LL(1) 260.00 260.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 84.00 84.00 BC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) SM (1) 21.00 21.00 TC + 0-0 35-9 1/2 L-BL Axial (Ibs) SM(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) IP (1) 60.00 60.00 TC + 0-0 35-9 1/2 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 35-9 1/2 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 8,414.14 8,461.79 2,115.45 40,797.75 39,899.28 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,043.71 15,566.37 0.00 0.00 16,003.95 1,202.02 46.07 0-2 V1S 1,002.75 15,127.18 0.00 0.00 97.21 1,063.06 25.81 2-6 W3 1,002.75 15,127.18 17,075.01 1,274.90 585.36 7,832.86 25.81 3-6 W4 1,743.58 24,785.03 17,075.01 1,274.90 9,690.28 710.23 33.14 4-6 W5 1,743.58 24,785.03 28,770.77 2,136.65 605.82 8,116.82 33.14 6-6 W6 2,454.09 34,071.63 28,770.77 2,136.65 6,939.26 501.41 33.14 8-6 W7 2,454.09 34,071.63 36,393.55 2,695.92 396.99 5,274.43 33.1410-6 W8 2,862.13 39,409.20 36,393.55 2,695.92 4,096.87 292.58 33.1412-6 W9 2,862.13 39,409.20 39,899.28 2,952.71 231.40 3,067.82 33.14 14-6 W10 2,967.68 40,797.75 39,899.28 2,952.71 3,067.82 231.40 33.14 16-6 W 10 2,967.68 40,797.75 39,287.93 2,907.02 3,067.82 231.40 33.14 18-6 W9 2,770.75 38,237.27 39,287.93 2,907.02 231.40 3,067.82 33.14 20-6 W8 2,770.75 38,237.27 34,559.51 2,558.86 4,096.87 292.58 33.14 22-6 W7 2,271.35 31,727.77 34,559.51 2,558.86 396.99 5,274.43 33.14 24-6 W6 2,271.35 31,727.77 25,714.02 1,908.21 6,939.26 501.41 33.14 26-6 W5 1,469.46 21,269.23 25,714.02 1,908.21 605.82 8,116.82 33.14 28-6 W4 1,469.46 21,269.23 12,817.63 955.09 9,690.28 710.23 33.14 30-6 W3 810.94 12,687.16 12,817.63 955.09 567.61 7,599.40 23.63 32-6 V1S 810.94 12,687.16 0.00 0.00 65.09 742.77 24.75 33-91/2 W2 834.33 12,937.90 0.00 0.00 13,776.65 1,030.74 38.92 33-0 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 86.84 1,012.98 22.85 STRESS ANALYSIS- PAGE 2 �/� Job Number: Job Name: Date Run: �/� 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:33:05 PM NEW MILLENNIUM Location: Joist Description: Mark: AI"it Winn G` *F^+s TIGARD,OR Long Span 24LH386/260 TJ49 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x .216 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 399.95 335.16 502.74 17-1 7/8 25-9 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 24.00 24.00 15.50 22.00 1.1250 Min Weld Len 2X: Bending Load 406.00 406.00 406.00 406.00 406.00 0.5000 Axial Load 15,566.37 15,127.18 40,797.75 12,687.16 12,937.90 Max Load Fillers TC: fa 3,882.27 9,254.36 24,958.86 7,761.63 3,226.73 44,789.44 Maximum K L/r 71.36 61.16 45.87 39.50 56.07 Max Load no Fillers TC: Fcr 34,457.82 38,034.96 42,869.89 44,609.14 39,733.42 41,125.26 Fa 20,674.69 22,820.98 25,721.93 26,765.48 23,840.05 TCCAL/Ryy: 328.23 Fe 2,570,920.50 186,966.06 332,384.13 448,251.63 4,164,466.25 BCOAL/Ryy: Cm 0.9992 0.9753 0.9497 0.9913 0.9996 330.06 Panel Point Moment 1661.03 1661.03 1624.00 1270.18 430.94 BC Stress: Mid Panel Moment 2091.04 798.47 812.00 192.48 1831.29 0.93 BC URz: Panel Point fb 166.97 3835.32 3749.82 2932.85 43.32 121.8893 Mid Panel fb 271.16 752.14 764.88 181.31 237.48 TC Shear Stress: Fillers 0 0 0 0 0 10,123.80 Panel Point Stress 4,049.24 13,089.68 28,708.68 10,694.48 3,270.05 BC Shear Stress: Mid Panel Stress 0.1029 0.4292 0.9949 0.2955 0.0756 11,616.36 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 16,003.95 21,935.91 1,202.02 9,601.28 5.75 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W3 585.36 14,381.54 7,832.86 8,711.84 3.52 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 9,690.28 14,381.54 710.23 7,419.86 4.35 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W5 605.82 18,714.09 8,116.82 9,542.60 3.11 x 0.176 1 C34AA= 1.125 x 1.549 x .176 W6 6,939.26 8,984.69 501.41 4,644.87 3.96 x 0.118 1 C18BB= 1.125 x 1.035 x .118 W7 396.99 14,381.54 5,274.43 7,419.86 2.37 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W8 4,096.87 5,758.64 292.58 2,484.76 3.07 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W9 231.40 7,826.93 3,067.82 3,835.49 2.03 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W 10 _ 3,067.82 4,802.89 231.40 1,915.97 2.68 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W 10 3,067.82 4,802.89 231.40_ 1,915.97 2.68 x 0.077 1 C10AB= 1.125 x 0.756 x .077 W9 231.40 7,826.93 3,067.82 3,835.49 2.03 x 0.102 1 C16BB= 1.125 x 1.025 x .102 W8 4,096.87 5,758.64 292.58 2,484.76 3.07 x 0.090 1 C12BB= 1.125 x 0.799 x .090 W7 396.99 14,381.54 5,274.43 7,419.86 2.37 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W6 6,939.26 8,984.69 501.41 4,644.87 3.96 x 0.118 1 C18BB= 1.125 x 1.035 x .118 W5 605.82 18,714.09 8,116.82 9,542.60 3.11 x 0.176 1 C34AA= 1.125 x 1.549 x .176 W4 9,690.28 14,381.54 710.23 7,419.86 4.35 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W3 567.61 14,381.54 7,599.40 9,111.89 3.41 x 0.150 1 C28BB= 1.125 x 1.344 x .150 W2 13,776.65 15,057.20 1,030.74 7,884.31 5.87 x 0.158 1 C32BA= 1.125 x 1.520 x .158 V1 97.21 4,802.89 1,063.06 2,689.05 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x .077 V2 86.84 4,802.89 1,012.98 2,998.68 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 10/25/2018 3:33:05 PM NEW MILLENNIUM Location: Joist Description: Mark: 131111_rvtic SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ49 TCX Design TCX Left TCX Right TCX Length 0-5 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-5 1/2 BPL Length 2-5 7/8 Clear Bearing 1-3 1/4 Clear Bearing 0-8 7/8 BPL Material:2525= 2 1/2 x 2 1/2 x.250 BPL Material:2525= 2 1/2 x 2 1/2 x.250 Total Load 386.00 Total Load 386.00 Reqd TL Def U80 0.06 Reqd TL Def L/80 0.00 Live Load 260.00 Live Load 260.00 Reqd LL Def L/120 0.04 Reqd LL Def U120 0.00 Section Modulus 7.7114 Section Modulus 7.7114 Reqd SM 0.0263 Reqd SM 0.0000 Mom of Inertia 28.2363 Mom of Inertia 28.2363 Reqd MI 0.0038 Reqd MI 0.0000 Seat Type:Pegged or Butted(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 STRESS ANALYSIS- PAGE 1 4 Job Number: Job Name: Date Run: 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:11:39 AM NEW MILLENNIUM Location: Joist Description: Mark: ®U1t-01NG sVs*aMs TIGARD,OR Long Span 20LH444/300 TJ5 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 28-4 28-0 20.00 18.84 ,5 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 4-2 4-2 TC Panel 3-2 3-2 � A ;: , f First Half 2-0 2-0 ��1k11TI-T TIT1` MTTTTT7 THIIf I I[LTTTl'FTIhT1 TTiTLTTT TIITT>TT' --- First Diag. 6-2 6-2 Depth 20.00 20.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference !' Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 L-BL Uniform (plf) LL (1) 300.00 300.00 TC + 0-0 28-4 L-BL Uniform (plf) SM (1) 24.00 24.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC _ + 0-0 0-0 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 L-BL Conc @ any pp(Ibs) _ SM(1) 300.00 0.00 TC + 14-2 0-0 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Axial (Ibs) SM(1) 3,500.00 0.00 BC + 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) 96.00 96.00 BC + 0-0 28-4 L-BL Conc @ any pp(Ibs) WL(1) 300.00 0.00 TC + 14-2 0-0 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 BC + 0-0 0-0 L-BL Additional Shear (Ibs) LL(1) 700.00 0.00 TC + 0-0 0-0 L-BL Axial (Ibs) WL(2) 3,000.00 0.00 BC + 0-0 0-0 L-BL Conc @ any pp(Ibs) WL (2) 300.00 0.00 TC - 14-2 0-0 L-BL Conc @ any pp(Ibs) SM (2) 300.00 0.00 TC - 14-2 0-0 L-BL Gross Uplift (plf) WL (2) 42.00 42.00 TC - 0-0 28-4 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 9,264.07 8,982.00 2,316.02 41,969.11 42,809.88 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 7,598.52 22,419.11 0.00 0.00 24,147.46 8,459.77 51.56 0-2 V1S 5,808.44 21,372.92 0.00 0.00 3,825.37 2,971.50 22.34.3-2 W3 5,808.44 21,372.92 29,120.49 8,277.54 1,407.75 11,650.11 30.51 4-2 W4 6,146.32 35,124.41 29,120.49 8,277.54 9,330.15 1,407.75 30.51 6-2 W5 6,146.32 35,124.41 39,244.22 8,434.84 1,407.75 6,852.29 30.51 8-2 W6 6,143.11 41,969.11 39,244.22 8,434.84 4,996.32 1,407.75 30.51 10-2 W7 6,143.11 41,969.11 42,809.88 8,271.12 2,050.34 3,750.83 30.51 12-2 W7 5,532.25 41,969.10 42,809.88 8,271.12 2,050.34 3,750.83 30.51 14-2 W6 5,532.25 41,969.10 39,244.22 7,213.12 4,996.32 1,407.75 30.51 16-2 W5 4,313.73 35,124.41 39,244.22 7,213.12 1,407.75 6,852.29 30.51 18-2 W4 4,313.73 35,124.41 29,120.49 5,834.09 9,330.15 1,407.75 30.51 20-2 W3 2,754.13 21,372.92 29,120.49 5,834.09 1,407.75 11,650.11 30.51 22-2 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 4 Job Number: Job Name: Date Run: ��/ 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:11:39 AM NEW M I L L E N N I UM Location: Joist Description: Mark: AIM rIl�r: SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ5 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length_ PP Dist. V1S 2,754.13 21,372.92 0.00 0.00 3,825.37 2,971.50 22.34 25-2 W2 3,118.86 22,419.11 0.00 0.00 24,147.46 8,459.77 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 396.84 2,048.09 18.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:11:39 AM NEW MILL EN N I U IV5 Location: Joist Description: Mark: 111111 ninm %VSTFM'i TIGARD,OR Long Span 20LH444/300 TJ5 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X .188 Axial and Bendin Analysis K. Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 491.22 736.83 17-1 18-3 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00_ 573.00 0.5000 Axial Load 22,419.11 21,372.92 41,969.11. 21,372.92 22,419.11 Max Load Fillers TC: fa 5,292.52 11,484.64 22,551.91 11,484.64 6,805.22 50,573.97 Maximum K Ur 92.02 92.02 46.01 92.02 92.02 Max Load no Fillers TC: Fcr 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 257.58 T y: 7.58 Pe 539,299.88 81,962.00 327,847.97 81,962.00 266,614.72 BC OAURyy: Cm 0.9951 0.9299 0.9539 0.9299 0.9872 260.64 Panel Point Moment 115025.55 5218.23 2292.00 4378.83 20249.96 BC Stress: Mid Panel Moment 91838.84 4281.25 1146.00 3364.69 13307.27 11X) BC Panel Point fb 19730.13 10646.52 4676.26 8933.94 8190.10 121 88 121.8893 Mid Panel fb 15752.96 3663.79 980.72 2879.43 5382.13 TC Shear Stress: Fillers 0 0 0 0 0 10,750.33 Panel Point Stress 25,022.65 22,131.16 27,228.18 20,418.58 14,995.32 BC Shear Stress: Mid Panel Stress 0.7999 0.8429 0.9089 0.8146 0.5858 14,110.97 Web Design Member Web Tension Allow Tension Web Comp ' Allow Comp Weld Qty Material W2 24,147.46 25,761.95 8,459.77 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 1,407.75 24,373.24 11,650.11 12,698.97 4.18 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 9,330.15 10,742.43 1,407.75 6,045.24 4.87 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 1,407.75 14,381.54 6,852.29 7,876.57 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 4,996.32 5,758.64 1,407.75 2,799.53 3.74 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 4,996.32 5,758.64 1,407.75 2,799.53 3.74 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 1,407.75 14,381.54 6,852.29 7,876.57 3.08 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 9,330.15 10,742.43 1,407.75 6,045.24 4.87 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,407.75 24,373.24 11,650.11 12,698.97 4.18 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 24,147.46 25,761.95 8,459.77 9,511.41 8.67 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1 3,825.37 4,802.89 2,971.50 3,034.97 3.35 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 396.84 4,802.89 2,048.09 3,292.50 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 10/24/2018 9:11:39 AM NEW MILLENNIUM Location: Joist Description: Mark: ilt-r111,1f1 SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ5 TCX Design TCX Left TCX Right TCX Length 5-9 1/2 TCX Length 2-4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 9-5 BPL Length 5-10 7/8 Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material:302025=3 x 2 x.250 BPL Material:2018=2 X 2 X .188 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.87 Reqd TL Def U80 0.35 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.39 Reqd LL Def U180 0.16 Section Modulus 4.6476 Section Modulus 2.4725 Reqd SM 3.8342 Reqd SM 0.6750 Mom of Inertia 10.3441 Mom of Inertia 3.9771 Reqd MI 7.0899 Reqd MI 0.5237 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: �/i/ 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:33:27 PM NEW NIILLENNIUNt Location: Joist Description: Mark: BUILDING SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ52 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 35-91/2 35-51/2 24.00 22.47 8 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-6 2-9 1/2 111 VFW fIFylT1TlT 1:TTIIMIR ITT IZ1IMTIMI-Till j-rrr i7TTyR7r�TT n Tr i94-144, TC Panel 2-6 2-0 f First Half 1-0 0-6 Ulna' tidathUdiIif) ,ithLTCfLII(fI1 , IL / First Diag. _4-6 3-3 1/2 Depth 24.00 24.00 i' Loads Load Type Category Load1 Load2 ' Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL (1) 260.00 260.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 126.00 126.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) IP (1) 60.00 60.00 TC + 0-0 35-9 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) 500.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) SM(1) 21.00 21.00 TC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 84.00 84.00 BC + 0-0 35-9 1/2 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 35-9 1/2 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Conc Load (Ibs) CL(1) 3,000.00 0.00 TC + 5-3 5-3 L-OAL Conc Load(Ibs) CL(1) 3,000.00 0.00 TC + 16-5 16-5 L-OAL Gross Uplift(plf) WL(2) 36.00 36.00 TC - 0-0 35-9 1/2 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 12,679.71 10,196.23 3,169.93 57,303.71 58,280.09 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,061.22 23,381.69 0.00 0.00 25,935.71 1,217.25 45.88 0-2 V1S 1,019.57 22,935.13 0.00 0.00 586.10 1,672.63 25.48 2-6 W3 1,019.57 22,935.13 27,230.97 1,296.29 587.50 13,263.80 25.48 3-6 W4 1,772.83 36,918.01 27,230.97 1,296.29 13,044.87 733.13 32.88 4-6 W5 1,772.83 36,918.01 42,359.83 2,172.49 733.13 11,457.51 32.88 6-6 W6 2,495.26 49,063.38 42,359.83 2,172.49 10,269.54 733.13 32.88 8-6 W7 2,495.26 49,063.38 52,813.48 2,741.14 733.13 8,590.01 32.88 10-6 W8 2,910.14 57,193.47 52,813.48 2,741.14 7,402.05 733.13 32.88 12-6 W9 2,910.14 57,193.47 58,280.09 3,002.24 733.13 5,722.52 32.88 14-6 W10 3,017.46 57,303.71 58,280.09 3,002.24 4,637.63 4,637.63 32.88 16-6 W10 3,017.46 57,303.71 53,954.11 2,955.79 4,637.63 4,637.63 32.88 18-6 W9 2,817.23 50,995.90 53,954.11 2,955.79 733.13 5,722.52 32.88 20-6 W8 2,817.23 50,995.90 45,442.01 2,601.78 7,402.05 733.13 32.88 22-6 W7 2,309.45 40,672.84 45,442.01 2,601.78 733.13 8,590.01 32.88 24-6 W6 2,309.45 40,672.84 32,743.77 1,940.23 10,269.54 733.13 32.88 26-6 W5 1,494.11 26,334.50 32,743.77 1,940.23 733.13 11,457.51 32.88 28-6 W4 1,494.11 26,334.50 15,926.68 971.11 13,044.87 733.13 32.88 30-6 W3 824.55 15,293.23 15,926.68 971.11 568.23 9,920.38 23.26 32-6 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name Date Run: 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:33:27 PM NEW Nt I L L E N N I U NI Location: Joist Description: Mark: ELM nItin SYSTEMS TIGARD,OR Long Span 24LH386/260 TJ52 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. V1S 824.55 15,293.23 0.00 0.00 542.84 1,300.41 24.40 33-91/2 W2 848.32 15,548.18 0.00 0.00 17,775.68 1,042.10 38.70 33-0 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 87.09 2,344.80 22.47 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/25/2018 3:33:27 PM NEW MILLENNIUM Location: Joist Description: Mark: RI III 1-11NC ss*FMS TIGARD,OR Long Span 24LH386/260 TJ52 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 1.0151 0.7748 0.4934 1.4841 0.7033 0.6093 0.9679 2521 =2 1/2 x 2 1/2 x.212 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 541.10 453.44 680.16 21-101/4 29-81/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 28.00 24.00 24.00 15.50 22.00 1'1250 Min Weld Len 2X:: Bending Load 406.00 406.00 406.00 406.00 406.00 0.6174 Axial Load 23,381.69 22,935.13 57,303.71 15,293.23 15,548.18 Max Load Fillers TC: fa 5,064.92 10,232.50 25,566.03 6,823.07 3,368.03 59,849.52 Maximum K L/r 51.51 44.15 33.11 28.51 40.47 Max Load no Fillers TC: Fcr 38,755.03 40,650.88 43,072.44 43,908.75 41,518.74 57,427.07 Fa 23,253.02 24,390.53 25,843.46 26,345.25 24,911.25 TC OALRyy: 257.69 Fe 2,498,307.00 401,690.22 714,116.00 963,053.38 4,046,844.50 BCOAL/Ryy: Cm 0.9990 0.9873 0.9760 0.9965 0.9996 286.71 Panel Point Moment 1717.12 1717.11 1624.00 1252.19 514.68 BC Stress: Mid Panel Moment 2063.00 777.98 812.00 142.65 1789.54 0.96 BC Panel Point fb 169.89 1945.45 1839.95 1418.70 50.92 97.284 7.2841 Mid Panel fb 220.36 353.22 368.66 64.77 191.15 TC Shear Stress: Fillers 0 0 0 0 0 13,863.98 Panel Point Stress 5,234.80 12,177.95 27,405.99 8,241.77 3,418.95 BC Shear Stress: Mid Panel Stress 0.2249 0.4312 1.0015 0.2611 0.0745 13,215.63 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 25,935.71 28,624.38 1,217.25 11,091.20 9.32 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 587.50 24,373.24 13,263.80 14,244.36 4.76 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 13,044.87 14,381.54 733.13 7,464.59 5.86 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 733.13 24,373.24 11,457.51 11,996.09 4.12 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 10,269.54 10,742.43 733.13 5,736.18 5.36 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 733.13 18,714.09 8,590.01 9,601.19 3.29 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 7,402.05 7,826.93 733.13 3,860.34 4.89 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 733.13 10,742.43 5,722.52 5,736.18 2.99 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W 10 4,637.63 8,984.69 4,637.63 4,673.84 2.65 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W 10 4,637.63 8,984.69 4,637.63 4,673.84 2.65 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W9 733.13 10,742.43 5,722.52 5,736.18 2.99 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W8 7,402.05 7,826.93 733.13 3,860.34 4.89 x 0.102 1 C16BB = 1.125 x 1.025 x.102 W7 733.13 18,714.09 8,590.01 9,601.19 3.29 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 10,269.54 10,742.43 733.13 5,736.18 5.36 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W5 733.13 24,373.24 11,457.51 11,996.09 4.12 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 13,044.87 14,381.54 733.13 7,464.59 5.86 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W3 568.23 16,730.22 9,920.38 10,368.99 4.23 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W2 17,775.68 18,714.09 1,042.10 9,160.58 6.80 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V1 586.10 4,802.89 1,672.63 2,725.35 2.00 x 0.077 1 C10AB = 1.125 x 0.756 x.077 V2 87.09 4,802.89 2,344.80 3,025.24 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 10/25/2018 3:33:27 PM NEW M I L LE N N I UM Location: Joist Description: Mark: BILL-OINel SYSTEM= TIGARD,OR Long Span 24LH386/260 TJ52 TCX Design TCX Left TCX Right TCX Length 0-5 TCX Length 0-0 TCX Type S, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-5 1/2 BPL Length 2-5 3/4 Clear Bearing 1-2 7/8 Clear Bearing 0-8 7/8 BPL Material: 2525 =2 1/2 x 2 1/2 x .250 BPL Material:2525=2 1/2 x 2 1/2 x .250 Total Load 386.00 Total Load 386.00 Reqd TL Def U80 0.06 Reqd TL Def L/80 0.00 Live Load 260.00 Live Load 260.00 Reqd LL Def L/120 0.04 Reqd LL Def U120 0.00 Section Modulus 9.3618 Section Modulus 9.3618 Reqd SM 0.0263 Reqd SM 0.0000 Mom of Inertia 31.5913 Mom of Inertia 31.5913 Reqd MI 0.0038 Reqd MI 0.0000 Seat Type:Pegged or Butted(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(W L+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: Dale Run: �/�I 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 8:50:31 AM NEW MILLENNIUM Location. Joist Description: Mark: ®uiLOING SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ6 Geometry Base Length: Working Length: Joist Depth. Effective Depth: BC Panel Length: Shape: 28-4 28-0 20.00 18.84 5 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 4-2 4-2 F --fT T-FlifTTTHR:FITWITT FFTFTT, TC Panel 3-2 3-2 , First Half 2-0 2-0 -�hill IT EIT ffii 1111 T MUM I IT 1 t 1-1TU41 f ITIII iI Il 11TT IT UTTI: First Diag. 6-2 6-2 Depth 20.00 20.00 Loads Load Type Category Load1 Load2 Position I Direction 1 Loc/Begin Sp/End Reference '. Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-4 L-BL Uniform (plf) SM (1) 24.00 24.00 TC + 0-0 28-4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-4 L-BL Axial (Ibs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-4 L-BL Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 _28-4 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-4 L-BL Gross Uplift(plf) WL(2) 42.00 42.00 TC - 0-0 28-4 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 9,264.07 8,982.00 2,316.02 41,109.22 41,148.43 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 7,421.99 22,132.48 0.00 0.00 22,231.54 7,973.21 51.56 0-2 V1S 5,521.81, 21,086.29 0.00 0.00 3,825.37 2,141.56 22.34 3-2 W3 5,521.81 21,086.29 27,512.54 5,597.60 872.94 10,516.45 30.51 4-2 W4 5,573.06 34,551.15 27,512.54 5,597.60 8,196.49 745.40 30.51 6-2 W5 5,573.06 34,551.15 37,739.45 5,468.27 643.37 5,718.63 30.51 8-2 W6 5,283.23_ 41,109.22 37,739.45 5,468.27_ 3,862.66 541.34 30.51 10-2 W7 5,283.23 41,109.22 41,148.43 5,017.92 2,050.34 3,750.83 30.51 12-2 W7 4,672.36 41,109.21 41,148.43 5,017.92 2,050.34 3,750.83 30.51 14-2 W6 4,672.36_ 41,109.21 37,739.45 4,246.55_ 3,862.66 541.34 30.51 16-2 W5 3,740.48 34,551.15 37,739.45 4,246.55 643.37 5,718.63 30.51 18-2 W4 3,740.48 34,551.15 27,512.54 3,154.15 8,196.49 745.40 30.51 20-2 W3 2,467.50 21,086.29 27,512.54 3,154.15 872.94 10,516.45 30.51 22-2 V1S 2,467.50 21,086.29 0.00 0.00 3,825.37 2,141.56 22.34 25-2 W2 2,832.24 22,132.48 0.00 0.00 22,231.54 7,973.21 51.56 24-2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.84 1,348.09 18.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618-0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 8:50:31 AM NEW Nt I L L E N N I LJ Nt Location: Joist Description: Mark: REM rtiNG SVRTFM5 TIGARD,OR Long Span 20LH444/300 TJ6 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024= 2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 491.22 736.83 17-1 22-5 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 36.00 36.00 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 22,132.48 21,086.29 41,109.22 21,086.29 22,132.48 Max Load Fillers TC: fa 5,224.85 11,330.62 22,089.86 11,330.62 6,718.21 50,573.97 Maximum K Ur 92.02 92.02 46.01 92.02 92.02 Max Load no Fillers TC: Far 26,918.89 26,918.89 42,829.38 26,918.89 26,918.89 46,413.96 TC Fa 16,151.33 16,151.33 25,697.63 16,151.33 16,151.33 257.58 57.58 yy: F'e 539,299.88 81,962.00 327,847.97 81,962.00 266,614.72 BC OAURyy: Cm 0.9952 0.9309 0.9549 0.9309 0.9874 260•64 Panel Point Moment 115025.55 5218.23 2292.00 4378.83 20249.96 BC Stress: Mid Panel Moment 91838.84 4281.25 1146.00 3364.69 13307.27 0.96 Panel Point fb 19730.13 10646.52 4676.26 8933.94 8190.10 BC 121.888893 Mid Panel fb 15752.96 3663.79 980.72 2879.43 5382.13 TC Shear Stress: Fillers 0 0 0 0 0 9,897.37 Panel Point Stress 24,954.99 21,977.14 26,766.12 20,264.56 14,908.31 BC Shear Stress: Mid Panel Stress 0.7956 0.8329 0.8909 0.8048 0.5803 12,991.37 Web Design Member Web Tension Allow Tension Web Camp Allow Comp Weld Qty Material W2 22,231.54 25,761.95 7,973.21 9,511.41 7.98 x 0.188 1 C4OBA= 1.125 x 2.014 x .218 W3 872.94 24,373.24 10,516.45 12,698.97 3.78 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 8,196.49 10,742.43 745.40 6,045.24 4.28 x 0.129 1 C22BB = 1.125 x 1.110 x.129 W5 643.37 14,381.54 5,718.63 7,876.57 2.57 x 0.150 1 C28BB = 1.125 x 1.344 x.150 W6 3,862.66 5,758.64 541.34 2,799.53 2.89 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 2,050.34 7,826.93 3,750.83 4,091.27 2.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 3,862.66 5,758.64 541.34 2,799.53 2.89 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 643.37 14,381.54 5,718.63 7,876.57 2.57 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 8,196.49 10,742.43 745.40 6,045.24 4.28 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 872.94 24,373.24 10,516.45 12,698.97 3.78 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 22,231.54 25,761.95 7,973.21 9,511.41 7.98 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 V1 3,825.37 4,802.89 2,141.56 3,034.97 3.35 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V2 96.84 4,802.89 1,348.09 3,292.50 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 10/24/2018 8:50:31 AM NEW MILLENNIUM Location: Joist Description: Mark: A , mina; SVST@MS TIGARD,OR Long Span 20LH444/300 TJ6 TCX Design TCX Left TCX Right TCX Length 5-9 1/2 TCX Length 2-4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 _BPL Length 9-5 BPL Length 5-10 7/8 _Clear Bearing 1-1 1/2 Clear Bearing 1-1 1/2 BPL Material:302025=3 x 2 x.250 BPL Material:2018=2 X 2 X.188 Total Load 540.00 Total Load 540.00 Reqd TL Def U80 0.87 Reqd TL Def U80 0.35 Live Load 300.00 Live Load 300.00 Reqd LL Def U180 0.39 Reqd LL Def L/180 0.16 Section Modulus 4.6476 Section Modulus 2.4725 Reqd SM 3.8342 Reqd SM 0.6750 Mom of Inertia 10.3441 Mom of Inertia 3.9771 Reqd MI 7.0899 Reqd MI 0.5237 Seat Type:Bird Cage(Reinforced) Seat Type:Bird Cage(Reinforced) 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: rj// 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:02:48 AM NEW NI ILL E N N I U NI Location: Joist Description: Mark: BWLOING SYSTEMS TIGARD,OR Long Span 20LH444/300 TJ7 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: I 28-1 3/4 27-9 3/4 20.00 18.84 5 @ 4-0 Parallel Chords i Variable Left End Right End . BC Panel 3-113/4 4-2 lei}T�}iif+Tf}�} 1�11[fFFET}1Fft}�F}}fN1 � .{} TC Panel 3 0 3-2 � A �� / ` /�, - First Half 2-0 2-0 �-2,i fTfTTI I:1Tel ,t'(11I I I I1)111'[l 1111TT FfS 111111 t!4 1111111'11l i', First Diag. 5-11 3/4 6-2 Depth 20.00 20.00 i Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 300.00 300.00 TC + 0-0 28-1 3/4 L-BL Uniform (plf) DL(1) 144.00 144.00 TC + 0-0 28-1 3/4 L-BL Uniform (plf) SM (1) 24.00 24.00 TC + 0-0 28-1 3/4 L-BL Axial (Ibs) WL(1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) DL(1) 20.00 20.00 TC + 0-0 28-1 3/4 L-BL Axial (lbs) SM (1) 3,000.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) IP (1) 66.00 66.00 TC + 0-0 28-1 3/4 L-BL Uniform (plf) DL(1) 96.00 96.00 BC + 0-0 28-1 3/4 L-BL Uniform (plf) CL(1) 109.00 109.00 TC + 0-0 28-1 3/4 L-BL Gross Uplift (plf) WL (2) 42.00 42.00 TC - 0-0 28-1 3/4 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 8,934.75 8,982.48 2,245.62 40,667.43 40,611.69 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,273.84 21,202.36 0.00 0.00 21,332.81 1,377.62 49.48 0-2 V1S 1,197.71 20,209.97 0.00 0.00 150.23 2,061.25 22.20 3-0 W3 1,197.71 20,209.97 26,669.09 1,710.46 651.86 10,147.44 30.51 3-113/4 W4 2,090.00 33,814.84 26,669.09 1,710.46 7,837.15 482.51 30.51 5-113/4 W5 2,090.00 33,814.84 37,049.36 2,362.54 346.48 5,359.29 30.51 7-113/4 W6 2,528.07 40,520.16 37,049.36 2,362.54 3,636.82 241.35 30.51 9-113/4 W7 2,528.07 40,520.16 40,611.69 2,586.59 236.47 3,636.82 30.51 11-113/4 W7 2,538.10 40,667.43 40,611.69 2,586.59 236.47 3,636.82 30.51 13-113/4 W6 2,538.10 40,667.43 37,356.07 2,382.60 3,636.82 241.35 30.51 15-113/4 W5 2,240.91 34,256.63 37,356.07 2,382.60 346.48 5,359.29 30.51 17-113/4 W4 2,240.91 34,256.63 27,282.51 2,029.47 7,837.15 482.51 30.51 19-113/4 W3 1,717.72 20,939.02 27,282.51 2,029.47 651.86 10,147.44 30.51 21-113/4 V1S 1,717.72 20,939.02 0.00 0.00 689.33 2,140.80 22.34 24-11 3/4 W2 2,082.45 21,985.22 0.00 0.00 22,066.79 2,237.11 51.56 23-11 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 96.69 1,345.79 18.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618 0007 TIGARD HIGH SCHOOL-SHOPORDERS 10/24/2018 9:02:48 AM NEW M I L L E N N I U M Location: Joist Description: Mark: RILL niNr. SYS*FMS TIGARD,OR Long Span 20LH444/300 TJ7 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and BendingAnalysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 288.64 501.22 751.83 17-1 1/4 25-9 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 34.00 35.75 24.00 36.00 36.00 1.1250 Min Weld Len 2X: Bending Load 573.00 573.00 573.00 573.00 573.00 0.5000 Axial Load 21,202.36 20,209.97 40,667.43 20,939.02 21,985.22 Max Load Fillers TC: fa 6,435.88 10,859.74 21,852.46 11,251.49 6,673.51 50,573.97 Maximum K Ur 86.91 91.39 46.01 92.02 92.02 MaxLoadnoFillersTC: Fcr 28,781.03 27,150.58 42,829.38 26,918.89 26,918.89 46,413.96 Fa 17,268.62 16,290.35 25,697.63 16,151.33 16,151.33 Tco8URyy: 255.85 F'e 298,903.69 83,112.33 327,847.97 81,962.00 266,614.72 BcoAURyy: Cm 0.9892 0.9347 0.9553 0.9314 0.9875 258.89 Panel Point Moment 5890.23 5890.23 2292.00 4378.83 20249.96 BC Stress: Mid Panel Moment 4169.83 2778.38 1146.00 3364.69 13307.27 0. 4 1 BC liRz: Panel Point fb 2382.30 12017.57 4676.26 8933.94 8190.10 121.8893 Mid Panel fb 1458.88 2377.67 980.72 2879.43 5382.13 TC Shear Stress: Fillers 0 0 0 0 0 98Y4.02 Panel Point Stress 8,818.18 22,877.31 26,528.72 20,185.43 14,863.61 BC Shear Stress: Mid Panel Stress 0.4170 0.7509 0.8816 0.7997 0.5775 12,895.10 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 21,332.81 25,761.95 1,377.62 10,068.69 7.66 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W3 651.86 24,373.24 10,147.44 12,698.97 3.64 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 7,837.15 10,742.43 482.51 6,045.24 4.09 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 346.48 14,381.54 5,359.29 7,876.57 2.41 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 3,636.82 4,802.89 241.35 2,184.64 3.18 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W7 236.47 7,826.93 3,636.82 4,091.27 2.40 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 236.47 7,826.93 3,636.82 4,091.27 2.40 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W6 3,636.82 4,802.89 241.35 2,184.64 3.18 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W5 346.48 14,381.54 5,359.29 7,876.57 2.41 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W4 7,837.15 10,742.43 482.51 6,045.24 4.09 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 651.86 24,373.24 10,147.44 12,698.97 3.64 x 0.188 1 C38BA= 1.125 x 1.845 x .199 W2 22,066.79 25,761.95 2,237.11 9,511.41 7.93 x 0.188 1 C40BA= 1.125 x 2.014 x .218 V1 689.33 5,758.64 2,140.80 3,742.51 2.00 x 0.090 1 C12BB= 1.125 x 0.799 x .090 V2 96.69 4,802.89 1,345.79 3,292.50 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 10/24/2018 9:02:48 AM NEW MILLENNIUM Location: Joist Description: Mark: BrIR111Nr: SVSTFMS TIGARD,OR Long Span 20LH444/300 TJ7 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 2-4 , TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 6 1/2 TCX Depth 6 1/2 BPL Length 3-4 7/8 BPL Length 5-10 7/8 Clear Bearing 1-0 3/4 Clear Bearing 1-1 1/2 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 444.00 Total Load 540.00 Reqd TL Def L/80 0.00 Reqd TL Def L/80 0.35 Live Load 300.00 Live Load 300.00 Reqd LL Def L/120 0.00 Reqd LL Def L/180 0.16 Section Modulus 2.4725 Section Modulus 2.4725 Reqd SM 0.0000 Reqd SM 0.6750 Mom of Inertia 3.9771 Mom of Inertia 3.9771 Reqd MI 0.0000 Reqd MI 0.5237 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+W L+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 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)+W L-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