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26 I <br /> Steel Beam File=P:i176001176591Calculations\Structural1PIW South117659 South.ec6 . <br /> Software copyright ENERCALC,INC.1983-2019,Build:12.19.11.12 . <br /> Lic.#:KW-06002611 SITTS&HILL ENGINEERING,INC. <br /> DESCRIPTION: Hangar Trench Lid Edge Member in Flexure I <br /> CODE REFERENCES <br /> Calculations per AISC 360-10, IBC 2015, CBC 2016,ASCE 7-10 I <br /> Load Combination Set:ASCE 7-10 <br /> Material Properties <br /> Analysis Method: Allowable Strength Design Fy:Steel Yield: 36.0 ksi I <br /> Beam Bracing: Completely Unbraced E:Modulus: 29,000.0 ksi <br /> Bending Axis: Major Axis Bending <br /> L(32 72) <br /> I <br /> i <br /> I <br /> .A.. C8x18 7 ... <br /> - Span= 3.0ft I <br /> Applied Loads Service loads entered.Load Factors will be applied for calculations. <br /> Beam self weight calculated and added to loading <br /> Load(s)for Span Number 1 I <br /> Point Load: L=32.720 k @ 1.50 ft,(Wheel Load) <br /> DESIGN SUMMARY Design OK I <br /> Maximum Bending Stress Ratio = 0.984: 1 Maximum Shear Stress Ratio= 0.325 : 1 <br /> Section used for this span C8x18.7 Section used for this span C8x18.7 <br /> Ma:Applied 24.561 k-ft Va:Applied 16.388 k I <br /> Mn/Omega:Allowable 24.970 k-ft Vn/Omega:Allowable 50.391 k <br /> Load Combination +D+L Load Combination +D+L <br /> Location of maximum on span 1.500ft Location of maximum on span 0.000 ft <br /> Span#where maximum occurs Span#1 Span#where maximum occurs Span#1 I <br /> Maximum Deflection <br /> Max Downward Transient Deflection 0.025 in Ratio= 1,434>=360. <br /> Max Upward Transient Deflection 0.000 in Ratio= 0<360.0 <br /> Max Downward Total Deflection 0.025 in Ratio= 1433 >=240. I <br /> Max Upward Total Deflection 0.000 in Ratio= 0<240.0 <br /> I <br />