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Company Boeing <br />IIRISA <br />Designer :Daniel Jaffe <br />Job Number : <br />Model Name : 40-26 4th Floor Cantilever Rack <br />Vy=V,,y=1.946k <br />Molo,z 43.509 k-ft <br />VY=82.129k <br />(M'alo,z) a + (V,I,) z = 0.509 <br />Combined Axial Load and Bending <br />M,, M,,,,, 0.028 k- ft <br />Mz=M11z=22.131k-ft <br />Maz = 33.839 k- ft <br />P= P = 5.172 k <br />Pa = 68.606 k <br />P+M`=0.731 <br />Pa Maz <br />Shear force due to factored loads, y (see <br />Applied Loading - Shear + Torsion) <br />Factored flexural resistance for globally <br />braced member <br />Factored shear resistance <br />12/17/2024 <br />3:46:16 PM <br />Checked By: Clemens Ro... <br />(Eq. H2-1) <br />Flexural force due to factored loads (with <br />respect to y-axis) <br />Flexural force due to factored loads (with <br />respect to z-axis) <br />Factored flexural resistance (strong axis) (Sec. 63.2) <br />Compressive axial force due to factored loads <br />Factored axial resistance (Sec. 133.2) <br />(Eq. H1.2-1) <br />RISA-3D Version 19 [ 40-26 cantilever rack copy.r3d ] Page 13 <br />