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Section Properties and Stresses A nalysis Results <br />Axes X-Y Centroidal Axes Principal Axes <br />Ix (in^4) +11.893 +11.893 +11.893 <br />Iy (in^4) +0.872 +0.872 +0.872 <br />Ixy (in^4) +0.043 +0.043 +0. <br />Io (in^4) +12.765 +12.765 +12.765 <br />rx (in) +2.246 +2.246 +2.246 <br />ry (in) +0.608 +0.608 +0.608 <br />ro (in) +2.327 +2.327 +2.327 <br />Y top (in)+4.111 +4.11 <br />Y bot (in)+4.139 +4.14 <br />Sx top (in^3)+2.893 +2.893 <br />Sx bot (in^3)+2.873 +2.873 <br />X right (in)+0.792 +0.792 <br />X left (in)+0.834 +0.834 <br />Sy right (in^3)+1.101 +1.101 <br />Sy left (in^3)+1.046 +1.045 <br />Zpx (in^3)+4.566 +4.566 <br />Zpy (in^3)+1.369 +1.369 <br />Max Mx (lb.in)+114922.741 +114922.969 <br />Max My (lb.in)+41823.885 +41818.977 <br />Mpx (lb.in)+182646.816 +182647.743 <br />Mpy (lb.in)+54770.632 +54757.484 <br />SFx +1.589 +1.589 <br />SFy +1.31 +1.309 <br />IMax (in^4)+11.893 <br />IMin (in^4)+0.872 <br />Theta (Deg)-0.224 <br />Elastic Neutral Axis <br />In (in^4) +11.862 <br />ENA Angle(°) +2.825 <br />Y top (in) +4.107 <br />Y bot (in) +4.133 <br />Sx top (in^3) +2.889 <br />Sx bot (in^3) +2.87 <br />X right (in) +0.816 <br />X left (in) +0.859 <br />Sy right (in^3) +1.107 <br />Sy left (in^3) +1.051 <br />Zpx (in^3) +4.56 <br />Zpy (in^3) +1.384 <br />Max Mx (lb.in) +114791.278 <br />Max My (lb.in) +42053.212 <br />Mpx (lb.in) +182412.749 <br />Mpy (lb.in) +55369.105 <br />SFx +1.589 <br />SFy +1.317 <br />Torque Max (lb.in) +25455.322 <br />Buckling <br />jy (monosymmetry) +0.042 in <br />jx (monosymmetry) +0.086 in <br />Cxrt Shear Constant +0.226 in^2 <br />Cyrt Shear Constant +1.54 in^2 <br />ßtf Torsional-flexural +1. <br />a Torsional-Bending +0.441 in <br />Area +2.358 in^2 <br />Mass/L +0.231 lb/ in <br />Xc +0. in <br />Yc +0. in <br />NA (Deg)+2.82 Deg <br />PNA (x,y)(+0.0,-0.01) <br />Torsion and Shear <br />J(Torsion) +2.621 in^4 <br />Cw(Warping) +0.192 in^6 <br />Xs (Shear) +0.012 in <br />Ys (Shear) +0.038 in <br />Ax +0.609 in^2 <br />Kx +0.258 <br />Ay +0.61 in^2 <br />Ky +0.259 <br />Ios +12.769 in^4 <br />ros +2.327 in <br />Swx +0.033 in^5 <br />Swy -0.14 in^5 <br />Dsc +0.04 in <br />Composite Section <br />Ref. Aluminium 606 +10000000. psi <br />Transf. Area +2.358 in^2 <br />Xcc +0. in <br />Ycc +0. in <br />Stressses Yield & Max/Min <br />Sig-yield T +40000. psi <br />Sig-yield C -40000. psi <br />Tau yield +30000. psi <br />Sig-x max T) +34.804 psi <br />Sig-x max C) -34.577 psi <br />Fpt +47154.757 lb <br />Fpc +47154.757 lb <br />Loads <br />Moment Mx +100. lb.in <br />Moment My +0. lb.in <br />Axial N [.0,.0] +0. lb <br />Torque Tz +100. lb.in <br />Bimoment Bw +10000. lb.in² <br />Shear Vx +100. lb <br />Shear Vy +100. lb Date : 04- 27- 2023 / 11:52:36 <br /> Engineer : <br /> C lient : <br /> C om m ent : <br /> Project Ref.: <br /> Project Nam e: EL 601 <br /> page 2/ 2A pproved by: <br />System U nits: <br /> Length:[in] <br /> M ass :[lb] <br /> Stress:[psi] <br />Section M aterial Identi cation: <br />[A lum inium 6061 - T6(extruded)]: E= + 10000000. [psi]; N u= 0.33; Ro= + 0.098[lb/ in ] <br />5