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Section Properties and Stresses A nalysis Results <br />Axes X-Y Centroidal Axes Principal Axes <br />Ix (in^4) +5.653 +5.653 +5.653 <br />Iy (in^4) +1.362 +1.362 +1.362 <br />Ixy (in^4) +0.+0.+0. <br />Io (in^4) +7.016 +7.016 +7.016 <br />rx (in) +1.67 +1.67 +1.67 <br />ry (in) +0.82 +0.82 +0.82 <br />ro (in) +1.86 +1.86 +1.86 <br />Y top (in)+2.642 +2.642 <br />Y bot (in)+2.669 +2.669 <br />Sx top (in^3)+2.14 +2.14 <br />Sx bot (in^3)+2.118 +2.118 <br />X right (in)+1.125 +1.125 <br />X left (in)+1.125 +1.125 <br />Sy right (in^3)+1.211 +1.211 <br />Sy left (in^3)+1.211 +1.211 <br />Zpx (in^3)+2.991 +2.991 <br />Zpy (in^3)+1.438 +1.438 <br />Max Mx (lb.in)+84710.208 +84710.208 <br />Max My (lb.in)+48437.115 +48437.115 <br />Mpx (lb.in)+119641.355 +119641.355 <br />Mpy (lb.in)+57512.102 +57512.102 <br />SFx +1.412 +1.412 <br />SFy +1.187 +1.187 <br />IMax (in^4)+5.653 <br />IMin (in^4)+1.362 <br />Theta (Deg)+0. <br />Elastic Neutral Axis <br />In (in^4) +5.653 <br />ENA Angle(°) +0. <br />Y top (in) +2.642 <br />Y bot (in) +2.669 <br />Sx top (in^3) +2.14 <br />Sx bot (in^3) +2.118 <br />X right (in) +1.125 <br />X left (in) +1.125 <br />Sy right (in^3) +1.211 <br />Sy left (in^3) +1.211 <br />Zpx (in^3) +2.991 <br />Zpy (in^3) +1.438 <br />Max Mx (lb.in) +84710.208 <br />Max My (lb.in) +48437.115 <br />Mpx (lb.in) +119641.355 <br />Mpy (lb.in) +57512.102 <br />SFx +1.412 <br />SFy +1.187 <br />Torque Max (lb.in) +48891.546 <br />Buckling <br />jy (monosymmetry) -0.008 in <br />jx (monosymmetry) +0. in <br />Cxrt Shear Constant +0.586 in^2 <br />Cyrt Shear Constant +0.932 in^2 <br />ßtf Torsional-flexural +0.971 <br />a Torsional-Bending +0.594 in <br />Area +2.028 in^2 <br />Mass/L +0.199 lb/ in <br />Xc +0. in <br />Yc +0. in <br />NA (Deg)+0.0 Deg <br />PNA (x,y)(+0.0,-0.41) <br />Torsion and Shear <br />J(Torsion) +3.145 in^4 <br />Cw(Warping) +0.417 in^6 <br />Xs (Shear) +0. in <br />Ys (Shear) +0.32 in <br />Ax +0.857 in^2 <br />Kx +0.422 <br />Ay +0.857 in^2 <br />Ky +0.422 <br />Ios +7.223 in^4 <br />ros +1.887 in <br />Swx +0.436 in^5 <br />Swy -0.001 in^5 <br />Dsc +0.32 in <br />Composite Section <br />Ref. Aluminium 606 +10000000. psi <br />Transf. Area +2.028 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) +47.221 psi <br />Sig-x max C) -46.725 psi <br />Fpt +40559.421 lb <br />Fpc +40559.421 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 : 06- 01- 2022 / 12:21:12 <br /> Engineer : <br /> C lient : <br /> C om m ent : <br /> Project Ref.: <br /> Project Nam e: OPG 6010 <br /> page 2/ 2A pproved by: <br />V2018.1 - © M echaTools Technologies Inc. 2022 <br />This Product is licenced to : A daptive Re- U se Engineering <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 />60