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Section Properties and Stresses Analysis Results <br />Axes X-Y Centroidal Axes Principal Axes <br />Ix (in^4) +2.952 +2.952 +2.952 <br />Iy (in^4) +0.683 +0.681 +0.681 <br />Ixy (in^4) +0.021 +0.021 +0. <br />Io (in^4) +3.635 +3.633 +3.633 <br />rx (in) +1.503 +1.503 +1.503 <br />ry (in) +0.723 +0.722 +0.722 <br />ro (in) +1.668 +1.668 +1.668 <br />Y top (in)+2.314 +2.323 <br />Y bot (in)+2.186 +2.195 <br />Sx top (in^3)+1.276 +1.271 <br />Sx bot (in^3)+1.35 +1.345 <br />X right (in)+1.015 +1.035 <br />X left (in)+0.985 +1.007 <br />Sy right (in^3)+0.671 +0.658 <br />Sy left (in^3)+0.691 +0.676 <br />Zpx (in^3)+1.675 +1.675 <br />Zpy (in^3)+0.826 +0.826 <br />Max Mx (lb.in)+31890.6 +31763.421 <br />Max My (lb.in)+16786.58 +16449.725 <br />Mpx (lb.in)+41883.042 +41886.005 <br />Mpy (lb.in)+20640.256 +20639.342 <br />SFx +1.313 +1.319 <br />SFy +1.23 +1.255 <br />IMax (in^4)+2.952 <br />IMin (in^4)+0.681 <br />Theta (Deg)-0.538 <br />Elastic Neutral Axis <br />In (in^4)+2.948 <br />ENA Angle(°) +1.792 <br />Y top (in)+2.343 <br />Y bot (in)+2.217 <br />Sx top (in^3) +1.258 <br />Sx bot (in^3) +1.33 <br />X right (in)+1.087 <br />X left (in)+1.053 <br />Sy right (in^3) +0.63 <br />Sy left (in^3) +0.65 <br />Zpx (in^3) +1.674 <br />Zpy (in^3) +0.827 <br />Max Mx (lb.in) +31448.928 <br />Max My (lb.in) +15758.368 <br />Mpx (lb.in) +41850.973 <br />Mpy (lb.in) +20676.642 <br />SFx +1.331 <br />SFy +1.312 <br />Torque Max (lb.in) +6717.002 <br />Buckling <br />jy (monosymmetry) +0.339 in <br />jx (monosymmetry) -0.052 in <br />Cxrt Shear Constant +0.393 in^2 <br />Cyrt Shear Constant +0.287 in^2 <br />ßtf Torsional-flexural +0.949 <br />a Torsional-Bending +1.711 in <br />Area +1.306 in^2 <br />Mass/L +0.128 lb/ in <br />Xc -0.041 in <br />Yc +0. in <br />NA (Deg)+1.79 Deg <br />PNA (x,y)(-0.04,-0.13) <br />Torsion and Shear <br />J(Torsion)+0.874 in^4 <br />Cw(Warping) +0.962 in^6 <br />Xs (Shear) -0.059 in <br />Ys (Shear) +0.385 in <br />Ax +0.596 in^2 <br />Kx +0.456 <br />Ay +0.597 in^2 <br />Ky +0.457 <br />Ios +3.827 in^4 <br />ros +1.712 in <br />Swx +0.262 in^5 <br />Swy +0.061 in^5 <br />Dsc +0.385 in <br />Stressses Yield & Max/Min <br />Sig-yield T +25000. psi <br />Sig-yield C -25000. psi <br />Tau yield +15000. psi <br />Sig-x max T) +75.161 psi <br />Sig-x max C) -79.457 psi <br />Fpt +16328.504 lb <br />Fpc +16328.504 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 : 05-14-2024 / 10:45:21 <br /> Engineer : <br /> Client : <br /> Comment : <br /> Project Ref.: <br /> Project Name: TB-251 <br /> <br /> page 2/2Approved by: <br /> <br />V2018.1 - © MechaTools Technologies Inc. 2024 <br />This Product is licenced to : Keller Engineering <br />System Units: <br /> Length:[in] <br /> Mass :[lb] <br /> Stress:[psi] <br />Section Material Identiļ¬cation: <br />[Aluminium 6061 - T6(extruded)]: E=+10000000. [psi]; Nu=0.33; Ro=+0.098[lb/in³] <br />6