Tire mean dimensions of the cross section of the leading edge and torsion box of an airplane wing can be approximated as shown. If the wing is made of 2014-T6 aluminum alloy having an allowable shear stress τallow = 125MPa and the wall thickness is 10mm determine the maximum allowable torque and the corresponding angle of twist per meter length of the wing.
We need at least 10 more requests to produce the solution.
0 / 10 have requested this problem solution
The more requests, the faster the answer.