A portion of an airplane fuselage can be approximated by the cross section shown. If the t...
A portion of an airplane fuselage can be approximated by the cross section shown. If the thickness of iis 20l4-T6-aluminum skin is 10 mm. determine the maximum wing torque. T that can be applied if τallow = 4 MPa. Also, in a i m long-section, del ermine the angle ol twist.
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