The mean dimensions of the cross section of an airplane fuselage are shown. If the fuselage is
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The mean dimensions of the cross section of an airplane fuselage are shown. If the fuselage is made of 2014-T6 aluminum alloy having allowable shear stress of τallow = 18 ksi, and it is subjected to a torque of 6000 kip ft, determine the required minimum thickness t of the cross section to the nearest 1/16 in. Also, find the corresponding angle of twist per foot length of the fuselage.
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