PROBLEMS 14.11. The skin on the upper side of an airplane wing is of 24S-T Alclad material. The s...
PROBLEMS 14.11. The skin on the upper side of an airplane wing is of 24S-T Alclad material. The stringer spacing is 5 in. and the rib spacing is 20 in. Assuming the edges to be simply supported, find the compression buckling stress for skin gages of (a) 0.020 in., (b) 0.032 in, (e) 0.040 in., and (a) 0.064 in.
PROBLEMS 14.11. The skin on the upper side of an airplane wing is of 24S-T Alclad material. The stringer spacing is 5 in. and the rib spacing is 20 in. Assuming the edges to be simply supported, find the compression buckling stress for skin gages of (a) 0.020 in., (b) 0.032 in, (e) 0.040 in., and (a) 0.064 in.