Question
Two cylindrical fuselage shells carry the same internal pressure. The shell thickness of the first is twice that of the second and the diameter
Two cylindrical fuselage shells carry the same internal pressure. The shell thickness of the first is twice that of the second and the diameter of first is 3 times that of the second. The ratio of longitudinal stress of the first shell to that of the second is (a) 2/3 (b) 3/2 (c) 3/400 02 (d) 4/3
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Mechanics of Materials
Authors: Russell C. Hibbeler
10th edition
134319656, 978-0134319650
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