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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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