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
Step by Step Solution
3.38 Rating (151 Votes )
There are 3 Steps involved in it
The detailed ... View full answer
Get step-by-step solutions from verified subject matter experts
