An extension is made to the theory on which most aircraft pressure cabins are designed. In the existing theory the effect of the curvature of the deformed cylinder is neglected. This paper examines the manner in which this effect influences the stress distribution.
Pressure Cabin Analysis
An Extension to Existing Theory
Aircraft Engineering and Aerospace Technology ; 32 , 5 ; 126-131
1960-05-01
6 pages
Article (Journal)
Electronic Resource
English
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