As result of trend toward thicker skin and fewer stiffening elements in aircraft construction larger fraction of load is being carried by skin and thus ability to predict behavior of skin under load has become more important; method of analysis developed to solve these problems. (published 1949, 20¢)
Simplified method of elastic-stability analysis for thin cylindrical shells
Nat Advisory Committee Aeronautics -- Report
1947
25 pages
Report
English
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Engineering Index Backfile | 1947
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