Report is first attempt to devise calculation method for representing buckling behavior of cylindrical shells of variable curvature; problem occurs, for instance, in dimensioning wing noses, stability behavior of which is decisively influenced by variability of curvature. English translation from (ZWB) Forschungsbericht n 1671 Sept 16 1942.
Stability of cylindrical shell of variable curvature
Nat Advisory Committee Aeronautics -- Tech Memo
1951
64 pages
Diagrs, Charts
Report
Englisch
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