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
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Stability of the cylindrical shell of variable curvature
TIBKAT | 1951
|Developments in cylindrical shell stability analysis
AIAA | 1997
|Stability of a cylindrical shell of variable thickness depending on the nonuniform radial load
British Library Online Contents | 2014
|Design and manufacture of a variable-stiffness cylindrical shell
Tema Archive | 2009
|