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Buckling of moderately thick, laminated cylindrical shells under torsion

โœ Scribed by Tabiei, A.; Simitses, G. J.


Book ID
121255936
Publisher
American Institute of Aeronautics and Astronautics
Year
1994
Tongue
English
Weight
869 KB
Volume
32
Category
Article
ISSN
0001-1452

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Buckling of moderately thick laminated c
โœ George J. Simitses ๐Ÿ“‚ Article ๐Ÿ“… 1996 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 946 KB

The present paper is a review article on the problem of buckling of moderately thick, laminated, composite shells subjected to destabilizing loads. The loads consist of uniform axial compression, uniform lateral pressure and torsion applied individually or in combination. In all the works reported i