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Buckling of thick orthotropic cylindrical shells under combined external pressure and axial compression

โœ Scribed by Kardomateas, G. A.; Philobos, M. S.

Book ID
125511123
Publisher
American Institute of Aeronautics and Astronautics
Year
1995
Tongue
English
Weight
865 KB
Volume
33
Category
Article
ISSN
0001-1452

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๐Ÿ“œ SIMILAR VOLUMES

Post-buckling analysis of imperfect stif
Post-buckling analysis of imperfect stiffened laminated cylindrical shells under combined external pressure and axial compression
โœ Hui-Shen Shen ๐Ÿ“‚ Article ๐Ÿ“… 1997 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 961 KB

A post-buckling analysis is presented for a stiffened laminated cylindrical shell of finite length subject to combined loading of external pressure and axial compression. The formulations are based on a boundary layer theory of shell buckling which includes the effects of the nonlinear pre-buckling