The e}ect of local geometric imperfections on the buckling and postbuckling of composite laminated cylindrical shells subjected to combined axial compression and uniform temperature loading was investigated[ The two cases of compressive postbuckling of initially heated shells and of thermal postbuck
Thermal postbuckled vibrations of symmetrically laminated composite plates with initial geometric imperfections
โ Scribed by J. Girish; L.S. Ramachandra
- Publisher
- Elsevier Science
- Year
- 2005
- Tongue
- English
- Weight
- 321 KB
- Volume
- 282
- Category
- Article
- ISSN
- 0022-460X
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๐ SIMILAR VOLUMES
Thermal postbuckling analysis is presented for a simply supported, shear deformable laminated plate subjected to a uniform temperature rise and resting on an elastic foundation. The material properties of the composite are assumed to be functions of temperature. The formulations are based on Reddy's
The geometrically non-linear free vibration of thin composite laminated plates is investigated by using a theoretical model based on Hamilton's principle and spectral analysis previously applied to obtain the non-linear mode shapes and resonance frequencies of thin straight structures, such as beams