Postbuckling and vibration analyses considering large thermopiezoelastic de#ections are performed for fully symmetric and partially eccentric piezolaminated composite plates. Non-linear "nite element equations based on the layerwise displacement theory are formulated for piezolaminated plates subjec
Postbuckling of multilayered composite plates subjected to combined axial and thermal loads
โ Scribed by Ahmed K. Noor; Jeanne M. Peters
- Publisher
- Elsevier Science
- Year
- 1992
- Tongue
- English
- Weight
- 733 KB
- Volume
- 11
- Category
- Article
- ISSN
- 0168-874X
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