A finite element analysis for the free vibration behaviour of doubly curved shells is presented in which eight-noded curved quadrilateral isoparametric finite elements are used. The first order shear deformation theory for thin and shallow shells is used in the formulation. Results are obtained for
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Interlaminar failure and buckling of doubly-curved laminated composite shells
β Scribed by A. Muc
- Publisher
- Springer US
- Year
- 1995
- Tongue
- English
- Weight
- 594 KB
- Volume
- 31
- Category
- Article
- ISSN
- 1573-8922
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