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
β¦ LIBER β¦
Buckling of moderately thick, laminated cylindrical shells under lateral pressure
β Scribed by G.J. Simitses; A. Tabiei; J.S. Anastasiadis
- Publisher
- Elsevier Science
- Year
- 1993
- Weight
- 537 KB
- Volume
- 3
- Category
- Article
- ISSN
- 0961-9526
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