## Abstract A method is presented for the minimum weight optimum design of laminated fibre composite plates, subject to multiple inplane loading conditions, which includes stiffness, strength and elastic stability constraints. The buckling analysis is based on an equivalent orthotropic plate approa
Optimum design of composite laminates with STROPT
β Scribed by Belsare, S. ;Haririan, M.
- Publisher
- John Wiley and Sons
- Year
- 1993
- Tongue
- English
- Weight
- 419 KB
- Volume
- 9
- Category
- Article
- ISSN
- 1069-8299
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