Two-level optimization technique of composite laminate panels by genetic algorithms
- 15 April 1996
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Genetic algorithms with local improvement for composite laminate designStructural and Multidisciplinary Optimization, 1994
- Design sensitivity analysis with isoparametric shell elementsStructural and Multidisciplinary Optimization, 1993
- Optimization of laminate stacking sequence for buckling load maximization by genetic algorithmAIAA Journal, 1993
- Stiffness design method of symmetric laminates using lamination parametersAIAA Journal, 1992
- Optimum design of laminated composite plates using lamination parametersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Stiffness Optimization of Orthotropic Laminated Composites Using Lamination ParametersAIAA Journal, 1991