Use of genetic algorithms for optimal design of laminated composite sandwich panels with bending-twisting coupling
- 15 April 1996
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Optimal design of laminated composite structures using coarse-grain parallel genetic algorithmsComputing Systems in Engineering, 1994
- Stacking sequence optimization of simply supported laminates with stability and strain constraintsAIAA Journal, 1992
- Shear Correction Factors for Orthotropic Laminates Under Static LoadJournal of Applied Mechanics, 1973
- Elastic wave propagation in heterogeneous platesInternational Journal of Solids and Structures, 1966