Design optimization of composites using genetic algorithms and failure mechanism based failure criterion
- 30 June 2008
- journal article
- research article
- Published by Elsevier in Composite Structures
- Vol. 83 (4), 354-367
- https://doi.org/10.1016/j.compstruct.2007.05.005
Abstract
No abstract availableKeywords
This publication has 15 references indexed in Scilit:
- On the effect of progressive damage on composite helicopter rotor system behaviorComposite Structures, 2007
- Multi-objective optimization of cutting parameters for drilling laminate composite materials by using genetic algorithmsComposites Science and Technology, 2006
- Modeling progressive damage accumulation in thin walled composite beams for rotor blade applicationsComposites Science and Technology, 2006
- Strength design of composite beam using gradient and particle swarm optimizationComposite Structures, 2006
- Design optimization of a two-dimensional hydrofoil by applying a genetic algorithmEngineering Optimization, 2006
- Optimization of piezoelectric sensor location for delamination detection in composite laminatesEngineering Optimization, 2006
- A failure mechanism based failure theory for laminated composites including the effect of shear stressComposite Structures, 2005
- Towards a Rational Failure Criterion for Unidirectional Composite LaminaeMechanics of Advanced Materials and Structures, 2005
- A failure mechanism-based approach for design of composite laminatesComposite Structures, 1999
- Optimization of laminate stacking sequence for buckling load maximization by genetic algorithmAIAA Journal, 1993