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Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm

AIAA Journal · 1993 · Vol. 31(5) · pp. 951–956
Rodolphe Le RicheRaphael T. Haftka

Abstract

The use of a genetic algorithm to optimize the stacking sequence of a composite laminate for buckling load maximization is studied. Various genetic parameters including the population size, the probability of mutation, and the probability of crossover are optimized by numerical experiments. A new genetic operator - permutation - is proposed and shown to be effective in reducing the cost of the genetic search. Results are obtained for a graphite-epoxy plate, first when only the buckling load is considered, and then when constraints on ply contiguity and strain failure are added. The influence on the genetic search of the penalty parameter enforcing the contiguity constraint is studied. The advantage of the genetic algorithm in producing several near-optimal designs is discussed.

Composite Structure Analysis and OptimizationTopology Optimization in EngineeringAeroelasticity and Vibration ControlStackingBucklingSequence (biology)Genetic algorithmMaximizationStructural engineeringAlgorithmMaterials scienceComputer scienceMathematical optimization

Funding

  • National Aeronautics and Space Administration
Citations
583
FWCI
28.94
field-weighted impact
References
14
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Cited by
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International Journal for Numerical Methods in Engineering · 2005 · 720 citations
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