A method for aerodynamic shape optimization based on a genetic algorithm approach is demonstrated. The algorithm is coupled with a transonic full potential flow solver and is used to optimize the flow about transonic wings including multi-objective solutions that lead to the generation of pareto fronts. The results indicate that the genetic algorithm is easy to implement, flexible in application and extremely reliable.


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    Title :

    Transonic Wing Shape Optimization Using a Genetic Algorithm


    Contributors:

    Conference:

    Transonicum IV ; 2002 ; Goettingen, Germany


    Publication date :

    2002-07-05


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English




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