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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    Titel :

    Transonic Wing Shape Optimization Using a Genetic Algorithm


    Beteiligte:
    Holst, Terry L. (Autor:in) / Pulliam, Thomas H. (Autor:in) / Kwak, Dochan (Autor:in)

    Kongress:

    Transonicum IV ; 2002 ; Goettingen, Germany


    Erscheinungsdatum :

    05.07.2002


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch




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