Method system, and product from application of the method, for design of a subsonic airfoil shape, beginning with an arbitrary initial airfoil shape and incorporating one or more constraints on the airfoil geometric parameters and flow characteristics. The resulting design is robust against variations in airfoil dimensions and local airfoil shape introduced in the airfoil manufacturing process. A perturbation procedure provides a class of airfoil shapes, beginning with an initial airfoil shape.


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    Titel :

    Robust, optimal subsonic airfoil shapes


    Beteiligte:
    Rai, Man Mohan (Autor:in)

    Erscheinungsdatum :

    18.11.2008


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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