It is presently demonstrated that highly cambered, low aspect ratio airfoil configurations can be neither experimentally nor numerically developed on the basis of two-dimensional methods; the strong dependency of airfoil shape on aspect ratio requires the definition of a planform to be conducted first, in order to serve as input for three-dimensional optimization methods. It is found that even the simplified three-dimensional computational method presently employed can accelerate a multielement-airfoil wing development.


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    Titel :

    Aerodynamics of high-lift, low-aspect-ratio unswept wings


    Beteiligte:
    Katz, Joseph (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.08.1989



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :