Composed of frictional and pressure resistance; method is based on limiting theory that separation of boundary layer is slight; pressure resistance is thus calculated from boundary layer coefficients.


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    Title :

    Theoretical calculation of airfoil profile drag


    Additional title:

    Zur theoretischen Berechnung des Profilwiderstandes


    Contributors:
    Pretsch, J. (author)


    Publication date :

    1938


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :


    Airfoil Profile Drag

    M. A. Schwartzberg | NTIS | 1975


    Theoretical Predication of Airfoil Drag Polars

    Nark, Theodore C. | SAE Technical Papers | 1968


    Airfoil profile drag increase due to acoustic excitation

    SHEARIN, JOHN / JONES, MICHAEL | AIAA | 1989