Proceeding from fundamental problem on mutual relation of wing and free boundaries, distribution of circulation is determined for airfoil spaning open jet of rectangular section at different aspect ratios, and then for open jet of circular section; solution obtained by means of Fourier series; experiments performed for purpose of proving theory.


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    Title :

    Airfoil spanning open jet


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:
    Stueper, J. (author)


    Publication date :

    1933


    Size :

    22 pages


    Remarks:

    9 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    An airfoil spanning an open jet

    Stüper, J. | TIBKAT | 1933


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