General formulation of 3-dimensional flow problem with application to calculation of wall interference in wind tunnel testing at high speeds is given; wing theory is examined from usual point of view; this involves derivation of Biot-Savart law for compressible flow by Glauert-Prandtl approximation. (See also - discussion in n 4 Oct p 432)


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    Title :

    Glauert-Prandtl approximation for subsonic flows of compressible fluid


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Hsue-Shen Tsien (author) / Lees, L. (author)


    Publication date :

    1945


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :