Janzen-Rayleigh method used to calculate velocity potential for steady subsonic compressible flow; formulas obtained for fluid velocity at solid boundary and along axis of symmetry.


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    Title :

    Subsonic flow past paraboloid of revolution


    Additional title:

    NACA -- Tech Note


    Contributors:
    Kaplan, C. (author)


    Publication date :

    1957


    Size :

    21 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :






    Subsonic gas flow past wing profile

    Christianovich, S.A. / Yurev, I.M. | Engineering Index Backfile | 1950