Perturbation field induced by line vortex in supersonic stream and downwash behind supersonic lifting surface, examined to establish approximate methods for determining downwash behind supersonic wings.


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    Title :

    Line-vortex theory for calculation of supersonic downwash


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Mirels, H. (author) / Haefeli, R.C. (author)


    Publication date :

    1950


    Size :

    16 pages


    Remarks:

    Diagrs, Graphs


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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