Theoretical calculation of pressure distribution, span loading, and rolling moment due to sideslip at supersonic speeds for thin sweptback tapered wings with supersonic trailing edges and wing tips parallel to axis of wing symmetry.


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    Title :

    Theoretical calculation of pressure distribution, span loading, and rolling moment due to sideslip at supersonic speeds for thin sweptback tapered wings with supersonic trailing edges and wing tips parallel to axis of wing symmetry


    Additional title:

    NACA -- Tech Note


    Contributors:
    Margolis, K. (author) / Sherman, W.L. (author) / Hannah, M.E. (author)


    Publication date :

    1953


    Size :

    70 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :