Analytical expressions derived for downwash throughout entire induced flow field of lifting triangles of infinite chord with leading edges either in front of or behind Mach cone.


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    Title :

    Charts for conical part of downwash field of swept wings at supersonic speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :