Methods introduced by M.M.MUNK extended to prove that liftcurve slope of thin wings in either subsonic or supersonic flow is same when direction of flight of wing is reversed.


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    Title :

    Reversibility theorem for thin airfoils in subsonic and supersonic flow


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Brown, C.E. (author)


    Publication date :

    1949


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :