Tentative method presented depends upon use of strip theory, in manner of E.G.BROADBENT, and calculation of lift distribution in transonic range for wings in roll, as suggested by K.W.MANGLER; aileron reversal criterion in transonic case.


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    Title :

    Note on problems of aileron reversal at transonic speeds


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Hunn, B.A. (author)

    Published in:

    Publication date :

    1953


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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