Basic assumption underlying work is that downwash behind wing is dependent only upon lift coefficient of wing which produces it and is independent of incidence; equations furnish proof of contention.


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    Title :

    Compressible flow behind wing


    Additional title:

    Aircraft Eng


    Contributors:
    Husk, D.I. (author)

    Published in:

    Publication date :

    1942


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Compressible Flow Behind a Wing

    Husk, D.I. | Emerald Group Publishing | 1942


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    ICAS-92-7.4.1 An Adaptive Region Method for Computation of Vortex Sheet Behind a Wing in Compressible Flow

    Sun, G. / Qiao, Z. D. / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1992


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    Wichmann, G. | British Library Online Contents | 1994