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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    Titel :

    Compressible flow behind wing


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Husk, D.I. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1942


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Compressible Flow Behind a Wing

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


    An Adaptive Region Method for Computation of Vortex Sheet Behind a Wing in Compressible Flow

    Sun, G. / Qiao, Z. D. | British Library Online Contents | 1992


    FLAPPING-WING THRUST IN COMPRESSIBLE FLOW

    Send, W. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2006


    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


    Investigations Concerning Wing-Body-Interference for Compressible Flow

    Wichmann, G. | British Library Online Contents | 1994