THE changes in the relationship between the downwash behind a wing and the wing incidence in passing from flow at low values of Mach Number to flow at high values of Mach Number came to the notice of the author when investigating some high speed stressing cases.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Compressible Flow Behind a Wing


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


    Erscheinungsdatum :

    01.06.1942


    Format / Umfang :

    1 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Compressible flow behind wing

    Husk, D.I. | Engineering Index Backfile | 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