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.


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    Title :

    Compressible Flow Behind a Wing


    Contributors:
    Husk, D.I. (author)


    Publication date :

    1942-06-01


    Size :

    1 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Compressible flow behind wing

    Husk, D.I. | Engineering Index Backfile | 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


    Investigations Concerning Wing-Body-Interference for Compressible Flow

    Wichmann, G. | British Library Online Contents | 1994