Pressure distribution over thin airfoil of infinite span is calculated by integrating disturbances due to appropriate distribution of sources over forepart of Mach cone for point at which pressure is desired; result expressed in terms of Green's function giving pressure at any point on airfoil due to unit harmonic velocity at any other point. (correction) n 11 Nov p 630.


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    Titel :

    Aerodynamic forces on oscillating airfoil at supersonic speeds


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Miles, J.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1947


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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