Surface integral developed which yields solutions of linearized partial differential equation for supersonic flow; these solutions satisfy boundary conditions arising in wing theory; particular applications of this general method are made using acceleration potentials, to flat surface and to uniformly loaded lifting surfaces.


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    Titel :

    Volterra's solution of wave equation as applied to three-dimensional supersonic airfoil problems


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Heaslet, M.A. (Autor:in) / Lomax, H. (Autor:in) / Jones, A.L. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    56 pages


    Anmerkungen:

    Bibliography, 21 Supp Sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Volterra's solution of wave equation as applied to three-dimensional supersonic airfoil problems

    Heaslet, M.A. / Lomax, H. / Jones, A.L. | Engineering Index Backfile | 1947



    Volterraś solution of the wave equation as applied to three-dimensional supersonic airfoil problems

    Heaslet, Max A. / Lomax, Harvard / Jones, Arthur L. | TIBKAT | 1947



    Airfoil With Supersonic Wave-Tripping Structure

    O'LEARY PATRICK | Europäisches Patentamt | 2023

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