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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Heaslet, M.A. (author) / Lomax, H. (author) / Jones, A.L. (author)


    Publication date :

    1947


    Size :

    56 pages


    Remarks:

    Bibliography, 21 Supp Sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    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 | European Patent Office | 2023

    Free access