Following methods introduced by J. HADAMARD, solution to thin airfoil problem in supersonic theory is given in terms of distribution of sources and doublets over given reference plane; nature of boundary values required discussed.


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    Title :

    Use of source-sink and doublet distributions extended to solution of arbitrary boundary value problems in supersonic flow


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


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


    Publication date :

    1948


    Size :

    48 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :