Methods of solution given for two- and three-dimensional steady state and two-dimensional unsteady state equations of compressible flow.


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    Title :

    Application of green's theorem to solution of boundary-value problems in linearized supersonic wing theory


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


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


    Publication date :

    1949


    Size :

    41 pages


    Remarks:

    Diagrams, Photographs, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :