Simple technique presented for correcting singularities predicted by this theory at subsonic edges; thus, M.J.LIGHTHILL's rule for speeds on round nosed airfoils in incompressible flow is extended to higher approximations, compressible flow, 3-dimensional wings, sharp edges, and slender bodies of revolution.


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    Titel :

    Subsonic edges in thin-wing and slender-body theory


    Weitere Titelangaben:

    NACA -- Tech Note


    Beteiligte:
    Van Dyke, M.D. (Autor:in)


    Erscheinungsdatum :

    1954


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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