Perturbation field induced by line vortex in supersonic stream and downwash behind supersonic lifting surface, examined to establish approximate methods for determining downwash behind supersonic wings.


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    Titel :

    Line-vortex theory for calculation of supersonic downwash


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Mirels, H. (Autor:in) / Haefeli, R.C. (Autor:in)


    Erscheinungsdatum :

    1950


    Format / Umfang :

    16 pages


    Anmerkungen:

    Diagrs, Graphs


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Line vortex theory for calculation of supersonic downwash

    Mirels, H. / Haefeli, R.C. | Engineering Index Backfile | 1949


    Calculation of downwash behind supersonic wing

    Ward, G.N. | Engineering Index Backfile | 1949


    Note on evaluation of supersonic downwash integral

    Hunn, B.A. | Engineering Index Backfile | 1954


    Calculation of downwash behind supersonic wings with application to triangular plan forms

    Lomax, H. / Sluder, L. / Heaslet, M.A. | Engineering Index Backfile | 1950