Perturbation field induced by line vortex in supersonic stream and downwash behind supersonic lifting surfaces are examined for purpose of establishing approximate methods for determining downwash behind supersonic wings; lifting line methods are presented for calculating supersonic downwash.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Line vortex theory for calculation of supersonic downwash


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


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


    Erscheinungsdatum :

    1949


    Format / Umfang :

    54 pages


    Anmerkungen:

    Diagrs, Charts


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Line-vortex theory for calculation of supersonic downwash

    Mirels, H. / Haefeli, R.C. | Engineering Index Backfile | 1950


    Line-vortex theory for calculation of supersonic downwash

    Mirels, Harold / Haefeli, Rudolph C. | TIBKAT | 1949


    Line-vortex theory for calculation of supersonic downwash

    Mirels, Harold / Haefeli, Rudolph C | NTRS | 1949


    Downwash behind wings at supersonic speeds

    Jacobs, W. | Engineering Index Backfile | 1955


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

    Heaslet, M.A. / Lomax, H. | Engineering Index Backfile | 1948