Aerodynamic influence of wings on tailplane loads; downwash induced in plane of symmetry of aircraft when wings have straight leading edges whose sweepback is such that they are subsonic in supersonic main stream; downwash due to delta wing at incidence, having simple triangular planform, case of swallow tail wings.


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    Titel :

    Note on evaluation of supersonic downwash integral


    Weitere Titelangaben:

    Aeronautical Quarterly


    Beteiligte:
    Hunn, B.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1954


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Calculation of downwash behind supersonic wing

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


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


    Downwash

    Online Contents | 1999


    Unsteady downwash of supersonic flow at wing's rear edge

    Kislyagin, N.N. | Engineering Index Backfile | 1964