Cambered wing was tested in transonic wind tunnel with indented and nonindented body, and similar plane wing with indented body; conical camber reduced and delayed wing tip stall and reduced severity of its associated longitudinal instability; other results.


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    Titel :

    Transonic aerodynamic loading characteristics of wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for design mach number of root 2


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Cassetti, M.D. (Autor:in) / Re, R.J. (Autor:in) / Igoe, W.B. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    99 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :