Canard model had twisted wing with 67° of sweepback and aspect ratio of 2.91 and 3-trapezoidal canard surfaces having ratios of exposed area to wing area of 0.032, 0.076, and 0.121; details of outboard tail model; longitudinal characteristics of models were obtained for various control deflections, and lateral stability derivatives over maximum test angle of attack of -2 to 22° for lower test Mach numbers.


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    Titel :

    Aerodynamic characteristics of canard and outboard-tail airplane model at high subsonic speeds


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Fournier, P.G. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    67 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :