Tests were made in the Langley 16-foot transonic tunnel to determine the longitudinal and lateral stability and control characteristics and aileron hinge moments of a 0.087 scale model of a supercritical-wing research aircraft. Mach number was varied from 0.90 to 1.30 at a Reynolds number of approximately 2.4 million; angle of attack was varied from -8 degrees to 14 degrees; and angle of sideslip was set at about -5.5 degrees, 0 degrees, and 5.5 degrees. Aileron hinge moments were obtained at deflection angles of -15 degrees to 15 degrees. Aileron, horizontal-tail, and rudder effectiveness parameters were determined.


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    Titel :

    Stability and Control Characteristics: Including Aileron Hinge Moments of a Model of a Supercritical-Wing Research Airplane


    Beteiligte:
    R. J. Re (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    133 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch