Spin resistance of two typical general aviation airplanes has been studied. Improvement in spin resistance due to an outboard wing leading-edge modification was evaluated through wind-tunnel and flight tests. The basic airplanes would readily enter a spin; however, with the wing modification the airplanes were highly spin resistant. Spin resistance has been related to the angle of attack of the outer wing panel and the yaw rate as a step toward development of guidelines for design of more spin resistant airplanes.


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    Titel :

    Use of a discontinuous wing leading-edge modification to enhance spin resistance for general aviation airplanes


    Beteiligte:
    Dicarlo, D. J. (Autor:in) / Glover, K. E. (Autor:in) / Stewart, E. C. (Autor:in) / Stough, H. P. (Autor:in)

    Erscheinungsdatum :

    1984-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Discontinuous wing leading edge to enhance spin resistance

    DICARLO, D. J. / GLOVER, K. E. / STEWART, E. C. et al. | AIAA | 1985


    Discontinuous wing leading edge to enhance spin resistance

    Dicarlo, D. J. / Glover, K. E. / Stewart, E. C. et al. | NTRS | 1985


    Development of spin resistance criteria for light general aviation airplanes

    DICARLO, D. / STOUGH, III, H. / GLOVER, K. et al. | AIAA | 1986


    Development of spin resistance criteria for light general aviation airplanes

    Dicarlo, D. J. / Stough, H. P., III / Glover, K. E. et al. | NTRS | 1986