A brief history of stall/spin technology for light general aviation airplanes is presented. Criteria needed to describe desirable characteristics of a spin-resistant airplane and means to evaluate airplanes for compliance with the criteria have been developed. Initial results from limited flight tests of an experimental high-wing airplane indicated that the basic configuration would not meet the spin resistance criteria. Further tests with the airplane modified to enhance its spin resistance are planned.


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    Titel :

    Development of spin resistance criteria for light general aviation airplanes


    Beteiligte:
    Dicarlo, D. J. (Autor:in) / Stough, H. P., III (Autor:in) / Glover, K. E. (Autor:in) / Brown, P. W. (Autor:in) / Patton, J. M., Jr. (Autor:in)

    Erscheinungsdatum :

    01.04.1986


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch