A flight dynamic model of aircraft spinning was developed. It is capable of simulating aircraft behavior from conventional flight through stall, spin entry, steady spin, and spin recovery. A data base storage technique has been used to provide the six force and moment coefficients required. The data base embodies rotary balance data measured for a basic training aircraft plus computed small disturbance data calculated from a line vortex model.


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    Titel :

    Flight Dynamic Model of Aircraft Spinning


    Beteiligte:
    S. D. Hill (Autor:in) / C. A. Martin (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    45 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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