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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    Title :

    Flight Dynamic Model of Aircraft Spinning


    Contributors:
    S. D. Hill (author) / C. A. Martin (author)

    Publication date :

    1990


    Size :

    45 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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