The AD-1 is a variable-sweep oblique-wing research airplane that exhibits unconventional stability and control characteristics. In this report, flight-determined and predicted stability and control derivatives for the AD-1 airplane are compared. The predictions are based on both wind tunnel and computational results. A final best estimate of derivatives is presented.


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    Title :

    Flight-Determined Aerodynamic Derivatives of the AD-1 Oblique-Wing Research Airplane


    Contributors:
    A. G. Sim (author) / R. E. Curry (author)

    Publication date :

    1984


    Size :

    39 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English