The results were determined as a function of values at the wing trailing edge and at the Trefftz-plane. A correction for off the wing plane points is given. A description of the method, a FORTRAN listing of the coded method and results to be compared with theoretical and experimental values of downwash are presented.


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    Title :

    Downwash Calculation at Close Range Behind a Trapezoidal Wing in Supersonic Flow


    Contributors:

    Publication date :

    1980


    Size :

    37 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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