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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    Titel :

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


    Beteiligte:
    A. Hasselrot (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    37 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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