A computational transonic design procedure for three-dimensional wings in which shapes are determined supporting prescribed pressure distributions, is presented. The method uses an existing three-dimensional modified small disturbance theory analysis code to include the design procedure. A consistent analysis-design differencing procedure at the wing slit is implemented. Design results are presented for aft and forward swept wings in isolation as well as in the presence of a fuselage. Performance of the designed wing at off-design Mach number and in the presence of solid and free jet wind tunnel walls is also reported. (DePo)


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    Titel :

    Computational transonic design procedure for three-dimensional wings and wing-body combinations


    Weitere Titelangaben:

    Rechnergestuetzte Konstruktion dreidimensionaler Fluegel und von Fluegel-Koerperkombinationen fuer den transsonischen Bereich


    Beteiligte:
    Shankar, V. (Autor:in) / Malmuth, N.D. (Autor:in) / Cole, J.D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1979


    Format / Umfang :

    14 Seiten, 11 Bilder, 17 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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