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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    Title :

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


    Additional title:

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


    Contributors:
    Shankar, V. (author) / Malmuth, N.D. (author) / Cole, J.D. (author)

    Published in:

    Publication date :

    1979


    Size :

    14 Seiten, 11 Bilder, 17 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English