A method using a transonic small disturbance code with successive line over-relaxation is described for treating wing/fuselage configurations with a nacelle/pylon/powered jet. Examples illustrating its use for the NASA transport research model are given. Reasonable test/theory comparisons were obtained.


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    Title :

    Transonic perturbation analysis of wing-fuselage-nacelle-pylon configurations with powered jet exhausts


    Contributors:
    Wai, J. C. (author) / Sun, C. C. (author) / Yoshihara, H. (author)

    Publication date :

    1982-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :