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

    Publication date :

    1982


    Size :

    67 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English