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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    Titel :

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


    Beteiligte:
    Wai, J. C. (Autor:in) / Sun, C. C. (Autor:in) / Yoshihara, H. (Autor:in)

    Erscheinungsdatum :

    1982-02-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




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