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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Transonic Perturbation Analysis of Wing-Fuselage-Nacelle-Pylon Configurations with Powered Jet Exhausts


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

    Erscheinungsdatum :

    1982


    Format / Umfang :

    67 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Block-structured solution of transonic flows around wing/pylon/nacelle configurations

    ECER, A. / SPYROPOULOS, J. / ROUT, R. et al. | AIAA | 1989



    Unsteady Wing-Pylon-Nacelle Interference in Transonic Flow

    Dietz, Guido / Mai, Holger / Schroeder, Andreas et al. | AIAA | 2007