A numerical method is developed to analyze the inviscid flowfield of a high speed inlet by the solution of the Euler equations. The lower-upper implicit scheme in conjunction with adaptive dissipation proves to be an efficient and robust nonoscillatory shock capturing technique for high Mach number flows as well as for transonic flows.


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    Titel :

    An LU implicity scheme for high speed inlet analysis


    Beteiligte:
    Yoon, S. (Autor:in) / Jameson, A. (Autor:in)

    Kongress:

    Joint Propulsion Conference ; 1986 ; Huntsville, AL, United States


    Erscheinungsdatum :

    01.04.1986


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    An LU implicit scheme for high speed inlet analysis

    Yoon, S. / Jameson, A. | NTRS | 1986


    An LU implicit scheme for high speed inlet analysis

    YOON, S. / JAMESON, A. | AIAA | 1986


    Lower-upper implicit scheme for high-speed inlet analysis

    YOON, SEOKKWAN / Sverdrup Technology / Inc. et al. | AIAA | 1987


    Lower-upper implicit scheme for high-speed inlet analysis

    Yoon, Seokkwan / Jameson, Anthony | NTRS | 1987


    Inlet Design for High-Speed Propfans

    Little, B. H. / Hinson, B. L. | SAE Technical Papers | 1982