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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    An LU implicity scheme for high speed inlet analysis


    Contributors:
    Yoon, S. (author) / Jameson, A. (author)

    Conference:

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


    Publication date :

    1986-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


    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