A numerical method is developed to analyze the inviscid flowfield of a high speed inlet by the solution of the Euler equations. The LU 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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    Title :

    An LU implicit scheme for high speed inlet analysis


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

    Publication date :

    1986-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    An LU implicit scheme for high speed inlet analysis

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


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


    Lower-upper implicit scheme for high-speed inlet analysis

    Yoon, Seokkwan / Jameson, Anthony | NTRS | 1987


    An LU implicity scheme for high speed inlet analysis

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