Further applications of a three-dimensional Euler code which is able to treat arbitrary aerodynamic configurations in a wide range of flight conditions are presented. Previous publications have demonstrated the ability of the code to handle complex aircraft configurations. The present applications verify the code in flight regimes not covered by potential codes (e.g., high supersonic flow and vortex flow) by comparison with reliable, internationally reported wind tunnel experiments and analytical solutions (where available). A short description of the code is also included.


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    Title :

    Euler Solver for Arbitrary Configurations: Further Applications


    Contributors:
    B. Epstein (author) / A. L. Luntz (author) / A. Nachshon (author)

    Publication date :

    1990


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Cartesian Euler method for arbitrary aircraft configurations

    EPSTEIN, BORIS / LUNTZ, ALEXANDER L. / NACHSHON, AHARON | AIAA | 1992


    Cartesian Euler method for arbitrary aircraft configurations

    Epstein, B. / Luntz, A.L. / Nachshon, A. | Tema Archive | 1992