The grid embedding scheme is used to solve the whole flowfields around the combined configuration of the Hope, H-II rocket and rocket booster designed by the National Space Development Agency (NASDA). Three computational grids are overlapped with each other and the solutions are combined by interpolation at the boundaries. The Harten type Total Variation Diminishing (TVD) scheme is used to solve the Euler equations for hypersonic flow from M = 1.3 to 2.5, and it is shown the results of numerical simulation using the present methods are reasonable.


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    Title :

    Numerical Simulations of Flow around a Body of Complex Configurations


    Contributors:
    S. Ogawa (author) / Y. Wada (author) / T. Ishiguro (author) / Y. Takakura (author)

    Publication date :

    1989


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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