A numerical simulation of transonic flows over complete ASKA aircraft configuration is performed. A computational grid system is constructed using the algebraic multi-block method. The Euler equations are numerically solved by the upwind finite volume scheme.


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    Title :

    Aerodynamic Simulation for Complete ASKA Aircraft Configuration


    Contributors:
    S. Takanashi (author) / K. Sawada (author)

    Publication date :

    1987


    Size :

    4 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English