A numerical finite-volume method is proposed for solving the Euler equations of a steady three-dimensional flow. The subsonic regions embedded in steady supersonic flow about aircraft are computed by introducing a time-dependent coordinate system that maps the fuselage and wing into one coordinate surface. The suitability of the method to a delta-winged aircraft is demonstrated, and its applicability to rectangular-winged aircraft and problems in internal transonic flow is pointed out.


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    Title :

    Finite-volume solution of the Euler equations for steady three-dimensional transonic flow


    Contributors:
    Rizzi, A. (author) / Bailey, H. (author)

    Conference:

    International Conference on Numerical Methods in Fluid Dynamics ; 1976 ; Enschede, Netherlands


    Publication date :

    1976-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :




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