Three dimensional transonic visous flow computations are presented for a generic high-speed accelerator model which includes wing, body, fillets, and a no-flow through engine nacelle. Solutions are obtained from an algorithm for the compressible Navier-Stokes equations which incorporates an upwind-biased, flux-vector splitting approach along with longitudinally patched grids.


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    Title :

    Transonic Navier-Stokes Solutions About a Complex High-Speed Accelerator Configuration


    Contributors:
    F. Ghaffari (author) / B. Bates (author) / J. Luckring (author) / J. Thomas (author)

    Publication date :

    2004


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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