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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    Titel :

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


    Beteiligte:
    F. Ghaffari (Autor:in) / B. Bates (Autor:in) / J. Luckring (Autor:in) / J. Thomas (Autor:in)

    Erscheinungsdatum :

    2004


    Format / Umfang :

    22 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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