CNS, a new computational fluid dynamics procedure, has been developed to aid in hypersonic vehicle design. The code can be used to model the entire external flow around hypersonic vehicle shapes, from the captured shock at the nose to the beginning of the wake. Unlike space-marching codes, the technique allows axially separated flow regions to be modeled. Validation trials using sphere-cone data reveal good solution accuracy for the surface pressure and flowfield temperature.


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    Titel :

    Development and validation of CNS (compressible Navier-Stokes) for hypersonic external flows


    Beteiligte:
    Flores, Jolen (Autor:in) / Chow, Chuen-Yen (Autor:in) / Ryan, James S. (Autor:in)

    Erscheinungsdatum :

    01.06.1989


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Development and validation of CNS (compressible Navier-Stokes) for hypersonic external flows

    RYAN, JAMES S. / FLORES, JOLEN / CHOW, CHUEN-YEN | AIAA | 1989


    Transformation of the hypersonic compressible Navier-Stokes equations.

    ROGERS, D. F. / U.S. Navy / Officeof Naval Research et al. | AIAA | 1973


    Development and validation of a Navier-Stokes code for hypersonic external flow

    Ryan, James Stevenson / Chow, Chuen-Yen / Flores, Jolen | NTRS | 1990


    Development and validation of a Navier-Stokes code for hypersonic external flow

    RYAN, JAMES STEVENSON / CHOW, CHUEN-YEN / FLORES, JOLEN | AIAA | 1990


    Navier-Stokes results for hypersonic inlet flows

    BRENNEIS, A. / WANIE, K. | AIAA | 1991