NASCRIN program analyzes two-dimensional flow fields in supersoniccombustion ramjet (scramjet) inlets. Solves two-dimensional Euler or Navier-Stokes equations in conservative form by unsplit, explicit, two-step finite-difference method. More recent explicit/implicit, two-step scheme incorporated by analysis of viscous flow. Algebraic, two-layer eddy-viscosity model used for turbulent-flow calculations. Vectorized version, written for CDC CYBER 205, whereas scalar version, can be run on CRAY or other scalar computers.


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    Titel :

    Analysis of Scramjet Inlets


    Beteiligte:
    Kumar, A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.03.1987



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Scramjet Inlets

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    Murthy, S.N.B. / Curran, E.T. | AIAA | 2001


    Analysis of Scramjet Inlets

    Kumar, A. | NTRS | 1986


    CFD for scramjet inlets

    Gaible, F. / Garnero, P. / Keghian, S. et al. | British Library Conference Proceedings | 1995


    CFD for scramjet inlets

    Gaible, F. / Garnero, P. / Keghian, S. | British Library Online Contents | 1995