A set of computer programs was developed to analyze flow through supersonic combustion ramjet (scramjet) inlets. These programs solve either the two or three dimensional Euler/Navier-Stokes equations in full conservation form by MacCormack's explicit or explicit-implicit method. An algebraic two-layer eddy viscosity model is used for turbulent flow calculations. The programs are operational in Control Data CYBER-200 series vector-processing computer system and were optimized to take maximum advantage of the vector processing capability of the system. Since their development, the programs were extensively verified and used to analyze a number of very complex inlet configurations. Results are presented from two-dimensional, quasi-three-dimensional, and three-dimensional analyses of the inlet flow field to illustrate the use of the program.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Numerical analysis of flow through scramjet engine inlets


    Beteiligte:
    Kumar, Ajay (Autor:in)


    Erscheinungsdatum :

    01.11.1987


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Scramjet Inlets

    M. K. Smart | NTIS | 2010


    Scramjet Inlets

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


    Analysis of Scramjet Inlets

    Kumar, A. | NTRS | 1987


    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