Planar laser-induced fluorescence (PLIF) of OH and wall-pressure measurements have been used to investigate the combustion in a cavity flame- holder scramjet combuster.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hydrocarbon-Fueled Scramjet Research at Hypersonic Mach Numbers


    Beteiligte:
    F. Houwing (Autor:in)

    Erscheinungsdatum :

    2005


    Format / Umfang :

    138 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Hydrocarbon and Hydrogen-Fueled Scramjet Cavity Flameholder Performance at High Flight Mach Numbers

    Boyce, Russell / Houwing, Frank / Neely, Andrew et al. | AIAA | 2003


    Development of Hydrocarbon-Fueled Scramjet Engines: The Hypersonic Technology (HyTech) Program

    O. A. Powell / J. T. Edwards / R. B. Norris et al. | AIAA | 2001


    Hydrocarbon-fueled scramjet combustor investigation

    KAY, I. / PESCHKE, W. / GUILE, R. | AIAA | 1990


    Hydrocarbon-fueled scramjet combustor investigation

    KAY, I. W. / PESCHKE, W. T. / GUILE, R. N. | AIAA | 1992


    Hydrocarbon-fueled scramjet combustor investigation

    Kay, I. W. / Peschke, W. T. / Guile, R. N. | NTRS | 1992