Contents include the folloving: 1. Motivation. Support NASA's 3d generation launch vehicle technology program. RBCC is promising candidate for 3d generation propulsion system. 2. Approach. Focus on ejector mode p3erformance (Mach 0-3). Perform testing on established flowpath geometry. Use conventional propulsion measurement techniques. Use advanced optical diagnostic techniques to measure local combustion gas properties. 3. Objectives. Gain physical understanding of detailing mixing and combustion phenomena. Establish an experimental data set for CFD code development and validation.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Recent Experimental Results Related to Ejector Mode Studies of Rocket-Based Combined Cycle (RBCC) Engines


    Beteiligte:
    Cramer, J. M. (Autor:in) / Pal, S. (Autor:in) / Marshall, W. M. (Autor:in) / Santoro, R. J. (Autor:in)

    Kongress:

    MSFC Spring Fluids Workshop ; 2003 ; Birmingham, AL, United States


    Erscheinungsdatum :

    2003-01-01


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Experimental investigation of the RBCC rocket-ejector mode

    Lehman, M. / Pal, S. / Santoro, R. | AIAA | 2000


    Focused Rocket-Ejector RBCC Experiments

    R. J. Santoro / S. Pal | NTIS | 2003


    Focused Rocket-Ejector RBCC Experiments

    Santoro, Robert J. / Pal, Sibtosh | NTRS | 2003


    Rocket Ejector Studies for Application to RBCC Engines: An Integrated Experimental/CFD Approach

    Pal, S. / Lehman, M. / Broda, J. C. et al. | British Library Conference Proceedings | 1997


    Options for Flight Testing Rocket-Based Combined-Cycle (RBCC) Engines

    Olds, J. / American Institute of Aeronautics and Astronautics / Society of Automotive Engineers et al. | British Library Conference Proceedings | 1996