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.


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    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 :

    01.01.2003


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch




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    Experimental investigation of the RBCC rocket-ejector mode

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


    Focused Experimental and Analytical Studies of the RBCC Rocket-Ejector Mode

    Lehman, M. K. / Pal, S. / Schwer, D. A. et al. | British Library Conference Proceedings | 1999


    Experimental/Analytical Characterization of the RBCC Rocket-Ejector Mode

    Ruf, J. H. / Lehman, M. / Pal, S. et al. | NTRS | 2000


    Focused Rocket-Ejector RBCC Experiments

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