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    Titel :

    Influence of Turbulence Modelling on Combustor Flowfield in Scramjet Mode of RBCC Engine


    Beteiligte:
    Salloum, Joseph (Autor:in) / Candon, Michael (Autor:in) / Ogawa, Hideaki (Autor:in) / Kodera, Masatoshi (Autor:in)

    Kongress:

    23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference



    Erscheinungsdatum :

    2020-01-01



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    INFLUENCE OF TURBULENCE MODELLING ON COMBUSTOR FLOWFIELD IN SCRAMJET MODE OF RBCC ENGINE

    Salloum, Joseph / Candon, Michael / Ogawa, Hideaki et al. | TIBKAT | 2020


    Dual-mode flowfield in scramjet combustor

    Abdel-Salam, T. / Tiwari, S. / Mohieldin, T. | AIAA | 2001


    Numerical investigation of an RBCC combustor during Ramjet/Scramjet mode transition

    Salloum, Joseph / Candon, Michael J. / Ridings, Andrew et al. | AIAA | 2018


    Study of dual-mode flowfield in scramjet combustor

    Tiwari, S. / Abdel-Salam, T. / Chaturvedi, S. et al. | AIAA | 2001


    STUDY OF DUAL-MODE FLOWFIELD IN SCRAMJET COMBUSTOR

    Tiwari, S. N. / Abdel-Salam, T. M. / Chaturvedi, S. K. et al. | British Library Conference Proceedings | 2001