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    Titel :

    Evaluate of Boundary Layer Introduced Streamwise Vortices in Scramjet Combustor Using Quantitative Schlieren Method


    Beteiligte:
    Sakaue, S. (Autor:in) / Arai, T. (Autor:in) / Morisaki, T. (Autor:in) / Sunami, T. (Autor:in) / Itoh, K. (Autor:in)

    Kongress:

    25th, International symposium on space technology and science ; 2006 ; Kanazawa, Japan



    Erscheinungsdatum :

    01.01.2006


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Supersonic Streamwise Vortices Breakdown in Scramjet Combustor

    Arai, Takakage / Sakaue, Shoji / Morisaki, Tetsuro et al. | AIAA | 2006


    Scramjet combustor wall boundary layer analysis

    SCHETZ, J. / BILLIG, F. / FAVIN, S. | AIAA | 1981


    Streamwise Vortices Introduced by `Hyper-Mixer' on Supersonic Mixing

    Arai, T. / Sakaue, S. / Hayase, H. et al. | British Library Conference Proceedings | 2011


    Streamwise Vortices Introduced by 'Hyper-Mixer' on Supersonic Mixing

    Arai, Takakage / Sakaue, Shoji / Hayase, Hiroki et al. | AIAA | 2011


    STREAMWISE PORTHOLE FUEL INJECTION FOR BOUNDARY-LAYER COMBUSTION INSIDE A SCRAMJET ENGINE

    Barth, J.E. / Wheatley, V. / International Council of the Aeronautical Sciences; Optimage Ltd | British Library Conference Proceedings | 2012