Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:
    Sakaue, S. (author) / Arai, T. (author) / Morisaki, T. (author) / Sunami, T. (author) / Itoh, K. (author)

    Conference:

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



    Publication date :

    2006-01-01


    Size :

    6 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    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