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    Titel :

    Scramjet Thrust Performance Improved by Boundary Layer Control


    Beteiligte:

    Kongress:

    24th, 24th ISTS: the international symposium on space technology and science[s] ; 2004 ; Miyazaki, Japan



    Erscheinungsdatum :

    2004-01-01


    Format / Umfang :

    6 pages


    Anmerkungen:

    Held on CD-ROM. Selected papers in print form. Title from screen.



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Effect of Ingested Boundary Layer on Scramjet Engines' Thrust and Combustion Characteristics

    Hiraiwa, Tetsuo / Kanda, Takeshi / Kodera, Masatoshi et al. | AIAA | 2003


    Scramjet combustor wall boundary layer analysis

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


    Scramjet thrust measurement in a shock tunnel

    Paull, A. / Stalker, R. J. / Mee, D. J. | NTRS | 1995


    Scramjet thrust measurement in a shock tunnel

    Paull, A. / Stalker, R. J. / Mee, D. J. | NTRS | 1995


    Measurement of scramjet thrust in shock tunnels

    Stalker, R. / Simmons, J. / Paull, A. et al. | AIAA | 1994