A series of tests has been carried out to investigate the effects of various scale parameters on the direct connect scramjet combustor performance. The calculated combustion efficiency appears to be independent of scale for the same geometry, but tests with more precise scaling of the entire combustor are required to verify this. Combustion, however, can be strongly dependent on geometry for the same scale. It is suggested that the beneficial aspects of certain geometric or scale variations can be combined to improve the overall performance.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Effects of scale on supersonic combustor performance


    Beteiligte:

    Erscheinungsdatum :

    01.06.1987


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Effects of scale on supersonic combustor performance

    DISKIN, GLENN / NORTHAM, G. | AIAA | 1987



    Electrically Driven Supersonic Combustor

    Leonov, S. / Sabelnikov, V. / European Space Agency | British Library Conference Proceedings | 2009


    Effects of Injection Configuration on Performance of a Staged Supersonic Combustor

    Sadatake Tomioka / Kan Kobayashi / Kenji Kudo et al. | AIAA | 2003