A wind tunnel investigation was conducted to study the flow field in which separation is caused by an expanding plume, with emphasis on effects associated with periodic unsteadiness in the plume. The separation shock was photographed with high speed motion pictures, from which mean shock position and excursion data are reported. Pressure fluctuations were measured beneath the separation shock and statistics of the results are reported. A response of the separation shock to plume periodic unsteadiness was identified, and the magnitude of a corresponding transfer function was defined and is reported.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Effects of periodic unsteadiness of a rocket engine plume on the plume-induced separation shock wave


    Beteiligte:
    Doughty, J. O. (Autor:in)


    Erscheinungsdatum :

    01.01.1976


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Rocket Plume Modeling

    Cai, Chunpei | AIAA | 2015


    Rocket Plume Modeling

    Cai, Chunpei | AIAA | 2014


    Hydrocarbon Rocket Engine Plume Imaging with Laser Induced Incandescence

    Eseller, K. / Yueh, F. / Singh, J. et al. | British Library Conference Proceedings | 2007


    Hydrocarbon Rocket Engine Plume Imaging with Laser Induced Incandescence

    Eseller, Kemal / Yueh, Fang-Yu / Singh, Jagdish et al. | AIAA | 2007