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    Titel :

    Effect of outflow vortex of 3D Inlet on fuel injection and mixing in a scramjet combustor


    Beteiligte:
    Zhou, Xunhuang (Autor:in) / Teng, Jian (Autor:in) / Li, Yi-qing (Autor:in) / You, Yancheng (Autor:in)

    Kongress:

    21st AIAA International Space Planes and Hypersonics Technologies Conference



    Erscheinungsdatum :

    2017-01-01



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Effect of Outflow Vortex of 3D Inlet on Fuel Injection and Mixing in a Scramjet Combustor (AIAA 2017-2327)

    Zhou, Xunhuang / Teng, Jian / Li, Yi-qing et al. | British Library Conference Proceedings | 2017


    Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl.

    Flesberg, Sonja M. / Taghavi, Ray / Farokhi, Saeed | AIAA | 2018


    Mixing augmentation of transverse injection in SCRamjet combustor

    Lee, Sang-Hyeon / Kim, Young-Jin / Mitani, Tohru | AIAA | 2000



    Characterization of Scramjet Combustor with Transverse Fuel Injection

    Young, Gregory / Balar, Rama / Gupta, Ashwani et al. | AIAA | 2006