Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

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


    Contributors:
    Zhou, Xunhuang (author) / Teng, Jian (author) / Li, Yi-qing (author) / You, Yancheng (author)

    Conference:

    21st AIAA International Space Planes and Hypersonics Technologies Conference



    Publication date :

    2017-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    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