Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Steady State Characteristics of Scramjet Engines Using Hydrogen for High Mach Numbers


    Contributors:
    Ji, Zifei (author) / Wang, Bing (author) / Zhang, Huiqiang (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




    Steady State Characteristics of Scramjet Engines Using Hydrogen for High Mach Numbers (AIAA 2017-2294)

    Ji, Zifei / Wang, Bing / Zhang, Huiqiang | British Library Conference Proceedings | 2017


    Hydrocarbon and Hydrogen-Fueled Scramjet Cavity Flameholder Performance at High Flight Mach Numbers

    Boyce, Russell / Houwing, Frank / Neely, Andrew et al. | AIAA | 2003



    Boundary-Layer Control in Mach 4 and Mach 6 Scramjet Engines

    Tohru Mitani / Noboru Sakuranaka / Sadatake Tomioka et al. | AIAA | 2005


    A comparative study of scramjet injection strategies for high Mach numbers flows

    Riggins, D. W. / Mcclinton, C. R. / Rogers, R. C. et al. | NTRS | 1992