Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Use of an expansion tube to examine scramjet combustion at hypersonic velocities


    Contributors:
    RIZKALLA, O. (author) / BAKOS, R. (author) / PULSONETTI, M. (author) / CHINITZ, WALLACE (author) / ERDOS, JOHN (author)

    Conference:

    25th Joint Propulsion Conference ; 1989 ; Monterey , CA , U.S.A.



    Publication date :

    1989-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Rocketdyne Hypersonic Flow Laboratory as High-Performance Expansion Tube for Scramjet Testing

    Benjamin S. Stewart / Richard G. Morgan / Peter A. Jacobs | AIAA | 2003



    HYPERSONIC VEHICLE USING SCRAMJET

    ALHUSSAN KHALED ABDULLAH | European Patent Office | 2019

    Free access


    Simulation of hypersonic scramjet exhaust

    Oman, R. A. / Foreman, K. M. / Leng, J. et al. | NTRS | 1975