Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Hypervelocity Capability of HyPulse Shock Tunnel for Radiation and Heat Transfer Measurements at Mach 30+


    Contributors:

    Conference:

    2008 U.S. Air Force T&E Days ; 2008 ; Los Angeles , California



    Publication date :

    2008-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Mach 12 & 15 Scramjet Test Capabilities of the HYPULSE Shock-Expansion Tunnel

    Hass, N. E. / Shih, A. T. / Rogers, R. C. et al. | British Library Conference Proceedings | 2005


    Hypervelocity Capability of HyPulse Shock Tunnel for Radiative Heat Transfer Measurements at Lunar Reentries

    Tsai, C. / Chue, R. / Nicholson, C. et al. | British Library Conference Proceedings | 2009


    CFD evaluation of Mach 17 HYPULSE scramjet combustor data

    BOBSKILL, GLENN / BITTNER, ROBERT / RIGGINS, DAVID et al. | AIAA | 1991


    Static pressure measurements in a hypervelocity shock tunnel.

    Bowman, G. H. / Coon, G. W. | NTRS | 1965