1–5 of 5 hits
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    An integrated aeroramp injector/plasma-igniter for hydrocarbon fuels in a supersonic flow. I - Experimental studies of the geometric configuration

    Jacobsen, L. / Gallimore, S. / Schetz, J. et al. | AIAA | 2001
    Publisher: The American Institute of Aeronautics and Astronautics

    An integrated aeroramp-injector/plasma-igniter for hydrocarbon fuels in supersonic flow. II - Experimental studies of the operating conditions

    Gallimore, S. / Jacobsen, L. / O'Brien, W. et al. | AIAA | 2001
    Publisher: The American Institute of Aeronautics and Astronautics

    Angled Injection through Diamond-Shaped Orifices into a Supersonic Stream

    Tomioka, S. / Jacobsen, L. / Schetz, J. et al. | British Library Conference Proceedings | 2001
    Keywords: space planes , hypersonic systems , hypersonic technologies

    An Integrated Aeroramp-Injector/Plasma-Igniter for Hydrocarbon Fuels in Supersonic Flow - Part B: Experimental Studies of the Operating Conditions

    Gallimore, S. / Jacobsen, L. / O Brien, W. et al. | British Library Conference Proceedings | 2001
    Keywords: space planes , hypersonic systems , hypersonic technologies

    An Integrated Aeroramp-Injector/Plasma Igniter for Hydrocarbon Fuels in Supersonic Flow - Part A: Experimental Studies of the Geometric Configuration

    Jacobsen, L. / Gallimore, S. / Schetz, J. et al. | British Library Conference Proceedings | 2001
    Keywords: space planes , hypersonic systems , hypersonic technologies