1–14 of 14 hits
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    Modelling combustor performance of a ducted rocket

    Stowe, R. / De Champlain, A. / Mayer, A. | AIAA | 2000

    Thermomicromechanical model of damage for a composite structure

    Naboulsi, S. / Palazotto, A. / Mayer, A. | AIAA | 1999

    Modelling and flow visualization of mixing in a ducted rocket combustor

    Stowe, R. / DeChamplain, A. / Mayer, A. et al. | AIAA | 1998

    Thrust loss due to plume impingement effects

    MAYER, E. / HERMEL, J. / ROGERS, A. W. | AIAA | 1986

    Injection and mixing processes in high pressure LOX/GH2 rocket combustors

    Mayer, W. / Schik, A. / Schweitzer, C. et al. | AIAA | 1996

    Recent advances in H2/O2 high pressure coaxial injector performance analysis

    KRUELLE, G. / MAYER, W. / SCHLEY, C.-A. | AIAA | 1990

    Thrust loss due to plume impingement effects

    MAYER, E. / HERMEL, J. / ROGERS, A. | AIAA | 1985

    Ducted rocket combustion experiments at low gas-generator combustion temperatures

    Dijkstra, F / Mayer, A / Wilson, K et al. | AIAA | 1995

    Two phase flow combustion modelling of a ducted rocket

    Stowe, R. / Dubois, C. / Harris, P. et al. | AIAA | 2001

    Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions

    Wolfgang O. H. Mayer / Axel H. A. Schik / Bruno Vielle et al. | AIAA | 1998