101–120 von 126 Ergebnissen
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    Structure of gaseous detonations in a convergent-divergent channel

    KNYSTAUTAS, R. / LEE, B. H. K. / LEE, J. H. | AIAA | 1965

    Missile aerodynamic parameter and structure identification from flight test data

    KAIN, J. / BROWN, JR., C. / LEE, J. et al. | AIAA | 1978

    National Oxidizer-Rich Materials Synergy Team

    Lee, J / Gluszek, F / Eckel, A et al. | AIAA | 1995

    CARS temperature measurements in an MHD diffuser

    SINGH, J. / YUEH, F. / COOK, ROBERT et al. | AIAA | 1991

    Multi-point nose shape optimization of space launcher using response surface method

    Min, B.-Y. / Lee, J.-W. / Byun, Y.-H. et al. | AIAA | 2002

    Modeling and Simulation of Spacecraft Power Systems

    Lee, J. R. / Cho, B. H. / Kim, S. J. et al. | AIAA | 1987

    Testing of the RL10B-2 carbon-carbon nozzle extension

    Ellis, R. / Lee, J. / Payne, F. et al. | AIAA | 1998

    Supersonic wind tunnel tests of panel noise transmission

    Simpson, M. / Mathur, G. / Tran, B. et al. | AIAA | 1999

    Oklahoma weather phenomena that may affect aviation

    ZRNIC, D. S. / DOVIAK, R. J. / LEE, J. T. et al. | AIAA | 1987

    Computational and experimental study of aerodynamics and heat release in a liquid fueled combustor

    Brankovic, A. / Ryder, Jr., R. / Sturgess, G. et al. | AIAA | 2001

    Normal Shock/Boundary-Layer Interaction Control Using Aeroelastic Mesoflaps

    Everett S. Hafenrichter / Yeol Lee / J. Craig Dutton et al. | AIAA | 2003

    Dynamic Modeling of a Smart Materials Robot

    S. S. Ge / T. H. Lee / J. Q. Gong | AIAA | 1998