1–20 von 34 Ergebnissen
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    Acoustic response of droplet flames to pressure oscillations

    Sohn, C. H. / Chung, C. H. / Kim, J. S. et al. | AIAA | 1996

    Adaptive control of grid quality for computational fluid dynamics

    LEE, K. D. / LOELLBACH, J. M. / KIM, M. S. | AIAA | 1991

    Bimodal bound of system reliability for random composite structures

    Park, J. S. / Kim, C. G. / Hong, C. S. | AIAA | 1996

    Design, Implementation, and Validation of KOMPSAT-2 S/W Simulator

    Lee, Sanguk / Cho, S. / Kim, J. | AIAA | 2004

    Effects of gas models on hypersonic base flow calculations

    Kim, M. S. / Loelbach, J. M. / Lee, K. D. | AIAA | 1994

    Electrostatic field effects on a rotating liquid film conical radiator

    KIM, HYO / BANKOFF, S. G. / MIKSIS, MICHAEL J. | AIAA | 1993

    Flow field measurements near a fighter model at high angles of attack

    KOMERATH, N. / MCMAHON, H. / SCHWARTZ, R. et al. | AIAA | 1990

    Flow over a twin-tailed aircraft at angle of attack. I - Spatial characteristics

    KOMERATH, N. M. / LIOU, S. G. / SCHWARTZ, R. J. et al. | AIAA | 1992

    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

    Nd: YAG Laser-Based Dual-Line Rayleigh Scattering System

    M. Otugen / J. Kim / S. Popovic | AIAA | 1997

    Nonlinear Flight Control Using Neural Networks

    Byoung S. Kim / Anthony J. Calise | AIAA | 1997