21–40 von 57 Ergebnissen
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    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

    Experimental and numerical characterizations of unstable sources in a solid rocket motor

    Vetel, J. / Plourde, F. / Doan-Kim, S. et al. | AIAA | 2001

    Simulations of an aeroelastic control system for shock/boundary layer interactions

    McIlwain, S. / Kim, J. / Breitenfeld, S. et al. | AIAA | 2001

    Influence of hydrodynamic conditions on the vortex shedding phenomenon

    Vetel, J. / Plourde, F. / Doan-Kim, S. | AIAA | 2000

    Passive Control of Supersonic Rectangular Jets via Nozzle Trailing-Edge Modifications

    M. Samimy / J.-H. Kim / P. S. Clancy et al. | AIAA | 1998

    Numerical study of hydrogen jet flames in supersonic flows - Effect of shock waves

    Kim, J.-H. / Yoon, Y. / Choi, J.-Y. et al. | AIAA | 1998

    Nonlinear Flight Control Using Neural Networks

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

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

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

    Bimodal bound of system reliability for random composite structures

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

    Acoustic response of droplet flames to pressure oscillations

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

    Evaporation from an extended meniscus for nonisothermal interfacial conditions

    Hallinan, K. P. / Kim, S. J. / Chang, W. S. | AIAA | 1994

    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