1–20 von 23 Ergebnissen
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    Viscous shock-layer analysis of hypersonic flows over long slender bodies

    GUPTA, R. / LEE, K. / MOSS, J. et al. | AIAA | 1987

    Three-dimensional Navier-Stokes calculations using solution-adapted grids

    HENDERSON, T. / HUANG, W. / LEE, K. et al. | AIAA | 1993

    THE USE OF ANTIOPTIMIZATION TO COMPARE ALTERNATIVE STRUCTURAL MODELS

    GANGADHARAN, S. / NIKOLAIDIS, E. / LEE, K. et al. | AIAA | 1993

    System identification of flexible structures

    LEE, K. / HOSSIAN, S. / VENKAYYA, V. | AIAA | 1988

    Multi-point design of transonic airfoils using optimization

    HAGER, J. / EYI, S. / LEE, K. | AIAA | 1992

    Effects of gas models on hypersonic base flow calculations

    KIM, M. / LOELLBACH, J. / LEE, K. | AIAA | 1992

    A viscous-shock-layer analysis of the Martian aerothermal environment

    GUPTA, R. / MOSS, J. / SUTTON, K. et al. | AIAA | 1991

    An improvement of convection fidelity in Euler calculations

    LEE, K. / CHU, S. / ERICKSON, L. | AIAA | 1989

    An improved matching method for transonic computations

    LEE, K. / DICKSON, L. / RUBBERT, P. et al. | AIAA | 1978

    A multi-point optimization for transonic airfoil design

    HAGER, J. / EYI, S. / LEE, K. | AIAA | 1992

    A mapping technique for solution-adaptive grid control

    LEE, K. / LOELLBACH, J. | AIAA | 1989

    Airfoil design using the Navier-Stokes equations

    EYI, S. / HAGER, J. / LEE, K. | AIAA | 1993