1–20 of 25 hits
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    A new method for designing shock-free transonic configurations

    SOBIECZKY, H. / YU, N. / FUNG, K.-Y. et al. | AIAA | 1978

    An implicit shock-fitting scheme for unsteady transonic flow computations

    YU, N. / SEEBASS, A. / BALLHAUS, W. | AIAA | 1977

    Application of boundary layer control to HSCT low speed configuration

    PARIKH, P. / CHEN, A. / YU, N. et al. | AIAA | 1990

    Flow prediction for propfan configurations using Euler equations

    YU, N. / SAMANT, S. / RUBBERT, P. | AIAA | 1984

    Flow simulations for a complex airplane configuration using Euler equations

    YU, N. / KUSUNOSE, K. / CHEN, H. et al. | AIAA | 1987

    Flow simulations for general nacelle configurations using Euler equations

    CHEN, H. / YU, N. / RUBBERT, P. et al. | AIAA | 1983

    GMRES acceleration of computational fluid dynamics codes

    WIGTON, L. / YU, N. / YOUNG, D. | AIAA | 1985

    Grid generation and flow analyses for wing/body/winglet configurations

    YU, N. / CHEN, HAI-CHOW / CHEN, ALLEN et al. | AIAA | 1988

    Heat Transfer in the Heating Zone of Low-Temperature Heat Pipes

    V. I. Tolubinsky / V. A. Antonenko / Yu. N. Ostrovsky et al. | AIAA | 1979

    Inviscid drag calculations for transonic flows

    YU, N. / CHEN, H. / SAMANT, S. | AIAA | 1983

    Navier-Stokes calculations for massively separated flows

    Wilkinson, W. / Lines, T. / Yu, N. | AIAA | 1996