1–18 von 18 Ergebnissen
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    Inviscid drag calculations for transonic flows

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

    Fortified LEWICE with viscous effects

    CEBECI, TUNCER / CHEN, H. / ALEMDAROGLU, N. | AIAA | 1990

    Calculation of low Reynolds number flows at high angles of attack

    CEBECI, T. / CHEN, H. / LIEBECK, R. | AIAA | 1990

    MODAL SYNTHESIS METHOD BY ARMA MODEL

    CHEN, H. / YEE, ERIC / TSUEI, Y. | AIAA | 1993

    Flow simulations for general nacelle configurations using Euler equations

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

    Flow simulations for a complex airplane configuration using Euler equations

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

    An approach to the design of wings - The role of mathematics, physics and economics

    CEBECI, T. / KHATTAB, A. / CHEN, H. et al. | AIAA | 1992

    Transonic analysis for complex airplane configurations

    KUSUNOSE, K. / MARCUM, D. / CHEN, H. et al. | AIAA | 1987

    Analysis of iced wings

    CEBECI, TUNCER / CHEN, H. / KAUPS, K. et al. | AIAA | 1992

    Common lunar lander

    BAILEY, S. / STECKLEIN, J. / CHEN, H. et al. | AIAA | 1992