1–20 von 40 Ergebnissen
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    Cure for shock instability - Development of an improved Roe scheme

    Kim, S.-S. / Kim, C. / Rho, O.-H. et al. | AIAA | 2002

    Analysis of steady arc near current zero

    KIM, S. / NAGAMATSU, H. | AIAA | 1989

    Design study of an advanced gas generator

    KIM, S. / TRINH, H. | AIAA | 1993

    Calculation of scramjet inlet with thick boundary-layer ingestion

    LAI, H. / KIM, S. / NAGAMATSU, H. | AIAA | 1993

    A new guidance law for homing missiles

    CHO, H. S. / BIEN, Z. / KIM, Y. S. | AIAA | 1985

    Improved Method for Rotor Wake Capturing

    Haedong Kim / Marc H. Williams / Anastasios S. Lyrintzis | AIAA | 2002

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

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

    Three-Dimensional Nonequilibrium Viscous Shock-Layer Flows over Complex Geometries

    S. Swamhathan / M.D. Kim / Clark H. Lewis | AIAA | 1984

    Experimental and numerical studies of supersonic Coanda wall jets

    Kim, H. / Raghunathan, S. / Setoguchi, T. et al. | AIAA | 2000

    Optimum design of unbraced steel frames using advanced analysis

    Chang, C. / Park, M. / Park, S. et al. | AIAA | 2000

    An experimental study of structural damage detection using incomplete measurements

    Zimmerman, D. / Smith, S. / Kim, H. et al. | AIAA | 1994

    Leading-Edge Shape and Aeroengine Fan Blade Performance

    A. I. Sayma / M. Kim / N. H. S. Smith | AIAA | 2003

    Nonequilibrium viscous shock-layer flows over blunt sphere-cones at angle of attack

    LEWIS, C. H. / SWAMINATHAN, S. / KIM, M. D. | AIAA | 1983