1–20 von 27 Ergebnissen
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    Deciding Optimal Number of Fatigue Crack Growth Tests for Damage-Tolerant Design

    Bhachu, K. S. / Haftka, R. T. / Kim, N. H. | AIAA | 2016

    A new guidance law for homing missiles

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

    Processing and Characterization of Space-Durable High-Performance Polymeric Nanocomposite

    Iqbal, H. M. S. / Bhowmik, S. / Benedictus, R. et al. | AIAA | 2011

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

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

    Prioritizing Possible Force Models Error in Multiphase Flow Using Global Sensitivity Analysis

    Nili, Samaun / Park, Chanyoung / Kim, Nam H. et al. | AIAA | 2021

    Improved Method for Rotor Wake Capturing

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

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

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

    Leading-Edge Shape and Aeroengine Fan Blade Performance

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

    Proposed Boundary Conditions for Gust-Airfoil Interaction Noise

    Kim, Jae Wook / Lau, Alex S. H. / Sandham, Neil D. | AIAA | 2010

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

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

    Acoustic response of droplet flames to pressure oscillations

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