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Aerospace engineering / Dynamics / Mach number / Shock wave / Drag / Boundary layer / Speed of sound / Particle image velocimetry / Navier–Stokes equations / Aerodynamics / Fluid dynamics / Fluid mechanics


AIAA JOURNAL Vol. 48, No. 6, June 2010 Compressible Large-Eddy Simulation of Separation Control on a Wall-Mounted Hump Jennifer A. Franck∗ and Tim Colonius†
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Document Date: 2013-01-23 17:28:37


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Danvers / Pasadena / Springer / New York / /

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Viken S. A. / Honein A. E. / PIV / Clearance Center Inc. / S&P / Vatsa / Washburn A. E. / Reno NV / V. N. / LES / Suzuki / W. L. / Cabot / Aeronautics and Astronautics Inc. / /

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Brown University / Tim Colonius† California Institute of Technology / NASA Langley Research Center / /

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stable solutions / oil-film / energy buildup / internal energy / predictive tool / predictive tools / /

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California Institute of Technology / Copyright Clearance Center / American Institute of Aeronautics and Astronautics / National Science Foundation / Brown University / Cambridge Univ. / Division of Engineering / National Aeronautics and Space Administration / Division of Engineering and Applied Sciences / NASA Langley Research Center / U.S. Securities and Exchange Commission / Department of Defense High Performance Computing Centers / /

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Morgan / Reynolds Numbers / Tim Colonius / Jennifer A. Franck / /

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California / New York / Massachusetts / /

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Baseline / Journal of Computational Physics / Journal of Fluid Mechanics / /

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DNS / Fluid Dynamics / Simulation / /

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