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Heat transfer / Chemistry / Spacecraft propulsion / Chemical engineering / Aerodynamics / Scramjet / Boundary layer / Turbulence / Reaction rate / Aerospace engineering / Physics / Fluid dynamics


A thermo-chemical exploration of a two-dimensional reacting supersonic mixing layer Debasis Chakraborty,a) H. V. Nagaraj Upadhyaya, P. J. Paul, and H. S. Mukunda Department of Aerospace Engineering, Indian Institute of S
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Document Date: 2010-10-08 02:26:15


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New York / /

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Kubota / Academic Press / High Speed Flight Propulsion Systems / /

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J. L. Hall / Indian Institute of Science / American Institute of Physics / The Combustion Institute / /

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chemical reaction time / thermo-chemical exploration / large stream kinetic energy / grid-independent solutions / higher order numerical algorithms / chemical processes / http /

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/air stream / /

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American Institute of Physics / US Federal Reserve / Indian Institute of Science / Bangalore / P. J. Paul / and H. S. Mukunda Department of Aerospace Engineering / National Aeronautics and Space Administration / Combustion Institute / NASA TP / /

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G. Northam / M. Zhuang / R. Pitz / O. Jarret / Jr. / V. Adimurthy / J. Wehrmeyer / M. M. Koochesfahani / /

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2E/RT / Carpenter / /

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New York / /

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laser / heat transfer / SIMULATION / higher order numerical algorithms / pdf / /

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http /

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