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Fluid dynamics / Spacecraft propulsion / Continuum mechanics / Boundary layer / Heat transfer / Hypersonic speed / Scramjet / Aerospace engineering / Space technology / Aerodynamics


Brief Communication Effect of Confinement in High-Speed Reacting Mixing Layer DEBASIS CHAKRABORTY,*† H. S. MUKUNDA, and P. J. PAUL Department of Aerospace Engineering, Indian Institute of Science, Bangalore[removed], In
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Document Date: 2008-03-12 01:01:58


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File Size: 177,74 KB

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City

Washington / D.C. / Sandham / Pittsburgh / Clemens / /

Company

Arnett S. A. / Kubota / Elsevier Science Inc. / Ragab S. A. / /

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Facility

Indian Institute of Science / The Combustion Institute / /

IndustryTerm

finite rate chemical kinetics / /

NaturalFeature

Pa stream / /

Organization

MUKUNDA / High-Speed Reacting Mixing Layer DEBASIS CHAKRABORTY / *† H. S. MUKUNDA / and P. J. PAUL Department of Aerospace Engineering / Combustion Institute / Indian Institute of Science / Bangalore / /

Person

V. Adimurthy / /

Position

classical Kelvin-Helmholtz *Corresponding author / Scientist /Engineer / Aerodynamics Division / Carpenter / /

ProvinceOrState

North Dakota / Northern Territory / /

Technology

simulation / DNS / /

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