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Fluid dynamics / Spacecraft propulsion / Continuum mechanics / Boundary layer / Heat transfer / Hypersonic speed / Scramjet / Aerospace engineering / Space technology / Aerodynamics
Date: 2008-03-12 01:01:58
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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