A STREAMTUBE APPROXIMATION FOR CALCULATION OF REACTION RATES IN THE INVISCID FLOW FIELD OF HYPERSONIC OBJECTS
- 1 January 1961
- book chapter
- Published by Elsevier
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Low-Density Shock Tube for Chemical Kinetics StudiesPhysics of Fluids, 1961
- Inviscid Flow with Nonequilibrium Molecular Dissociation for Pressure Distributions Encountered in Hypersonic FlightJournal of the Aerospace Sciences, 1960
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- Theory of Radiation from Luminous Shock Waves in NitrogenPhysics of Fluids, 1959
- Hydrodynamics of a Reacting and Relaxing FluidJournal of Applied Physics, 1957
- Inviscid Hypersonic Flow Over Blunt-Nosed Slender BodiesJournal of the Aeronautical Sciences, 1957
- Note on the characteristics in unsteady one-dimensional flows with heat additionQuarterly of Applied Mathematics, 1950