Nonequilibrium, ionized, hypersonic flow over a blunt body at low Reynolds number
- 1 July 1970
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (7) , 1263-1270
- https://doi.org/10.2514/3.5883
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
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- Computation of nonequilibrium merged stagnation shock layers by successive accelerated replacementPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Merged stagnation shock layer of nonequilibrium dissociating gas.AIAA Journal, 1968
- Integral method for the stagnation region of a hypersonic viscous shock layer with blowing.AIAA Journal, 1968
- Prediction of the electron number density distribution in the laminar air boundary layer on sharp and blunt bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- APPROXIMATE METHOD FOR HYPERSONIC NONEQUILIBRIUM BLUNT BODY AIRFLOWSAIAA Journal, 1963
- CHEMICAL KINETICS OF HIGH TEMPERATURE AIRPublished by Elsevier ,1962
- Viscous Aerodynamic Characteristics in Hypersonic Rarefied Gas FlowJournal of the Aerospace Sciences, 1960
- Laminar Heat Transfer Around Blunt Bodies in Dissociated AirJournal of the Aerospace Sciences, 1959