Electron thermochemical nonequilibrium effects in re-entry boundary layers
Author:
Affiliation:
1. General Electric Company, Philadelphia, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6150
Reference19 articles.
1. Effects of Ionization on Stagnation-Point Heat Transfer in Air and in Nitrogen
2. A general theory of weakly ionized gas flows including compressibility and electron energy effects
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1. Modeling of the plasma sintering process at reduced pressures;Plasma Chemistry and Plasma Processing;1990-06
2. Laminar Stagnation-Point Heat Transfer for a Two-Temperature Argon Plasma;AIAA Journal;1984-08
3. Electrostatic probes for dense flowing plasma;Physics of Fluids;1984
4. Numerical investigation of supersonic non-equilibrium carbon dioxide flow past blunt bodies;International Journal of Heat and Mass Transfer;1981-04
5. Nonequilibrium ionization accompanying hypersonic flow of carbon dioxide gas over blunt bodies;Fluid Dynamics;1981-01
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