Computation of ionization in re-entry flowfields
- 1 June 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (6) , 1082-1089
- https://doi.org/10.2514/3.5835
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Computation of nonequilibrium merged stagnation shock layers by successive accelerated replacementPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Ionization Rate of Air behind High-Speed Shock WavesPhysics of Fluids, 1966
- Spherically blunted cone pressure distributions.AIAA Journal, 1966
- Estimates for collision-induced dissociation ratesAIAA Journal, 1965
- Nonequilibrium laminar boundary-layer flow of ionized airAIAA Journal, 1964
- Nonequilibrium, nonsimilar solutions of the laminar boundary-layer equationsAIAA Journal, 1964
- Rate of Ionization Behind Shock Waves in Air. II. Theoretical InterpretationsPhysics of Fluids, 1963
- Blunt-Nose Inviscid Airflows With Coupled Nonequilibrium ProcessesJournal of the Aerospace Sciences, 1962
- Direct Calculation of Pressure Distribution on Blunt Hypersonic Nose Shapes With Sharp CornersJournal of the Aerospace Sciences, 1961
- A STREAMTUBE APPROXIMATION FOR CALCULATION OF REACTION RATES IN THE INVISCID FLOW FIELD OF HYPERSONIC OBJECTSPublished by Elsevier ,1961