Numerical simulation of non-equilibrium ionized air flow around a re-entry capsule
Author:
Publisher
AIP Publishing
Link
http://aip.scitation.org/doi/pdf/10.1063/5.0051811
Reference13 articles.
1. W. L. Grantham, “Flight results of a 25,000 foot per second reentry experiment using microwave reflectometers to measure plasma electron density and standoff distance,” (1970), NASA TN D-6062.
2. Numerical study of hypersonic flows over reentry configurations with different chemical nonequilibrium models
3. Direct simulation of rarefied high-enthalpy flow around the RAM C-II capsule
4. Two-dimensional numerical analysis of flow ionization in the RAM-C-II flight experiment
5. Numerical Prediction of Hypersonic Flowfields Including Effects of Electron Translational Nonequilibrium
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