1. 1Linwood-Jones, W. and Cross, A. E. “Electrostatic Probe Measurements of Plasma Parameters for Two Reentry Flight Experiments at 25000 Feet Per Second,” Tech. Rep. NASA Technical Note D-6617, Langley Research Center, 1972.
2. 2Grantham, W. L. “Flight Results of a 25000 foot per second Reentry Experiment Using Microwave Reflectometers to Measure Plasma Density and Standoff Distance,” Tech. Rep. NASA Technical Note D-6062, Langley Research Center, 1970.
3. Computation of weakly ionized hypersonic flows in thermochemical nonequilibrium
4. Governing Equations for Weakly Ionized Plasma Flowfields of Aerospace Vehicles
5. Numerical Simulation of Weakly Ionized Hypersonic Flow for Reentry Configurations