1. Candler. Graham V. "TheComputation of FVrakly Ionized Hypersonic Flow in Thermo-Chemical Sionequliibrium," Ph.D Thesis,Stanford University, Jiine11188. Olynick. David R. and Hassan, H. A. "A New Twu Temperature Dissociation Model for Reactina Flows," AIAA Paper 92-2943, 1992. Gnoffo, Peter A, Gupta, Roop N., and Shinn, Judy L. `Conservation Equations and Physical Models ior Hypersonic Air Flows in Thermd and Chemical Nonequilibrium," NASA TP-2867, Feb. 1989. Lee, J. A, "Electron-Impact Vibrational Excitation Rates in the Flowfietd of Aeroassisted Orbital Transfer Vehicles," Progress in Astronautics and .Aeronautics: ThermophysicalAspects of ReentryFlowr, Val. 103, edited by J. N. Moss and C. C.Scott, AIAA,Icw York, 1980,pp. 197-224 Candler, Graham V., and MacCormack. Robert W. "The Computation of Hypersonic Ionized Flows in Chemical and Thermal Nonequilibrium." AIAA Paper 88-0511, 1988.
2. per 92-2877, Nashde, Tennessee. July 1992. [151 Steger, J., and Warming, R. F. "Flux-Vector Splitting
3. to Finite DifferenceMethods," NASA TM 78605, 1979. [IF] Yoon. Seokkwan, and Jameson, Antony, ".An LU-SSOR