MEGLI T W, KRIER H, BURTON R L. Plasmadynamics model for nonequilibrium processes in N2/H2 arcjets[J]. Journal of Thermophysics and Heat Transfer, 1996,10(4): 554-562.
[2]
GALLY T A, CARLSON L A, GREEN D. Flowfields coupled excitation and radiation model for nonequilibrium reacting flows[J]. Journal of Thermophysics and Heat Transfer, 1993, 7(2): 285-293.
[3]
GUPTA R N, YOS J M, THOMPSON R A. A review of reaction rates and thermodynamic and transport properties for the 11-species air model for chemical and thermal nonequilibrium calculations to 30 000 K[R]//NASA-TM-101528. Washington DC: NASA, 1989.
[4]
MEGLI T W, KRIER H, BURTON R L. Two-temperature plasma modeling of nitrogen/hydrogen arcjets[J]. Journal of Propulsion and Power, 1996, 12(6): 1062-1069.
[5]
SANTOVINCENZO A, DEININGER W D, LORENZO G D. Numerical simulation of a low power arcjet thruster[C] // IEPC-97-011. Cleveland, Ohio: Electric Rocket Propulsion Society, 1997.
[6]
ROBERTSON D, MARTINEZ-SANCHEZ M. Two dimensional numerical simulations of a cesium seeded hydrogen arcjet [R]//AIAA-98-4036. Cambridge, MA: MIT, 1998.
[7]
CARLSON L A, GALLY T A. Effect of electron temperature and impact ionization on martian return AOTV flowfields[J] . Journal of Thermophysics and Heat Transfer, 1991, 5(1): 9-19.
[8]
CARLSON L A, GALLY T A. Nonequilibrium chemical and radiation coupling, PartⅠ: theory and models[J]. Journal of Thermophysics and Heat Transfer, 1992,6(3): 385-391.
