TY - GEN
T1 - Nonequilibrium plasma flow computation with atomic and molecular state transitions
AU - Ogino, Yousuke
AU - Totani, Kosuke
AU - Ohnishi, Naofumi
N1 - Publisher Copyright:
© 2015 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2015
Y1 - 2015
N2 - A computational code for collisional-radiative rate equations coupled with momentum and energy conservation equations has been developed to study the effects of nonequilibrium atomic and molecular processes on the population densities in an air plasma flowfield. This model consists of fifteen air species: e-, N, N+, N2+, O, O+, O2+, O-, N2, N+ 2, NO, NO+, O2, O+2, and O-2 with their major electronic excited states. Many elementary processes are considered in the number density range of 1012/cm3 ≤ N ≤ 1019/cm3 and the temperature range of 300 K ≤ T ≤ 60,000 K. The state population, the chemical com-position and temperature profiles in a high enthalpy flow condition assuming the Fire II reentry problem are computed. Presented computational results indicated that the amount of radiative intensity emitted from nitrogen atoms has a possibility to be reduced more than 10 % due to the atomic and molecular state transitions.
AB - A computational code for collisional-radiative rate equations coupled with momentum and energy conservation equations has been developed to study the effects of nonequilibrium atomic and molecular processes on the population densities in an air plasma flowfield. This model consists of fifteen air species: e-, N, N+, N2+, O, O+, O2+, O-, N2, N+ 2, NO, NO+, O2, O+2, and O-2 with their major electronic excited states. Many elementary processes are considered in the number density range of 1012/cm3 ≤ N ≤ 1019/cm3 and the temperature range of 300 K ≤ T ≤ 60,000 K. The state population, the chemical com-position and temperature profiles in a high enthalpy flow condition assuming the Fire II reentry problem are computed. Presented computational results indicated that the amount of radiative intensity emitted from nitrogen atoms has a possibility to be reduced more than 10 % due to the atomic and molecular state transitions.
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U2 - 10.2514/6.2015-0979
DO - 10.2514/6.2015-0979
M3 - Conference contribution
AN - SCOPUS:84980338918
SN - 9781624103438
T3 - 53rd AIAA Aerospace Sciences Meeting
BT - 53rd AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 53rd AIAA Aerospace Sciences Meeting, 2015
Y2 - 5 January 2015 through 9 January 2015
ER -