TY - GEN
T1 - State-to-state modeling of CO for mars entry applications
AU - Macdonald, Robyn
AU - Munafò, Alessandro
AU - Johnston, Christopher O.
AU - Panesi, Marco
N1 - Funding Information:
Research of R. M. and M. P. is supported by NASA Grant No. NNX14AB67A. The authors have benefited rom numerous discussions with Dr. R.L. Jaffe, Dr. D.W. Schwenke and Y. Liu at NASA Ames Research.
Publisher Copyright:
© 2015 by Robyn Macdonald. Published by the American Institute of Aeronautics and Astronautics, Inc.
PY - 2015
Y1 - 2015
N2 - This work addresses the study of the dynamics of the excited states of CO in shock heated Mars’s atmosphere. The model accounts for thermal non-equilibrium between the translational energy mode of the gas and the vibrational energy mode of individual molecules. Furthermore, electronic states of molecules are treated as separate species, allowing for non-Boltzmann distributions of their populations. Two approaches have been considered and compared: i) state-to-state and ii) quasi-steady state. Both strategies are applied to the modeling of the flow behind a normal shock wave, for Mars entry conditions. The results indicate that the use of a quasi-steady state approach can lead to a substantial dissociation of the excited CO molecules, thus leading to a drastic underestimation of the radiation heat flux.
AB - This work addresses the study of the dynamics of the excited states of CO in shock heated Mars’s atmosphere. The model accounts for thermal non-equilibrium between the translational energy mode of the gas and the vibrational energy mode of individual molecules. Furthermore, electronic states of molecules are treated as separate species, allowing for non-Boltzmann distributions of their populations. Two approaches have been considered and compared: i) state-to-state and ii) quasi-steady state. Both strategies are applied to the modeling of the flow behind a normal shock wave, for Mars entry conditions. The results indicate that the use of a quasi-steady state approach can lead to a substantial dissociation of the excited CO molecules, thus leading to a drastic underestimation of the radiation heat flux.
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U2 - 10.2514/6.2015-0476
DO - 10.2514/6.2015-0476
M3 - Conference contribution
AN - SCOPUS:84980318175
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 -