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 - 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.
UR - http://www.scopus.com/inward/record.url?scp=84980318175&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84980318175&partnerID=8YFLogxK
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 -