TY - GEN
T1 - State-to-state and direct molecular simulation study of energy transfer and dissociation of nitrogen mixtures
AU - Macdonald, Robyn L.
AU - Torres, Erik
AU - Schwartzentruber, Thomas E.
AU - Panesi, Marco
N1 - Funding Information:
The authors would like to thank Dr. David Schwenke and Dr. Richard Jaffe from NASA Ames Research Center for access to the PES and kinetic database as well as their helpful discussions. Dr. R. Macdonald was supported by the University of Minnesota President’s Postdoctoral Fellowship Program. Dr. E. Torres and Dr. T. Schwartzentruber were supported by the Air Force Office of Scientific Research (AFOSR) under Grant Nos. FA9550-16-1-0161 and FA9550-17-1-0250. Dr. M. Panesi was supported by the AFOSR under Grant No. FA9550-18-1-0388. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the AFOSR or the US government.
Funding Information:
The authors would like to thank Dr. David Schwenke and Dr. Richard Jaffe from NASA Ames Research Center for access to the PES and kinetic database as well as their helpful discussions. Dr. R. Macdonald was supported by the University of Minnesota President?s Postdoctoral Fellowship Program. Dr. E. Torres and Dr. T. Schwartzentruber were supported by the Air Force Office of Scientific Research (AFOSR) under Grant Nos. FA9550-16-1-0161 and FA9550-17-1-0250. Dr. M. Panesi was supported by the AFOSR under Grant No. FA9550-18-1-0388. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the AFOSR or the US government.
Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - This work presents a comparison of the non-equilibrium dissociation and energy transfer processes predicted using the state-to-state (StS) and direct molecular simulation (DMS) methods. The StS method is a deterministic method, which relies on pre-computed kinetic data used in the master equation for each rovibrational energy state. The DMS method is a stochastic interpretation of molecular dynamics, directly tracking the changes in energy of particles due to collisions. Using both methods we study a simple zero-dimensional heat bath in which initially cold nitrogen molecules are instantaneously heated to between 5 000 K and 20 000 K. To isolate the effect of the N2-N collision processes, we ignore any reactions due to collisions between two molecules. We find that both methods are in excellent agreement in the temperature range studied, with both macroscopic (composition and average internal energies) and microscopic (distribution of internal energy states) properties matching throughout the energy transfer and dissociation processes.
AB - This work presents a comparison of the non-equilibrium dissociation and energy transfer processes predicted using the state-to-state (StS) and direct molecular simulation (DMS) methods. The StS method is a deterministic method, which relies on pre-computed kinetic data used in the master equation for each rovibrational energy state. The DMS method is a stochastic interpretation of molecular dynamics, directly tracking the changes in energy of particles due to collisions. Using both methods we study a simple zero-dimensional heat bath in which initially cold nitrogen molecules are instantaneously heated to between 5 000 K and 20 000 K. To isolate the effect of the N2-N collision processes, we ignore any reactions due to collisions between two molecules. We find that both methods are in excellent agreement in the temperature range studied, with both macroscopic (composition and average internal energies) and microscopic (distribution of internal energy states) properties matching throughout the energy transfer and dissociation processes.
UR - http://www.scopus.com/inward/record.url?scp=85092358825&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85092358825&partnerID=8YFLogxK
U2 - 10.2514/6.2020-1712
DO - 10.2514/6.2020-1712
M3 - Conference contribution
AN - SCOPUS:85092358825
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -