Rovibrationally state-specific collision model for the O2(Σg−3) + O(P3) system in DSMC
Author:
Affiliation:
1. Center for Hypersonics and Entry Systems Studies, University of Illinois at Urbana-Champaign, Urbana, Illinois 61801, USA
Funder
Air Force Office of Scientific Research
National Aeronautics and Space Administration
Publisher
AIP Publishing
Subject
Physical and Theoretical Chemistry,General Physics and Astronomy
Link
https://aip.scitation.org/doi/am-pdf/10.1063/5.0027411
Reference32 articles.
1. Construction of a coarse-grain quasi-classical trajectory method. I. Theory and application to N2–N2 system
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3. Modeling of molecular nitrogen collisions and dissociation processes for direct simulation Monte Carlo
4. Generalized Treanor–Marrone model for state-specific dissociation rate coefficients
5. Rovibrational internal energy transfer and dissociation of N2(1Σg+)−N(4Su) system in hypersonic flows
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1. State-to-state study of non-equilibrium recombination of oxygen and nitrogen molecules;The Journal of Chemical Physics;2024-04-03
2. Effects of the third body (O and N) on the recombination of molecular nitrogen using quasi-classical trajectory methods;Chemical Physics;2024-01
3. Diabatic potential energy surfaces and semiclassical multi-state dynamics for fourteen coupled 3 A′ states of O3;Electronic Structure;2022-11-21
4. Rate constants and molecular recombination pathways of oxygen from quasi-classical trajectory simulations of the O3 system;Chemical Physics;2022-01
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