Vibrational state-specific model for dissociation and recombination of the O2( 3Σg−)+O( 3P) system in DSMC
Author:
Affiliation:
1. Department of Mechanical Science and Engineering, University of Illinois at Urbana-Champaign, Urbana, Illinois 61801-2946, USA
Funder
National Aeronautics and Space Administration
Publisher
AIP Publishing
Subject
Physical and Theoretical Chemistry,General Physics and Astronomy
Link
http://aip.scitation.org/doi/pdf/10.1063/1.5035283
Reference48 articles.
1. Consistent post-reaction vibrational energy redistribution in DSMC simulations using TCE model
2. Nonequilibrium shock-heated nitrogen flows using a rovibrational state-to-state method
3. QCT-based vibrational collisional models applied to nonequilibrium nozzle flows
4. Consistent multi-internal-temperatures models for nonequilibrium nozzle flows
5. Dissociation–recombination models in hypersonic boundary layer O2/O flows
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