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Chul Park (1987)
Assessment of two-temperature kinetic model for ionizing airJournal of Thermophysics and Heat Transfer, 3
M. Furudate, Toshiyuki Suzuki, K. Sawada (2000)
Calculation of Intermediate Hypersonic Flow Using Multi-Temperature Model
S. Sharma, W. Huo, Chul Park (1988)
Rate parameters for coupled vibration-dissociation in a generalized SSH approximation. [Schwarz, Slawsky, and Herzfeld]
G. Shoev, Y. Bondar, Georgii Oblapenko, E. Kustova (2016)
Development and testing of a numerical simulation method for thermally nonequilibrium dissociating flows in ANSYS FluentThermophysics and Aeromechanics, 23
M. Benchikh, R. Haoui (2006)
Choice the vibration-dissociation coupling factor of flow in high temperature behind a plane shock wave
V. Casseau, R. Palharini, T. Scanlon, Richard Brown (2016)
A Two-Temperature Open-Source CFD Model for Hypersonic Reacting Flows, Part One: Zero-Dimensional Analysis †, 3
G. Shoev, Y. Bondar (2016)
Numerical study of non-equilibrium gas flows with shock waves by using the Navier–Stokes equations in the two-temperature approximation, 1770
R. Haoui (2010)
Physico-chemical state of the air at the stagnation point during the atmospheric reentry of a spacecraftActa Astronautica, 68
M. Panesi, T. Magin, A. Bourdon, A. Bultel, O. Chazot (2008)
Analysis of the FIRE II Flight Experiment by Means of a Collisional Radiative Model
C. Park (1985)
On convergence of computation of chemically reacting flows
G. Candler, R. Maccormack (1991)
Computation of weakly ionized hypersonic flows in thermochemical nonequilibrium, 5
M. Panesi, T. Magin, A. Bourdon, A. Bultel, O. Chazot (2009)
Fire II Flight Experiment Analysis by Means of a Collisional-Radiative ModelJournal of Thermophysics and Heat Transfer, 23
G. Candler, C. Park (1988)
The computation of radiation from nonequilibrium hypersonic flows
Chul Park, Seung-Ho Lee (1995)
Validation of Multitemperature Nozzle Flow CodeJournal of Thermophysics and Heat Transfer, 9
Tristan Soubrié (2006)
Prise en compte de l'ionisation et du rayonnement dans la modélisation des écoulements de rentrée terrestre et martienne
Chul Park, J. Howe, R. Jaffe, G. Candler (1993)
Review of Chemical-Kinetic Problems of Future NASA Missions, II: Mars EntriesJournal of Thermophysics and Heat Transfer, 8
C. Park (1989)
Nonequilibrium Hypersonic Aerothermodynamics
Y. Bondar, A. Shevyrin, Y. Chen, A. Shumakova, A. Kashkovsky, M. Ivanov (2013)
Direct Monte Carlo simulation of high-temperature chemical reactions in airThermophysics and Aeromechanics, 20
In this study, the effects of different thermo-chemical models on the macroscopic parameters of the flow behind a strong shock wave have been examined. The effect of the geometric average temperature proposed by Park and the effect of the electronic energy are also presented, and two CVD vibration-dissociation coupling models including those of Park and Kuznetsov are also examined and used for comparison. The Park93 chemical kinetic model with 11 species and 49 elementary reactions was used to describe the non-equilibrium air chemistry. The energy exchange model between translational and vibrational modes is described by the Landau-Teller formula, where the species relaxation time is based on the Millikan-White formula including Park’s high-temperature correction. The theoretical model consisting of the Euler equations supplemented with the equation of molecular vibration and the equations of chemical kinetics using a two-temperature model (translational-rotational temperature and vibrational-electron-electronic temperature) is discretized by a finite difference scheme. Good agreement is found for the relaxation zone between the present results and those obtained by Panesi for the two trajectory point (1634 s and 1643 s) for the FIRE II reentry capsule.
Thermophysics and Aeromechanics – Springer Journals
Published: Oct 1, 2019
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