Результаты исследований: Научные публикации в периодических изданиях › статья в журнале по материалам конференции › Рецензирование
Chemical kinetics in a five-component air behind shock waves. / Karpenko, A. G.; Tolstoguzov, S. S.; Volkov, K. N.
в: Journal of Physics: Conference Series, Том 2154, № 1, 012008, 19.01.2022.Результаты исследований: Научные публикации в периодических изданиях › статья в журнале по материалам конференции › Рецензирование
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TY - JOUR
T1 - Chemical kinetics in a five-component air behind shock waves
AU - Karpenko, A. G.
AU - Tolstoguzov, S. S.
AU - Volkov, K. N.
N1 - Publisher Copyright: © 2022 Institute of Physics Publishing. All rights reserved.
PY - 2022/1/19
Y1 - 2022/1/19
N2 - The influence of non-equilibrium kinetic processes on macroscopic parameters in air flows is a challenging and an important problem. Particularly, simulation of flows with high-temperature effects is important near the surface of spacecraft or meteorites when they enter the Earth's atmosphere. Non-equilibrium flows of a reacting five-component air mixture consisting of N2, O2, NO, N, O behind a shock wave at different altitudes in the Earth's atmosphere and different speeds of the inlet flow are investigated. The lengths of the relaxation zones are considered to evaluate the applicability of one-temperature thermodynamics model for calculating the macroscopic fluid quantities behind the shock wave. The results of the flow simulation are obtained with in-house code developed for super- and hypersonic applications. The results from the code are compared with the results of numerical calculations computed with the equilibrium thermodynamics model.
AB - The influence of non-equilibrium kinetic processes on macroscopic parameters in air flows is a challenging and an important problem. Particularly, simulation of flows with high-temperature effects is important near the surface of spacecraft or meteorites when they enter the Earth's atmosphere. Non-equilibrium flows of a reacting five-component air mixture consisting of N2, O2, NO, N, O behind a shock wave at different altitudes in the Earth's atmosphere and different speeds of the inlet flow are investigated. The lengths of the relaxation zones are considered to evaluate the applicability of one-temperature thermodynamics model for calculating the macroscopic fluid quantities behind the shock wave. The results of the flow simulation are obtained with in-house code developed for super- and hypersonic applications. The results from the code are compared with the results of numerical calculations computed with the equilibrium thermodynamics model.
UR - http://www.scopus.com/inward/record.url?scp=85124259981&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/2154/1/012008
DO - 10.1088/1742-6596/2154/1/012008
M3 - Conference article
AN - SCOPUS:85124259981
VL - 2154
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
SN - 1742-6588
IS - 1
M1 - 012008
T2 - PETER 2021 New Models and Hydrocodes for Shock Wave Physics
Y2 - 25 May 2021 through 27 May 2021
ER -
ID: 93107763