Standard

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 изданияхстатья в журнале по материалам конференцииРецензирование

Harvard

Karpenko, AG, Tolstoguzov, SS & Volkov, KN 2022, 'Chemical kinetics in a five-component air behind shock waves', Journal of Physics: Conference Series, Том. 2154, № 1, 012008. https://doi.org/10.1088/1742-6596/2154/1/012008

APA

Karpenko, A. G., Tolstoguzov, S. S., & Volkov, K. N. (2022). Chemical kinetics in a five-component air behind shock waves. Journal of Physics: Conference Series, 2154(1), [012008]. https://doi.org/10.1088/1742-6596/2154/1/012008

Vancouver

Karpenko AG, Tolstoguzov SS, Volkov KN. Chemical kinetics in a five-component air behind shock waves. Journal of Physics: Conference Series. 2022 Янв. 19;2154(1). 012008. https://doi.org/10.1088/1742-6596/2154/1/012008

Author

Karpenko, A. G. ; Tolstoguzov, S. S. ; Volkov, K. N. / Chemical kinetics in a five-component air behind shock waves. в: Journal of Physics: Conference Series. 2022 ; Том 2154, № 1.

BibTeX

@article{6d6eb04a94b640b8852199ab1a38eed3,
title = "Chemical kinetics in a five-component air behind shock waves",
abstract = "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.",
author = "Karpenko, {A. G.} and Tolstoguzov, {S. S.} and Volkov, {K. N.}",
note = "Publisher Copyright: {\textcopyright} 2022 Institute of Physics Publishing. All rights reserved.; PETER 2021 New Models and Hydrocodes for Shock Wave Physics ; Conference date: 25-05-2021 Through 27-05-2021",
year = "2022",
month = jan,
day = "19",
doi = "10.1088/1742-6596/2154/1/012008",
language = "English",
volume = "2154",
journal = "Journal of Physics: Conference Series",
issn = "1742-6588",
publisher = "IOP Publishing Ltd.",
number = "1",

}

RIS

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