Standard

State-to-state and simplified models for shock heated reacting air flows. / Kunova, O.V.; Nagnibeda, E.A.; Sharafutdinov, I.Z.

в: AIP Conference Proceedings, Том 1628, № 1, 2014, стр. 1194-1201.

Результаты исследований: Научные публикации в периодических изданиях › статья в журнале по материалам конференции › Рецензирование

Harvard

Kunova, OV, Nagnibeda, EA & Sharafutdinov, IZ 2014, 'State-to-state and simplified models for shock heated reacting air flows', AIP Conference Proceedings, Том. 1628, № 1, стр. 1194-1201. https://doi.org/10.1063/1.4902728

APA

Kunova, O. V., Nagnibeda, E. A., & Sharafutdinov, I. Z. (2014). State-to-state and simplified models for shock heated reacting air flows. AIP Conference Proceedings, 1628(1), 1194-1201. https://doi.org/10.1063/1.4902728

Vancouver

Kunova OV, Nagnibeda EA, Sharafutdinov IZ. State-to-state and simplified models for shock heated reacting air flows. AIP Conference Proceedings. 2014;1628(1):1194-1201. https://doi.org/10.1063/1.4902728

Author

Kunova, O.V. ; Nagnibeda, E.A. ; Sharafutdinov, I.Z. / State-to-state and simplified models for shock heated reacting air flows. в: AIP Conference Proceedings. 2014 ; Том 1628, № 1. стр. 1194-1201.

BibTeX

@article{d70c9a4821bc41f691c3a5def136d40e,
title = "State-to-state and simplified models for shock heated reacting air flows",
abstract = "Hypersonic flows of the five-component air mixture N2/O2/NO/N/O in the relaxation zone behind shock waves are studied on the basis of the state-to-state, three-temperature and one-temperature kinetic theory approaches. The equations of non-equilibrium vibrational and chemical kinetics are coupled to the gas dynamic equations and solved numerically for Mach numbers in the free stream M = 15. The results obtained using different approaches are compared and the influence of the kinetic model on the vibrational distributions, gas temperature, velocity and mixture composition is shown.",
author = "O.V. Kunova and E.A. Nagnibeda and I.Z. Sharafutdinov",
year = "2014",
doi = "10.1063/1.4902728",
language = "English",
volume = "1628",
pages = "1194--1201",
journal = "AIP Conference Proceedings",
issn = "0094-243X",
publisher = "American Institute of Physics",
number = "1",

}

RIS

TY - JOUR

T1 - State-to-state and simplified models for shock heated reacting air flows

AU - Kunova, O.V.

AU - Nagnibeda, E.A.

AU - Sharafutdinov, I.Z.

PY - 2014

Y1 - 2014

N2 - Hypersonic flows of the five-component air mixture N2/O2/NO/N/O in the relaxation zone behind shock waves are studied on the basis of the state-to-state, three-temperature and one-temperature kinetic theory approaches. The equations of non-equilibrium vibrational and chemical kinetics are coupled to the gas dynamic equations and solved numerically for Mach numbers in the free stream M = 15. The results obtained using different approaches are compared and the influence of the kinetic model on the vibrational distributions, gas temperature, velocity and mixture composition is shown.

AB - Hypersonic flows of the five-component air mixture N2/O2/NO/N/O in the relaxation zone behind shock waves are studied on the basis of the state-to-state, three-temperature and one-temperature kinetic theory approaches. The equations of non-equilibrium vibrational and chemical kinetics are coupled to the gas dynamic equations and solved numerically for Mach numbers in the free stream M = 15. The results obtained using different approaches are compared and the influence of the kinetic model on the vibrational distributions, gas temperature, velocity and mixture composition is shown.

U2 - 10.1063/1.4902728

DO - 10.1063/1.4902728

M3 - Conference article

VL - 1628

SP - 1194

EP - 1201

JO - AIP Conference Proceedings

JF - AIP Conference Proceedings

SN - 0094-243X

IS - 1

ER -

ID: 5726579