Standard

Development and testing of a numerical simulation method for thermally nonequilibrium dissociating flows in ANSYS Fluent. / Shoev, G.V.; Bondar, Y.A.; Oblapenko, G.P.; Kustova, E.V.

In: Thermophysics and Aeromechanics, Vol. 23, No. 2, 2016, p. 151-163.

Research output: Contribution to journal › Article › peer-review

Harvard

Shoev, GV, Bondar, YA, Oblapenko, GP & Kustova, EV 2016, 'Development and testing of a numerical simulation method for thermally nonequilibrium dissociating flows in ANSYS Fluent', Thermophysics and Aeromechanics, vol. 23, no. 2, pp. 151-163. https://doi.org/10.1134/S0869864316020013

APA

Shoev, G. V., Bondar, Y. A., Oblapenko, G. P., & Kustova, E. V. (2016). Development and testing of a numerical simulation method for thermally nonequilibrium dissociating flows in ANSYS Fluent. Thermophysics and Aeromechanics, 23(2), 151-163. https://doi.org/10.1134/S0869864316020013

Vancouver

Shoev GV, Bondar YA, Oblapenko GP, Kustova EV. Development and testing of a numerical simulation method for thermally nonequilibrium dissociating flows in ANSYS Fluent. Thermophysics and Aeromechanics. 2016;23(2):151-163. https://doi.org/10.1134/S0869864316020013

Author

Shoev, G.V. ; Bondar, Y.A. ; Oblapenko, G.P. ; Kustova, E.V. / Development and testing of a numerical simulation method for thermally nonequilibrium dissociating flows in ANSYS Fluent. In: Thermophysics and Aeromechanics. 2016 ; Vol. 23, No. 2. pp. 151-163.

BibTeX

@article{1082f2c52da34fde90189f4f6153d252,
title = "Development and testing of a numerical simulation method for thermally nonequilibrium dissociating flows in ANSYS Fluent",
abstract = "{\textcopyright} 2016, Pleiades Publishing, Ltd.Various issues of numerical simulation of supersonic gas flows with allowance for thermochemical nonequilibrium on the basis of fluid dynamic equations in the two-temperature approximation are discussed. The computational tool for modeling flows with thermochemical nonequilibrium is the commercial software package ANSYS Fluent with an additional userdefined open-code module. A comparative analysis of results obtained by various models of vibration-dissociation coupling in binary gas mixtures of nitrogen and oxygen is performed. Results of numerical simulations are compared with available experimental data.",
author = "G.V. Shoev and Y.A. Bondar and G.P. Oblapenko and E.V. Kustova",
year = "2016",
doi = "10.1134/S0869864316020013",
language = "English",
volume = "23",
pages = "151--163",
journal = "Thermophysics and Aeromechanics",
issn = "0869-8643",
publisher = "МАИК {"}Наука/Интерпериодика{"}",
number = "2",

}

RIS

TY - JOUR

T1 - Development and testing of a numerical simulation method for thermally nonequilibrium dissociating flows in ANSYS Fluent

AU - Shoev, G.V.

AU - Bondar, Y.A.

AU - Oblapenko, G.P.

AU - Kustova, E.V.

PY - 2016

Y1 - 2016

N2 - © 2016, Pleiades Publishing, Ltd.Various issues of numerical simulation of supersonic gas flows with allowance for thermochemical nonequilibrium on the basis of fluid dynamic equations in the two-temperature approximation are discussed. The computational tool for modeling flows with thermochemical nonequilibrium is the commercial software package ANSYS Fluent with an additional userdefined open-code module. A comparative analysis of results obtained by various models of vibration-dissociation coupling in binary gas mixtures of nitrogen and oxygen is performed. Results of numerical simulations are compared with available experimental data.

AB - © 2016, Pleiades Publishing, Ltd.Various issues of numerical simulation of supersonic gas flows with allowance for thermochemical nonequilibrium on the basis of fluid dynamic equations in the two-temperature approximation are discussed. The computational tool for modeling flows with thermochemical nonequilibrium is the commercial software package ANSYS Fluent with an additional userdefined open-code module. A comparative analysis of results obtained by various models of vibration-dissociation coupling in binary gas mixtures of nitrogen and oxygen is performed. Results of numerical simulations are compared with available experimental data.

U2 - 10.1134/S0869864316020013

DO - 10.1134/S0869864316020013

M3 - Article

VL - 23

SP - 151

EP - 163

JO - Thermophysics and Aeromechanics

JF - Thermophysics and Aeromechanics

SN - 0869-8643

IS - 2

ER -

ID: 7926993