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Comparison of Detailed Chemical Models of Hydrogen Combustion in Numerical Simulations of Detonation. / Borisov, S. P.; Kudryavtsev, A. N.; Shershnev, A. A.

в: Combustion, Explosion and Shock Waves, Том 57, № 3, 05.2021, стр. 270-284.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Harvard

Borisov, SP, Kudryavtsev, AN & Shershnev, AA 2021, 'Comparison of Detailed Chemical Models of Hydrogen Combustion in Numerical Simulations of Detonation', Combustion, Explosion and Shock Waves, Том. 57, № 3, стр. 270-284. https://doi.org/10.1134/S0010508221030023

APA

Borisov, S. P., Kudryavtsev, A. N., & Shershnev, A. A. (2021). Comparison of Detailed Chemical Models of Hydrogen Combustion in Numerical Simulations of Detonation. Combustion, Explosion and Shock Waves, 57(3), 270-284. https://doi.org/10.1134/S0010508221030023

Vancouver

Borisov SP, Kudryavtsev AN, Shershnev AA. Comparison of Detailed Chemical Models of Hydrogen Combustion in Numerical Simulations of Detonation. Combustion, Explosion and Shock Waves. 2021 май;57(3):270-284. doi: 10.1134/S0010508221030023

Author

Borisov, S. P. ; Kudryavtsev, A. N. ; Shershnev, A. A. / Comparison of Detailed Chemical Models of Hydrogen Combustion in Numerical Simulations of Detonation. в: Combustion, Explosion and Shock Waves. 2021 ; Том 57, № 3. стр. 270-284.

BibTeX

@article{bb33859836244a63af3a61e780eda205,
title = "Comparison of Detailed Chemical Models of Hydrogen Combustion in Numerical Simulations of Detonation",
abstract = "Four detailed chemical mechanisms used to describe detonation combustion of hydrogen in oxygen are considered. Ignition delays for various temperatures and pressures are found, the Chapman–Jouguet velocity is determined, and the Zel{\textquoteright}dovich–von Neumann–D{\"o}ring solution for different models is obtained. The effect of dilution of the stoichiometric mixture of hydrogen and oxygen by an inert gas is estimated. Direct numerical simulation of detonation wave propagation in a channel is performed. The emergence of instability of the plane wave and formation of a cellular (multifront) structure are studied. The results predicted by different chemical models are analyzed and compared with each other and with available experimental data.",
keywords = "detonation cell size, GPU computations, ignition delay, instability of a plane detonation wave",
author = "Borisov, {S. P.} and Kudryavtsev, {A. N.} and Shershnev, {A. A.}",
note = "Funding Information: This work was supported by the Russian Foundation for Basic Research (Grant Nos. 16-57-48007, 18-08-01442, and 18-33-00740). Publisher Copyright: {\textcopyright} 2021, Pleiades Publishing, Ltd.",
year = "2021",
month = may,
doi = "10.1134/S0010508221030023",
language = "English",
volume = "57",
pages = "270--284",
journal = "Combustion, Explosion and Shock Waves",
issn = "0010-5082",
publisher = "Springer New York",
number = "3",

}

RIS

TY - JOUR

T1 - Comparison of Detailed Chemical Models of Hydrogen Combustion in Numerical Simulations of Detonation

AU - Borisov, S. P.

AU - Kudryavtsev, A. N.

AU - Shershnev, A. A.

N1 - Funding Information: This work was supported by the Russian Foundation for Basic Research (Grant Nos. 16-57-48007, 18-08-01442, and 18-33-00740). Publisher Copyright: © 2021, Pleiades Publishing, Ltd.

PY - 2021/5

Y1 - 2021/5

N2 - Four detailed chemical mechanisms used to describe detonation combustion of hydrogen in oxygen are considered. Ignition delays for various temperatures and pressures are found, the Chapman–Jouguet velocity is determined, and the Zel’dovich–von Neumann–Döring solution for different models is obtained. The effect of dilution of the stoichiometric mixture of hydrogen and oxygen by an inert gas is estimated. Direct numerical simulation of detonation wave propagation in a channel is performed. The emergence of instability of the plane wave and formation of a cellular (multifront) structure are studied. The results predicted by different chemical models are analyzed and compared with each other and with available experimental data.

AB - Four detailed chemical mechanisms used to describe detonation combustion of hydrogen in oxygen are considered. Ignition delays for various temperatures and pressures are found, the Chapman–Jouguet velocity is determined, and the Zel’dovich–von Neumann–Döring solution for different models is obtained. The effect of dilution of the stoichiometric mixture of hydrogen and oxygen by an inert gas is estimated. Direct numerical simulation of detonation wave propagation in a channel is performed. The emergence of instability of the plane wave and formation of a cellular (multifront) structure are studied. The results predicted by different chemical models are analyzed and compared with each other and with available experimental data.

KW - detonation cell size

KW - GPU computations

KW - ignition delay

KW - instability of a plane detonation wave

UR - http://www.scopus.com/inward/record.url?scp=85107066672&partnerID=8YFLogxK

U2 - 10.1134/S0010508221030023

DO - 10.1134/S0010508221030023

M3 - Article

AN - SCOPUS:85107066672

VL - 57

SP - 270

EP - 284

JO - Combustion, Explosion and Shock Waves

JF - Combustion, Explosion and Shock Waves

SN - 0010-5082

IS - 3

ER -

ID: 34056525