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Numerical simulation of combustion initiation in hydrogen-air mixture in supersonic flow with energy impact. / Bedarev, I. A.; Vankova, O. S.; Goldfeld, M. A. и др.

Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. ред. / Fomin. Том 1893 American Institute of Physics Inc., 2017. 030141 (AIP Conference Proceedings; Том 1893).

Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование

Harvard

Bedarev, IA, Vankova, OS, Goldfeld, MA, Temerbekov, VM, Fedorova, NN & Fedorov, AV 2017, Numerical simulation of combustion initiation in hydrogen-air mixture in supersonic flow with energy impact. в Fomin (ред.), Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. Том. 1893, 030141, AIP Conference Proceedings, Том. 1893, American Institute of Physics Inc., 25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017, Novosibirsk, Российская Федерация, 05.06.2017. https://doi.org/10.1063/1.5007599

APA

Bedarev, I. A., Vankova, O. S., Goldfeld, M. A., Temerbekov, V. M., Fedorova, N. N., & Fedorov, A. V. (2017). Numerical simulation of combustion initiation in hydrogen-air mixture in supersonic flow with energy impact. в Fomin (Ред.), Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS (Том 1893). [030141] (AIP Conference Proceedings; Том 1893). American Institute of Physics Inc.. https://doi.org/10.1063/1.5007599

Vancouver

Bedarev IA, Vankova OS, Goldfeld MA, Temerbekov VM, Fedorova NN, Fedorov AV. Numerical simulation of combustion initiation in hydrogen-air mixture in supersonic flow with energy impact. в Fomin, Редактор, Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. Том 1893. American Institute of Physics Inc. 2017. 030141. (AIP Conference Proceedings). doi: 10.1063/1.5007599

Author

Bedarev, I. A. ; Vankova, O. S. ; Goldfeld, M. A. и др. / Numerical simulation of combustion initiation in hydrogen-air mixture in supersonic flow with energy impact. Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. Редактор / Fomin. Том 1893 American Institute of Physics Inc., 2017. (AIP Conference Proceedings).

BibTeX

@inproceedings{68f0dba8e7944097bebde0211b8b6b47,
title = "Numerical simulation of combustion initiation in hydrogen-air mixture in supersonic flow with energy impact",
abstract = "The results of numerical studies of the interaction of a detonation wave and an electron beam with supersonic reacting flows in channel of various configurations like channel with backward-facing step, symmetrical channel with abrupt expansion and channel with a cavity are presented. A mathematical technology has been created to implement such interaction based on the ANSYS Fluent software. The flow parameters at the outlet of the channel are compared for different channel configurations and ignition initiation ways. The possibility is shown to intensify the ignition in a supersonic flow by electron beams and pulsating detonation. The possibility is identified to use a cavity for stabilizing the combustion in a supersonic combustion chamber when exposed to a detonation wave.",
keywords = "IGNITION",
author = "Bedarev, {I. A.} and Vankova, {O. S.} and Goldfeld, {M. A.} and Temerbekov, {V. M.} and Fedorova, {N. N.} and Fedorov, {A. V.}",
year = "2017",
month = oct,
day = "26",
doi = "10.1063/1.5007599",
language = "English",
volume = "1893",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin",
booktitle = "Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017",
note = "25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017 ; Conference date: 05-06-2017 Through 09-06-2017",

}

RIS

TY - GEN

T1 - Numerical simulation of combustion initiation in hydrogen-air mixture in supersonic flow with energy impact

AU - Bedarev, I. A.

AU - Vankova, O. S.

AU - Goldfeld, M. A.

AU - Temerbekov, V. M.

AU - Fedorova, N. N.

AU - Fedorov, A. V.

PY - 2017/10/26

Y1 - 2017/10/26

N2 - The results of numerical studies of the interaction of a detonation wave and an electron beam with supersonic reacting flows in channel of various configurations like channel with backward-facing step, symmetrical channel with abrupt expansion and channel with a cavity are presented. A mathematical technology has been created to implement such interaction based on the ANSYS Fluent software. The flow parameters at the outlet of the channel are compared for different channel configurations and ignition initiation ways. The possibility is shown to intensify the ignition in a supersonic flow by electron beams and pulsating detonation. The possibility is identified to use a cavity for stabilizing the combustion in a supersonic combustion chamber when exposed to a detonation wave.

AB - The results of numerical studies of the interaction of a detonation wave and an electron beam with supersonic reacting flows in channel of various configurations like channel with backward-facing step, symmetrical channel with abrupt expansion and channel with a cavity are presented. A mathematical technology has been created to implement such interaction based on the ANSYS Fluent software. The flow parameters at the outlet of the channel are compared for different channel configurations and ignition initiation ways. The possibility is shown to intensify the ignition in a supersonic flow by electron beams and pulsating detonation. The possibility is identified to use a cavity for stabilizing the combustion in a supersonic combustion chamber when exposed to a detonation wave.

KW - IGNITION

UR - http://www.scopus.com/inward/record.url?scp=85034258231&partnerID=8YFLogxK

U2 - 10.1063/1.5007599

DO - 10.1063/1.5007599

M3 - Conference contribution

AN - SCOPUS:85034258231

VL - 1893

T3 - AIP Conference Proceedings

BT - Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017

A2 - Fomin, null

PB - American Institute of Physics Inc.

T2 - 25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017

Y2 - 5 June 2017 through 9 June 2017

ER -

ID: 9674477