Standard

Deceleration of a supersonic flow down to transonic speeds using gas-dynamic pulses during combustion of hydrocarbon fuels. / Zamuraev, V. P.; Kalinina, A. P.

International Conference on the Methods of Aerophysical Research, ICMAR 2020. ed. / Vasily M. Fomin; Alexander Shiplyuk. American Institute of Physics Inc., 2021. 030050 (AIP Conference Proceedings; Vol. 2351).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Zamuraev, VP & Kalinina, AP 2021, Deceleration of a supersonic flow down to transonic speeds using gas-dynamic pulses during combustion of hydrocarbon fuels. in VM Fomin & A Shiplyuk (eds), International Conference on the Methods of Aerophysical Research, ICMAR 2020., 030050, AIP Conference Proceedings, vol. 2351, American Institute of Physics Inc., 20th International Conference on the Methods of Aerophysical Research, ICMAR 2020, Akademgorodok, Novosibirsk, Russian Federation, 01.11.2020. https://doi.org/10.1063/5.0052907

APA

Zamuraev, V. P., & Kalinina, A. P. (2021). Deceleration of a supersonic flow down to transonic speeds using gas-dynamic pulses during combustion of hydrocarbon fuels. In V. M. Fomin, & A. Shiplyuk (Eds.), International Conference on the Methods of Aerophysical Research, ICMAR 2020 [030050] (AIP Conference Proceedings; Vol. 2351). American Institute of Physics Inc.. https://doi.org/10.1063/5.0052907

Vancouver

Zamuraev VP, Kalinina AP. Deceleration of a supersonic flow down to transonic speeds using gas-dynamic pulses during combustion of hydrocarbon fuels. In Fomin VM, Shiplyuk A, editors, International Conference on the Methods of Aerophysical Research, ICMAR 2020. American Institute of Physics Inc. 2021. 030050. (AIP Conference Proceedings). doi: 10.1063/5.0052907

Author

Zamuraev, V. P. ; Kalinina, A. P. / Deceleration of a supersonic flow down to transonic speeds using gas-dynamic pulses during combustion of hydrocarbon fuels. International Conference on the Methods of Aerophysical Research, ICMAR 2020. editor / Vasily M. Fomin ; Alexander Shiplyuk. American Institute of Physics Inc., 2021. (AIP Conference Proceedings).

BibTeX

@inproceedings{38eeecc967764a3ca20a0b6d209ce744,
title = "Deceleration of a supersonic flow down to transonic speeds using gas-dynamic pulses during combustion of hydrocarbon fuels",
abstract = "Creation of a transonic region by means of gas fuel burning in a supersonic flow with a Mach number M = 2 in a channel with a variable cross section is studied numerically. The averaged Navier - Stokes equations closed by the k-? model of turbulence are solved. The transonic region is created by using gas-dynamic pulses of a throttling jet, which initiates gaseous fuel combustion in the channel region with a constant cross section. The fuel (ethylene or kerosene) is supplied axially into the axisymmetric channel. It is shown that initiation of kerosene combustion requires using gas-dynamic pulses of higher power than those in the ethylene case. The evolution of the kerosene combustion process in channels of different lengths is studied. It is shown that the pulse action duration required for initiation increases with the length of the channel region with a constant cross section.",
author = "Zamuraev, {V. P.} and Kalinina, {A. P.}",
note = "Funding Information: This work was performed within the Program of the fundamental scientific research of the state academies of sciences in 2013–2020 (project AAAA-A17-117030610135-6) and with the financial support of the Russian Foundation for Basic Research (grant No. 20-08-00245). Publisher Copyright: {\textcopyright} 2021 Author(s). Copyright: Copyright 2021 Elsevier B.V., All rights reserved.; 20th International Conference on the Methods of Aerophysical Research, ICMAR 2020 ; Conference date: 01-11-2020 Through 07-11-2020",
year = "2021",
month = may,
day = "24",
doi = "10.1063/5.0052907",
language = "English",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin, {Vasily M.} and Alexander Shiplyuk",
booktitle = "International Conference on the Methods of Aerophysical Research, ICMAR 2020",

}

RIS

TY - GEN

T1 - Deceleration of a supersonic flow down to transonic speeds using gas-dynamic pulses during combustion of hydrocarbon fuels

AU - Zamuraev, V. P.

AU - Kalinina, A. P.

N1 - Funding Information: This work was performed within the Program of the fundamental scientific research of the state academies of sciences in 2013–2020 (project AAAA-A17-117030610135-6) and with the financial support of the Russian Foundation for Basic Research (grant No. 20-08-00245). Publisher Copyright: © 2021 Author(s). Copyright: Copyright 2021 Elsevier B.V., All rights reserved.

PY - 2021/5/24

Y1 - 2021/5/24

N2 - Creation of a transonic region by means of gas fuel burning in a supersonic flow with a Mach number M = 2 in a channel with a variable cross section is studied numerically. The averaged Navier - Stokes equations closed by the k-? model of turbulence are solved. The transonic region is created by using gas-dynamic pulses of a throttling jet, which initiates gaseous fuel combustion in the channel region with a constant cross section. The fuel (ethylene or kerosene) is supplied axially into the axisymmetric channel. It is shown that initiation of kerosene combustion requires using gas-dynamic pulses of higher power than those in the ethylene case. The evolution of the kerosene combustion process in channels of different lengths is studied. It is shown that the pulse action duration required for initiation increases with the length of the channel region with a constant cross section.

AB - Creation of a transonic region by means of gas fuel burning in a supersonic flow with a Mach number M = 2 in a channel with a variable cross section is studied numerically. The averaged Navier - Stokes equations closed by the k-? model of turbulence are solved. The transonic region is created by using gas-dynamic pulses of a throttling jet, which initiates gaseous fuel combustion in the channel region with a constant cross section. The fuel (ethylene or kerosene) is supplied axially into the axisymmetric channel. It is shown that initiation of kerosene combustion requires using gas-dynamic pulses of higher power than those in the ethylene case. The evolution of the kerosene combustion process in channels of different lengths is studied. It is shown that the pulse action duration required for initiation increases with the length of the channel region with a constant cross section.

UR - http://www.scopus.com/inward/record.url?scp=85107223092&partnerID=8YFLogxK

U2 - 10.1063/5.0052907

DO - 10.1063/5.0052907

M3 - Conference contribution

AN - SCOPUS:85107223092

T3 - AIP Conference Proceedings

BT - International Conference on the Methods of Aerophysical Research, ICMAR 2020

A2 - Fomin, Vasily M.

A2 - Shiplyuk, Alexander

PB - American Institute of Physics Inc.

T2 - 20th International Conference on the Methods of Aerophysical Research, ICMAR 2020

Y2 - 1 November 2020 through 7 November 2020

ER -

ID: 28866391