Computational-experimental study of hydrogen ignition with distributed injection from pylons into a supersonic flow

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Computational-experimental study of hydrogen ignition with distributed injection from pylons into a supersonic flow. / Akinin, S. A.; Starov, A. V.

International Conference on the Methods of Aerophysical Research, ICMAR 2020. ed. / Vasily M. Fomin; Alexander Shiplyuk. American Institute of Physics Inc., 2021. 040010 (AIP Conference Proceedings; Vol. 2351).

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

Harvard

Akinin, SA & Starov, AV 2021, Computational-experimental study of hydrogen ignition with distributed injection from pylons into a supersonic flow. in VM Fomin & A Shiplyuk (eds), International Conference on the Methods of Aerophysical Research, ICMAR 2020., 040010, 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/10.1063/5.0052139

APA

Akinin, S. A., & Starov, A. V. (2021). Computational-experimental study of hydrogen ignition with distributed injection from pylons into a supersonic flow. In V. M. Fomin, & A. Shiplyuk (Eds.), International Conference on the Methods of Aerophysical Research, ICMAR 2020 [040010] (AIP Conference Proceedings; Vol. 2351). American Institute of Physics Inc.. https://doi.org/10.1063/5.0052139

Vancouver

Akinin SA, Starov AV. Computational-experimental study of hydrogen ignition with distributed injection from pylons into a supersonic flow. In Fomin VM, Shiplyuk A, editors, International Conference on the Methods of Aerophysical Research, ICMAR 2020. American Institute of Physics Inc. 2021. 040010. (AIP Conference Proceedings). doi: 10.1063/5.0052139

Author

Akinin, S. A. ; Starov, A. V. / Computational-experimental study of hydrogen ignition with distributed injection from pylons into a supersonic flow. 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{77bc8fd61bbe450d8f151cd6f50681f4,

title = "Computational-experimental study of hydrogen ignition with distributed injection from pylons into a supersonic flow",

abstract = "The tests were carried out in the hot-shot wind tunnel IT-302M ITAM SB RAS in the attached pipe-line mode with Men = 3. Numerical simulation was performed using ANSYS FLUENT in a three-dimensional formulation. Satisfactory agreement between the calculated and experimental data is shown. The zones are determined in the section of the combustion chamber with a constant cross-sectional area of possible self-ignition of hydrogen with distributed injection from the pylons from the point of view of satisfying the ignition parameters. Ignition parameters are understood as static pressure and temperature levels, as well as ignition limits for local fuel-air equivalence ratio.",

author = "Akinin, {S. A.} and Starov, {A. V.}",

note = "Funding Information: The reported study was funded by RFBR according to the research project No. 18-08-01172. Publisher Copyright: {\textcopyright} 2021 Author(s).; 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 = "10.1063/5.0052139",

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 - Computational-experimental study of hydrogen ignition with distributed injection from pylons into a supersonic flow

AU - Akinin, S. A.

AU - Starov, A. V.

PY - 2021/5/24

Y1 - 2021/5/24

N2 - The tests were carried out in the hot-shot wind tunnel IT-302M ITAM SB RAS in the attached pipe-line mode with Men = 3. Numerical simulation was performed using ANSYS FLUENT in a three-dimensional formulation. Satisfactory agreement between the calculated and experimental data is shown. The zones are determined in the section of the combustion chamber with a constant cross-sectional area of possible self-ignition of hydrogen with distributed injection from the pylons from the point of view of satisfying the ignition parameters. Ignition parameters are understood as static pressure and temperature levels, as well as ignition limits for local fuel-air equivalence ratio.

AB - The tests were carried out in the hot-shot wind tunnel IT-302M ITAM SB RAS in the attached pipe-line mode with Men = 3. Numerical simulation was performed using ANSYS FLUENT in a three-dimensional formulation. Satisfactory agreement between the calculated and experimental data is shown. The zones are determined in the section of the combustion chamber with a constant cross-sectional area of possible self-ignition of hydrogen with distributed injection from the pylons from the point of view of satisfying the ignition parameters. Ignition parameters are understood as static pressure and temperature levels, as well as ignition limits for local fuel-air equivalence ratio.

UR - http://www.scopus.com/inward/record.url?scp=85107232248&partnerID=8YFLogxK

U2 - 10.1063/5.0052139

DO - 10.1063/5.0052139

M3 - Conference contribution

AN - SCOPUS:85107232248

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: 34054331