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PLIF investigation of turbulent mixing in a model GT-combustor. / Savitskii, A. G.

International Conference on the Methods of Aerophysical Research, ICMAR 2020. ed. / Vasily M. Fomin; Alexander Shiplyuk. American Institute of Physics Inc., 2021. 040002 (AIP Conference Proceedings; Vol. 2351).

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

Harvard

Savitskii, AG 2021, PLIF investigation of turbulent mixing in a model GT-combustor. in VM Fomin & A Shiplyuk (eds), International Conference on the Methods of Aerophysical Research, ICMAR 2020., 040002, 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/10.1063/5.0051886

APA

Savitskii, A. G. (2021). PLIF investigation of turbulent mixing in a model GT-combustor. In V. M. Fomin, & A. Shiplyuk (Eds.), International Conference on the Methods of Aerophysical Research, ICMAR 2020 [040002] (AIP Conference Proceedings; Vol. 2351). American Institute of Physics Inc.. https://doi.org/10.1063/5.0051886

Vancouver

Savitskii AG. PLIF investigation of turbulent mixing in a model GT-combustor. In Fomin VM, Shiplyuk A, editors, International Conference on the Methods of Aerophysical Research, ICMAR 2020. American Institute of Physics Inc. 2021. 040002. (AIP Conference Proceedings). doi: 10.1063/5.0051886

Author

Savitskii, A. G. / PLIF investigation of turbulent mixing in a model GT-combustor. 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{db0b8020d3564ba2b6f7d2a877ace8d7,
title = "PLIF investigation of turbulent mixing in a model GT-combustor",
abstract = "This paper was focused on studying of turbulent mixing in a model gas-turbine combustor by using planar laser-induced fluorescence. The case of model fuel injection through the pilot jet with Re = 30 000 was considered. Acetone was used as a fluorescent tracer. Data processing methods including correction of sensor sensitivity, background signal correction and correction of non-uniformity of the laser sheet were described. The instantaneous and averaged concentration fields and the concentration pulsations were demonstrated.",
author = "Savitskii, {A. G.}",
note = "Funding Information: This work was supported by Russian Science Foundation (grant No. 19-79-10225). 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 = "10.1063/5.0051886",
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 - PLIF investigation of turbulent mixing in a model GT-combustor

AU - Savitskii, A. G.

N1 - Funding Information: This work was supported by Russian Science Foundation (grant No. 19-79-10225). Publisher Copyright: © 2021 Author(s). Copyright: Copyright 2021 Elsevier B.V., All rights reserved.

PY - 2021/5/24

Y1 - 2021/5/24

N2 - This paper was focused on studying of turbulent mixing in a model gas-turbine combustor by using planar laser-induced fluorescence. The case of model fuel injection through the pilot jet with Re = 30 000 was considered. Acetone was used as a fluorescent tracer. Data processing methods including correction of sensor sensitivity, background signal correction and correction of non-uniformity of the laser sheet were described. The instantaneous and averaged concentration fields and the concentration pulsations were demonstrated.

AB - This paper was focused on studying of turbulent mixing in a model gas-turbine combustor by using planar laser-induced fluorescence. The case of model fuel injection through the pilot jet with Re = 30 000 was considered. Acetone was used as a fluorescent tracer. Data processing methods including correction of sensor sensitivity, background signal correction and correction of non-uniformity of the laser sheet were described. The instantaneous and averaged concentration fields and the concentration pulsations were demonstrated.

UR - http://www.scopus.com/inward/record.url?scp=85107193336&partnerID=8YFLogxK

U2 - 10.1063/5.0051886

DO - 10.1063/5.0051886

M3 - Conference contribution

AN - SCOPUS:85107193336

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: 28753304