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Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply. / Zamuraev, V. P.; Kalinina, A. P.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ed. / Fomin. Vol. 2027 American Institute of Physics Inc., 2018. 040024 (AIP Conference Proceedings; Vol. 2027).

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

Harvard

Zamuraev, VP & Kalinina, AP 2018, Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply. in Fomin (ed.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. vol. 2027, 040024, AIP Conference Proceedings, vol. 2027, American Institute of Physics Inc., 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, Akademgorodok, Novosibirsk, Russian Federation, 13.08.2018. https://doi.org/10.1063/1.5065298

APA

Zamuraev, V. P., & Kalinina, A. P. (2018). Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply. In Fomin (Ed.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 (Vol. 2027). [040024] (AIP Conference Proceedings; Vol. 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065298

Vancouver

Zamuraev VP, Kalinina AP. Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply. In Fomin, editor, 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Vol. 2027. American Institute of Physics Inc. 2018. 040024. (AIP Conference Proceedings). doi: 10.1063/1.5065298

Author

Zamuraev, V. P. ; Kalinina, A. P. / Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply. 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. editor / Fomin. Vol. 2027 American Institute of Physics Inc., 2018. (AIP Conference Proceedings).

BibTeX

@inproceedings{21bb32ee72bc4ea3b85d0098c846900b,
title = "Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply",
abstract = "Numerical modeling based on the Reynolds-averaged Navier - Stokes equations has shown qualitatively the possibility to realize controlled energy release and to obtain a transonic mode with the help of a transverse control air jet, as in modeling based on the Euler equations. The determining role in ignition in the vortex and detachment regions formed near the jets of hydrogen or ethylene and air are played by shock waves.",
author = "Zamuraev, {V. P.} and Kalinina, {A. P.}",
note = "Publisher Copyright: {\textcopyright} 2018 Author(s).; 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 ; Conference date: 13-08-2018 Through 19-08-2018",
year = "2018",
month = nov,
day = "2",
doi = "10.1063/1.5065298",
language = "English",
volume = "2027",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin",
booktitle = "19th International Conference on the Methods of Aerophysical Research, ICMAR 2018",

}

RIS

TY - GEN

T1 - Controlling transonic region formation in the supersonic flow by jet and near-wall energy supply

AU - Zamuraev, V. P.

AU - Kalinina, A. P.

N1 - Publisher Copyright: © 2018 Author(s).

PY - 2018/11/2

Y1 - 2018/11/2

N2 - Numerical modeling based on the Reynolds-averaged Navier - Stokes equations has shown qualitatively the possibility to realize controlled energy release and to obtain a transonic mode with the help of a transverse control air jet, as in modeling based on the Euler equations. The determining role in ignition in the vortex and detachment regions formed near the jets of hydrogen or ethylene and air are played by shock waves.

AB - Numerical modeling based on the Reynolds-averaged Navier - Stokes equations has shown qualitatively the possibility to realize controlled energy release and to obtain a transonic mode with the help of a transverse control air jet, as in modeling based on the Euler equations. The determining role in ignition in the vortex and detachment regions formed near the jets of hydrogen or ethylene and air are played by shock waves.

UR - http://www.scopus.com/inward/record.url?scp=85056298955&partnerID=8YFLogxK

U2 - 10.1063/1.5065298

DO - 10.1063/1.5065298

M3 - Conference contribution

AN - SCOPUS:85056298955

VL - 2027

T3 - AIP Conference Proceedings

BT - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018

A2 - Fomin, null

PB - American Institute of Physics Inc.

T2 - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018

Y2 - 13 August 2018 through 19 August 2018

ER -

ID: 17412271