Standard
Suppression of the separation zone by a spark discharge on laminar transonic airfoil. / Polivanov, P. A.; Sidorenko, A. A.; Maslov, A. A.
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. ed. / Fomin. Vol. 1893 American Institute of Physics Inc., 2017. 030154 (AIP Conference Proceedings; Vol. 1893).
Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
Harvard
Polivanov, PA, Sidorenko, AA & Maslov, AA 2017,
Suppression of the separation zone by a spark discharge on laminar transonic airfoil. in Fomin (ed.),
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. vol. 1893, 030154, AIP Conference Proceedings, vol. 1893, American Institute of Physics Inc., 25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017, Novosibirsk, Russian Federation,
05.06.2017.
https://doi.org/10.1063/1.5007612APA
Vancouver
Polivanov PA, Sidorenko AA, Maslov AA.
Suppression of the separation zone by a spark discharge on laminar transonic airfoil. In Fomin, editor, 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. Vol. 1893. American Institute of Physics Inc. 2017. 030154. (AIP Conference Proceedings). doi: 10.1063/1.5007612
Author
Polivanov, P. A. ; Sidorenko, A. A. ; Maslov, A. A. /
Suppression of the separation zone by a spark discharge on laminar transonic airfoil. 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. editor / Fomin. Vol. 1893 American Institute of Physics Inc., 2017. (AIP Conference Proceedings).
BibTeX
@inproceedings{53cb03d1e8044efab23ff6c0b85c220c,
title = "Suppression of the separation zone by a spark discharge on laminar transonic airfoil",
abstract = "The effect of plasma actuators on Shock Wave / Laminar Boundary Layer Interaction (SWBLI) was studied experimentally on transonic laminar aerofoil. The steady and unsteady characteristics of the separation zone were measured for several flow regimes including the transonic buffet. Multi Sliding Spark Discharge was used for the flow control. Successful suppression of separated flow and laminar transonic buffet by plasma actuators' was demonstrated. An analysis of the discharge pulse energy effect on SWBLI was carried out. The perturbation and thermal spot evolution generated by the discharge was studied in the zone of SWBLI.",
keywords = "FLOW",
author = "Polivanov, {P. A.} and Sidorenko, {A. A.} and Maslov, {A. A.}",
year = "2017",
month = oct,
day = "26",
doi = "10.1063/1.5007612",
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 - Suppression of the separation zone by a spark discharge on laminar transonic airfoil
AU - Polivanov, P. A.
AU - Sidorenko, A. A.
AU - Maslov, A. A.
PY - 2017/10/26
Y1 - 2017/10/26
N2 - The effect of plasma actuators on Shock Wave / Laminar Boundary Layer Interaction (SWBLI) was studied experimentally on transonic laminar aerofoil. The steady and unsteady characteristics of the separation zone were measured for several flow regimes including the transonic buffet. Multi Sliding Spark Discharge was used for the flow control. Successful suppression of separated flow and laminar transonic buffet by plasma actuators' was demonstrated. An analysis of the discharge pulse energy effect on SWBLI was carried out. The perturbation and thermal spot evolution generated by the discharge was studied in the zone of SWBLI.
AB - The effect of plasma actuators on Shock Wave / Laminar Boundary Layer Interaction (SWBLI) was studied experimentally on transonic laminar aerofoil. The steady and unsteady characteristics of the separation zone were measured for several flow regimes including the transonic buffet. Multi Sliding Spark Discharge was used for the flow control. Successful suppression of separated flow and laminar transonic buffet by plasma actuators' was demonstrated. An analysis of the discharge pulse energy effect on SWBLI was carried out. The perturbation and thermal spot evolution generated by the discharge was studied in the zone of SWBLI.
KW - FLOW
UR - http://www.scopus.com/inward/record.url?scp=85034264236&partnerID=8YFLogxK
U2 - 10.1063/1.5007612
DO - 10.1063/1.5007612
M3 - Conference contribution
AN - SCOPUS:85034264236
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 -
