Plasma control of boundary layer using low-temperature non-equilibrium plasma of gas discharge

D. F. Opaits; D. V. Roupassov; S. M. Starikovskaia; A. Yu Starikovskii; I. N. Zavialov; S. G. Saddoughi

doi:10.2514/6.2005-1180

Plasma control of boundary layer using low-temperature non-equilibrium plasma of gas discharge

D. F. Opaits
, D. V. Roupassov
, S. M. Starikovskaia
, A. Yu Starikovskii
, I. N. Zavialov
, S. G. Saddoughi

Moscow Institute of Physics and Technology
GE Global Research

Research output: Contribution to conference › Paper › peer-review

Abstract

The influence of barrier discharge on the flow pattern for the NACA-0015 profile within the velocity range 20 - 75 m/s was investigated. The pressure distribution near the profile was obtained by system of pressure gauges. Without discharge the stall angle was equal to 15⁰. When the additional momentum was produced by the actuator we obtained flow without separation up to angle of attack α = 21⁰. It was shown that gas acceleration by discharge can be explained by interaction between non-compensated charge in the streamer head region and strong electric field.

Original language	English
Pages	10469-10474
Number of pages	6
DOIs	https://doi.org/10.2514/6.2005-1180
Publication status	Published - 1 Jan 2005
Externally published	Yes
Event	43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States Duration: 10 Jan 2005 → 13 Jan 2005

Conference

Conference	43rd AIAA Aerospace Sciences Meeting and Exhibit
Country/Territory	United States
City	Reno, NV
Period	10/01/05 → 13/01/05

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10.2514/6.2005-1180

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title = "Plasma control of boundary layer using low-temperature non-equilibrium plasma of gas discharge",

abstract = "The influence of barrier discharge on the flow pattern for the NACA-0015 profile within the velocity range 20 - 75 m/s was investigated. The pressure distribution near the profile was obtained by system of pressure gauges. Without discharge the stall angle was equal to 150. When the additional momentum was produced by the actuator we obtained flow without separation up to angle of attack α = 210. It was shown that gas acceleration by discharge can be explained by interaction between non-compensated charge in the streamer head region and strong electric field.",

author = "Opaits, \{D. F.\} and Roupassov, \{D. V.\} and Starikovskaia, \{S. M.\} and Starikovskii, \{A. Yu\} and Zavialov, \{I. N.\} and Saddoughi, \{S. G.\}",

year = "2005",

month = jan,

day = "1",

doi = "10.2514/6.2005-1180",

language = "English",

pages = "10469--10474",

note = "43rd AIAA Aerospace Sciences Meeting and Exhibit ; Conference date: 10-01-2005 Through 13-01-2005",

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TY - CONF

T1 - Plasma control of boundary layer using low-temperature non-equilibrium plasma of gas discharge

AU - Opaits, D. F.

AU - Roupassov, D. V.

AU - Starikovskaia, S. M.

AU - Starikovskii, A. Yu

AU - Zavialov, I. N.

AU - Saddoughi, S. G.

PY - 2005/1/1

Y1 - 2005/1/1

N2 - The influence of barrier discharge on the flow pattern for the NACA-0015 profile within the velocity range 20 - 75 m/s was investigated. The pressure distribution near the profile was obtained by system of pressure gauges. Without discharge the stall angle was equal to 150. When the additional momentum was produced by the actuator we obtained flow without separation up to angle of attack α = 210. It was shown that gas acceleration by discharge can be explained by interaction between non-compensated charge in the streamer head region and strong electric field.

AB - The influence of barrier discharge on the flow pattern for the NACA-0015 profile within the velocity range 20 - 75 m/s was investigated. The pressure distribution near the profile was obtained by system of pressure gauges. Without discharge the stall angle was equal to 150. When the additional momentum was produced by the actuator we obtained flow without separation up to angle of attack α = 210. It was shown that gas acceleration by discharge can be explained by interaction between non-compensated charge in the streamer head region and strong electric field.

UR - https://www.scopus.com/pages/publications/30744451181

U2 - 10.2514/6.2005-1180

DO - 10.2514/6.2005-1180

M3 - Paper

AN - SCOPUS:30744451181

SP - 10469

EP - 10474

T2 - 43rd AIAA Aerospace Sciences Meeting and Exhibit

Y2 - 10 January 2005 through 13 January 2005

ER -

Plasma control of boundary layer using low-temperature non-equilibrium plasma of gas discharge

Abstract

Conference

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