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

Résultats de recherche: Contribution à une conférence › Papier › Revue par des pairs

Résumé

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.

langue originale	Anglais
Pages	10469-10474
Nombre de pages	6
Les DOIs	https://doi.org/10.2514/6.2005-1180
état	Publié - 1 janv. 2005
Modification externe	Oui
Evénement	43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, États-Unis Durée: 10 janv. 2005 → 13 janv. 2005

Une conférence

Une conférence	43rd AIAA Aerospace Sciences Meeting and Exhibit
Pays/Territoire	États-Unis
La ville	Reno, NV
période	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,

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doi = "10.2514/6.2005-1180",

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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

Résumé

Une conférence

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