Attenuation of cross-flow instability in three-dimensional boundary layer by means of multi-discharge actuator system
Keyword(s):
The Body
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Results of experiments in low-turbulence subsonic wind tunnel sustaining the possibility of significant attenuation of the cross-flow velocity and the intensity of stationary instability vortices due to the body force impact on three-dimensional boundary layer are presented. The unidirectional body force over a significant area of the streamlined surface has been created with the help of dielectric barrier discharge actuator.
Keyword(s):
1985 ◽
Vol 150
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pp. 329-356
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1970 ◽
Vol 41
(4)
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pp. 737-750
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Keyword(s):
Keyword(s):