Attenuation of cross-flow-type instability in compressible boundary layer by means of plasma actuators
Author:
Affiliation:
1. TsAGI
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-321
Reference35 articles.
1. Laminar flow control research at TsAGI: Past and present
2. Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma
3. 4Mack,L.M."OntheStabilityoftheBoundaryLayeronaTransonicSweptWing,"AIAAPaper1979-264,1979.
4. ATTENUATION OF CROSS FLOW-TYPE INSTABILITY IN A 3D BOUNDARY LAYER DUE TO VOLUMETRIC FORCE IMPACT
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