Active Flow Control by Dielectric Barrier Discharge to Increase Stall Angle of a NACA0012 Airfoil
Author:
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
http://link.springer.com/content/pdf/10.1007/s13369-013-0772-1.pdf
Reference28 articles.
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3. Juckes, T.N.; Choi, K.S.: Flow control around a circular cylinder using pulsed dielectric barrier discharge surface plasma. Phys. Fluids 21 (2009). doi: 10.1063/1.3194307
4. Benard N., Jolibois J., Moreau E.: Lift and drag performances of an axisymmetric airfoil controlled by plasma actuator. J. Electrostat. 67, 133–139 (2009)
5. Porter C.O., Baughn J.W., Mclaughlin T.E., Enloe C.L., Font G.I.: Plasma actuator force measurements. AIAA J. 45(7), 1562–1570 (2007)
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