Dielectric Barrier Discharge Plasma Actuators for Flow Control
By Thomas C. Corke, C. Enloe, Stephen Wilkinson. 2010
1,047 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Astronomy and Astrophysics, Radiology, Nuclear Medicine and Imaging
View Paper: https://www.semanticscholar.org/paper/9769b9f92e83715c4f3a8bc01f8fd3e31a705ef6
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Aerospace Engineering
- Marios Kotsonis
- Fulvio Scarano
- S. Ghaemi
- L. Veldhuis
- Igor V. Adamovich
- W. Lempert
- B. W. van Oudheusden
- Bernhard Wieneke
In Astronomy and Astrophysics
In Radiology, Nuclear Medicine and Imaging
Citations in the corpus
- Resolvent-analysis-based design of airfoil separation control (2018, neutral): “This magnitude is representative of those used in thermally actuated flow control studies (Corke et al. 2010; Sinha et al. 2012; Akins et al. 2015; Yeh et al. 2015).”
- Measurement of the body force field of plasma actuators (2011, background): “Comprehensive reviews on plasma actuators for aerodynamic flow control have been published recently [8, 9].”
- Characterization of a surface dielectric barrier discharge plasma sustained by repetitive nanosecond pulses (2010, background): “Plasmas generated in surface Dielectric Barrier Discharge (DBD) flow actuators have been extensively studied over the last decade (see [1,2] and references therein).”