1st Flow Control Conference 2002
DOI: 10.2514/6.2002-2833
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Electrohydrodynamic Airflow Control Along a Flat Plate by a DC Surface Corona Discharge - Velocity Profile and Wall Pressure Measurements

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Cited by 49 publications
(34 citation statements)
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“…However, it does not allows us to measure both components of the electric wind velocity. To characterize the electric wind topology, 2D velocity fields can be obtained by particle image velocimetry (PIV), such as in Léger et al (2001Léger et al ( , 2002 for the first time. Several authors, as Kriegseis et al (2011b) and Kotsonis and Ghaemi (2011) among others, use now this type of system.…”
Section: Time-averaged Electric Wind Topologymentioning
confidence: 99%
“…However, it does not allows us to measure both components of the electric wind velocity. To characterize the electric wind topology, 2D velocity fields can be obtained by particle image velocimetry (PIV), such as in Léger et al (2001Léger et al ( , 2002 for the first time. Several authors, as Kriegseis et al (2011b) and Kotsonis and Ghaemi (2011) among others, use now this type of system.…”
Section: Time-averaged Electric Wind Topologymentioning
confidence: 99%
“…The momentum transfer to the flow is covered by the fractional efficiency of electrokinetic conversion for the electric wind of the corona discharge as the relation of the fluid mechanic (output) power P FM to the electrical actuator a) 13 ). Based on this report, the fluid mechanic efficiency can be defined [14][15][16][17] as…”
Section: Power Flow Diagrammentioning
confidence: 99%
“…The system of equations (7,8,9) is highly nonlinear and stiff, and therefore numerically difficult to solve. The numerical scheme implemented in this work has been adapted from that of Boeuf,2 and uses an implicit difference representation based on the exponential discretization method of Scharfetter and Gummel.…”
Section: Mmentioning
confidence: 99%
“…The use of plasma actuators in such a role may offer several advantages over traditional flow control devices (e.g., slats, flaps, slots). Some of these advantages may be -Reduced size and weight -Increased reliability 6 -Increased aerodynamic agility -Reduced drag 7 -High bandwidth No tail fins (leading to increased weapon load out of combat aircraft) 9 Plasma flow control devices will, no doubt, have disadvantages in comparison to traditional flow control devices as well. For example, plasma actuators may not perform well in adverse weather conditions and will require electrical power to operate, although it has been shown that this latter requirement can be mitigated through a "smart" actuator methodology.II Whether plasma actuators offer any demonstrable advantages over traditional flow control methodologies remains to be seen.…”
mentioning
confidence: 99%