Flow Separation Control With Vortex Generators

2008 ◽  
Author(s):  
Benoit Gardarin ◽  
Laurent Jacquin ◽  
Philippe Geffroy
Keyword(s):  
Flow Separation ◽  
Vortex Generators ◽  
Separation Control ◽  
Flow Separation Control

scholarly journals Plasma Streamwise Vortex Generators for Flow Separation Control on Trucks

2018 ◽  
Vol 100 (4) ◽  
pp. 1101-1109 ◽  
Author(s):  
Julie A. Vernet ◽  
Ramis Örlü ◽  
David Söderblom ◽  
Per Elofsson ◽  
P. Henrik Alfredsson
Keyword(s):  
Flow Separation ◽  
Streamwise Vortex ◽  
Vortex Generators ◽  
Separation Control ◽  
Flow Separation Control

Design and Scaling of Plasma Streamwise Vortex Generators for Flow Separation Control

AIAA Journal ◽  
2016 ◽  
Vol 54 (11) ◽  
pp. 3397-3408 ◽  
Author(s):  
Christopher L. Kelley ◽  
Thomas C. Corke ◽  
Flint O. Thomas ◽  
Mehul Patel ◽  
Alan B. Cain
Keyword(s):  
Flow Separation ◽  
Streamwise Vortex ◽  
Vortex Generators ◽  
Separation Control ◽  
Flow Separation Control

Flow Separation Control on a Race Car Wing With Vortex Generators in Ground Effect

2009 ◽  
Vol 131 (12) ◽  
Author(s):  
Yuichi Kuya ◽  
Kenji Takeda ◽  
Xin Zhang ◽  
Scott Beeton ◽  
Ted Pandaleon
Keyword(s):  
Boundary Layer ◽  
Flow Separation ◽  
Large Scale ◽  
Vortex Generator ◽  
Ground Effect ◽  
Vortex Generators ◽  
Separation Control ◽  
Suction Surface ◽  
Flow Separation Control ◽  
Generator Type

Flow separation control using vortex generators on an inverted wing in ground effect is experimentally investigated, and its performance is characterized in terms of forces and pressure distributions over a range of incidence and ride height. Counter-rotating and co-rotating rectangular-vane type vortex generators are tested on the suction surface of the wing. The effect of device height and spacing is investigated. The counter-rotating sub-boundary layer vortex generators and counter-rotating large-scale vortex generators on the wing deliver 23% and 10% improvements in the maximum downforce, respectively, compared with the clean wing, at an incidence of one degree, and delay the onset of the downforce reduction phenomenon. The counter-rotating sub-boundary layer vortex generators exhibit up to 26% improvement in downforce and 10% improvement in aerodynamic efficiency at low ride heights. Chordwise pressure measurement confirms that both counter-rotating vortex generator configurations suppress flow separation, while the co-rotating vortex generators exhibit negligible effectiveness. This work shows that a use of vortex generators, notably of the counter-rotating sub-boundary layer vortex generator type, can be effective at controlling flow separation, with a resultant improvement in downforce for relatively low drag penalty.

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