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Separation control by NEQLab's nanosecond plasma actuator

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Uploaded by on Apr 26, 2010

This video is shot during the joint experiments performed by NEQLab and TU
Delft Aerospace Dept. The nanosecond plasma actuator applied onto an
airfoil controls the flow separation at flow speeds up to 40 m/s (maximum
speed for this tunnel). The effect can be seen by means of tufts applied
onto the airfoil. More information can be found at http://www.neqlab.com

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  • Do you guys have more videos?

  • I will like to see more about your set-up. How you placed the airfoil and why you chose a vertical wind tunnel?

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