Optimization of a synthetic jet actuator for flow control around an airfoil
This paper deals with the optimization of a synthetic jet actuator parameters in the control flow around the NACA0015 airfoil at two angles of attack: 13° (i.e. the stall angle of NACA0015) and 16° (i.e. the post stall angle of NACA0015) to maximize the aerodynamic performance of the airfoil. Synthe...
| Main Authors: | , , , , , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
IOP Publishing
2016
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| Online Access: | http://psasir.upm.edu.my/id/eprint/53445/1/Optimization%20of%20a%20synthetic%20jet%20actuator%20for%20flow%20control.pdf |