Plasma-Actuator Burst-Mode Frequency Effects on Leading-Edge Flow-Separation Control at Reynolds Number 2.6×105

AIAA Journal ◽  
2017 ◽  
Vol 55 (11) ◽  
pp. 3789-3806 ◽  
Author(s):  
Hikaru Aono ◽  
Soshi Kawai ◽  
Taku Nonomura ◽  
Makoto Sato ◽  
Kozo Fujii ◽  
...  
2017 ◽  
Vol 54 (1) ◽  
pp. 301-309 ◽  
Author(s):  
Xin Zhang ◽  
Hua-Xing Li ◽  
Yong Huang ◽  
Wan-Bo Wang

AIAA Journal ◽  
2009 ◽  
Vol 47 (1) ◽  
pp. 168-185 ◽  
Author(s):  
D. V. Roupassov ◽  
A. A. Nikipelov ◽  
M. M. Nudnova ◽  
A. Yu. Starikovskii

Author(s):  
M. Tadjfar ◽  
D. J. Kamari

Abstract The effects of applying a coupled unsteady blowing and suction combination over SD7003 airfoil at Reynolds number of 60,000 at an angle of attack of 13°, where a large separation on the suction side of the airfoil existed, was considered to investigate active flow control (AFC) mechanism. URANS equations were employed to solve the flow field and k–ω SST was used as the turbulence model. The unsteady blowing and suction were implemented at an angle to the surface crossing the boundary layer (CBL). The influence of location and frequency of the blowing/suction jets were examined.


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