Aerodynamic Flow Control of Bluff Bodies Using Synthetic Jet Actuators

1999 ◽  
pp. 273-278 ◽  
Author(s):  
M. Amitay ◽  
D. Smith ◽  
V. Kibens ◽  
D. Parekh ◽  
A. Glezer
Keyword(s):  
Flow Control ◽  
Synthetic Jet ◽  
Bluff Bodies ◽  
Synthetic Jet Actuators ◽  
Jet Actuators ◽  
Aerodynamic Flow Control

Aerodynamic Flow Control over an Unconventional Airfoil Using Synthetic Jet Actuators

AIAA Journal ◽  
2001 ◽  
Vol 39 (3) ◽  
pp. 361-370 ◽  
Author(s):  
Michael Amitay ◽  
Douglas R. Smith ◽  
Valdis Kibens ◽  
David E. Parekh ◽  
Ari Glezer
Keyword(s):  
Flow Control ◽  
Synthetic Jet ◽  
Synthetic Jet Actuators ◽  
Jet Actuators ◽  
Aerodynamic Flow Control

Aerodynamic flow control over an unconventional airfoil using synthetic jet actuators

AIAA Journal ◽  
2001 ◽  
Vol 39 ◽  
pp. 361-370 ◽  
Author(s):  
Michael Amitay ◽  
David E. Parekh ◽  
Douglas R. Smith ◽  
Valdis Kibens ◽  
Ari Glezer
Keyword(s):  
Flow Control ◽  
Synthetic Jet ◽  
Synthetic Jet Actuators ◽  
Jet Actuators ◽  
Aerodynamic Flow Control

10703 Study on condition of synthetic jet actuators for flow control around pantograph panhead using CFD analysis

2013 ◽  
Vol 2013.19 (0) ◽  
pp. 99-100
Author(s):  
Yasushi TAKANO ◽  
Takafumi OZAWA ◽  
Takeshi Mitsumodi ◽  
Yuichi SATO ◽  
Mitsuru IKEDA ◽  
...  
Keyword(s):  
Flow Control ◽  
Synthetic Jet ◽  
Cfd Analysis ◽  
Synthetic Jet Actuators ◽  
Jet Actuators

scholarly journals Investigation into clustering of synthetic jet actuators for flow separation control applications

2005 ◽  
Vol 109 (1091) ◽  
pp. 35-44 ◽  
Author(s):  
S. C. Liddle ◽  
N. J. Wood
Keyword(s):  
Boundary Layer ◽  
Flow Control ◽  
Input Signal ◽  
Streamwise Velocity ◽  
Synthetic Jet ◽  
Small Scale ◽  
Signal Phase ◽  
Control Applications ◽  
Synthetic Jet Actuators ◽  
Jet Actuators

Abstract An investigation into the behaviour of clustered synthetic jet Actuators for flow-control applications is described. Experiments have been undertaken with two small-scale synthetic jet actuators in a zero-pressure gradient boundary-layer, in order to investigate the effect of configuration yaw angle and relative input signal phase. Oil-flow visualisation and hotwire anemometry techniques were used, demonstrating that changes in the downstream flow structure could be observed. Compared to a streamwise configuration, in which a symmetrical counter-rotating vortex pair was produced by the synthetic jet-boundary-layer interaction, a broader asymmetric interaction was produced in a 15° yaw configuration. Streamwise velocity contour plots, illustrating the development of the interaction downstream, over four phase angles, were presented. Significant differences in the PSD analyses of downstream streamwise velocity time histories were found, suggesting that input signal phase could influence the stability and hence effectiveness of flow structures used in flow-control applications.

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