Experimental Characterization of a Supersonic Flow Control Actuator

2006 ◽  
Author(s):  
Bohdan Cybyk ◽  
H Land ◽  
Daniel Simon ◽  
Jun Chen ◽  
Joseph Katz
Keyword(s):  
Supersonic Flow ◽  
Flow Control ◽  
Experimental Characterization ◽  
Supersonic Flow Control

Characterization of a High-Frequency Pulsed-Plasma Jet Actuator for Supersonic Flow Control

AIAA Journal ◽  
2010 ◽  
Vol 48 (2) ◽  
pp. 297-305 ◽  
Author(s):  
Venkateswaran Narayanaswamy ◽  
Laxminarayan L. Raja ◽  
Noel T. Clemens
Keyword(s):  
Supersonic Flow ◽  
Flow Control ◽  
High Frequency ◽  
Plasma Jet ◽  
Pulsed Plasma ◽  
Supersonic Flow Control

A note on supersonic flow control with nanosecond plasma actuator

2018 ◽  
Vol 30 (4) ◽  
pp. 040907 ◽  
Author(s):  
J. G. Zheng ◽  
Y. D. Cui ◽  
J. Li ◽  
B. C. Khoo
Keyword(s):  
Supersonic Flow ◽  
Flow Control ◽  
Plasma Actuator ◽  
Supersonic Flow Control

Experimental Characterization of a Micro-Blower for Flow Control

2019 ◽  
Author(s):  
Maria Wu ◽  
Pierre Sullivan
Keyword(s):  
Flow Control ◽  
Turbulent Jets ◽  
Synthetic Jet ◽  
Experimental Characterization ◽  
Continuous Mode ◽  
Mean Velocity ◽  
Burst Mode ◽  
Synthetic Jet Actuator ◽  
Image Velocimetry

Abstract A compact, lightweight, low-power piezoelectric micro-blower was characterized using particle image velocimetry to determine its flow control potential. The micro-blower has been operated in continuous mode as well as in burst mode using two different actuation frequencies. The maximum mean velocity measured with the micro-blower operating in continuous mode was approximately Ūmax = 13 m/s which occurred at the centerline at an approximate stream-wise location of x/d = 4. The velocity profiles in the developed region resemble those of turbulent jets. The momentum-flux from the micro-blower in continuous mode was significantly greater than a typical synthetic jet actuator which was successfully used for flow control, indicating that the micro-blower can impart the necessary momentum to be effective for flow control. With burst mode, the results show that the micro-blower could impart an even greater momentum.

E07 Supersonic Flow Control on a Forward Ramp Using SDBD Plasma Actuators

2008 ◽  
Vol 2008 (0) ◽  
pp. 175-176
Author(s):  
Hironori ARAHORI ◽  
Takashi MATSUNO ◽  
Hiromitsu KAWAZOE
Keyword(s):  
Supersonic Flow ◽  
Flow Control ◽  
Plasma Actuators ◽  
Supersonic Flow Control

Virtual Shapes in Supersonic Flow Control with Energy Addition

2008 ◽  
Vol 24 (5) ◽  
pp. 900-915 ◽  
Author(s):  
M. N. Shneider ◽  
S. O. Macheret ◽  
S. H. Zaidi ◽  
I. G. Girgis ◽  
R. B. Miles
Keyword(s):  
Supersonic Flow ◽  
Flow Control ◽  
Energy Addition ◽  
Supersonic Flow Control
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