Flow Control on Gö 387 Airfoil by Using Nanosecond Pulse Plasma Actuator

2015 ◽  
pp. 65-70 ◽  
Author(s):  
Kentaro Kato ◽  
Christian Breitsamter
Keyword(s):  
Flow Control ◽  
Plasma Actuator ◽  
Nanosecond Pulse ◽  
Pulse Plasma

Flow-Control Characteristics with Nanosecond-Pulse Plasma Actuator for Different Airfoil Shapes

AIAA Journal ◽  
2021 ◽  
pp. 1-9
Author(s):  
Atsushi Komuro ◽  
Shoki Kanno ◽  
Kento Suzuki ◽  
Akira Ando ◽  
Taku Nonomura ◽  
...  
Keyword(s):  
Flow Control ◽  
Plasma Actuator ◽  
Nanosecond Pulse ◽  
Pulse Plasma

Flow control over swept wings using nanosecond-pulse plasma actuator

2016 ◽  
Vol 61 ◽  
pp. 58-67
Author(s):  
Kentaro Kato ◽  
Christian Breitsamter ◽  
Shinnosuke Obi
Keyword(s):  
Flow Control ◽  
Plasma Actuator ◽  
Nanosecond Pulse ◽  
Pulse Plasma ◽  
Swept Wings

G0406 Experimental Study of Nano-second Pulse Plasma Actuator for Low Reynolds Number Separated Flow Control

2013 ◽  
Vol 2013 (0) ◽  
pp. _G0406-01_-_G0406-03_
Author(s):  
Satoshi SEKIMOTO ◽  
Sulaiman Taufik ◽  
Masayuki ANYOJI ◽  
Taku NONOMURA ◽  
Kozo FUJII
Keyword(s):  
Experimental Study ◽  
Reynolds Number ◽  
Flow Control ◽  
Low Reynolds Number ◽  
Separated Flow ◽  
Plasma Actuator ◽  
Pulse Plasma ◽  
Low Reynolds

PIV measurement of separation flow control around airfoil using nanosecond-pulse driven plasma actuator

2016 ◽  
Vol 2016 (0) ◽  
pp. 0304
Author(s):  
Naoki TANAKA ◽  
Kaiki KONNO ◽  
Atsushi KOMURO ◽  
Keisuke TAKASHIMA ◽  
Akira ANDO ◽  
...  
Keyword(s):  
Flow Control ◽  
Plasma Actuator ◽  
Nanosecond Pulse ◽  
Separation Flow ◽  
Piv Measurement

Experimental Study of Flow Control Over a Standard Road Vehicle Using Plasma Actuator

2020 ◽  
Vol 22 (4) ◽  
pp. 1047-1060
Author(s):  
S. Shadmani ◽  
S. M. Mousavi Nainiyan ◽  
R. Ghasemiasl ◽  
M. Mirzaei ◽  
S. G. Pouryoussefi
Keyword(s):  
Flow Control ◽  
Pressure Distribution ◽  
Drag Force ◽  
Separated Flow ◽  
Plasma Actuator ◽  
Road Vehicle ◽  
Slant Angle ◽  
Total Drag ◽  
Slant Surface ◽  
Ahmed Body

AbstractAhmed Body is a standard and simplified shape of a road vehicle that's rear part has an important role in flow structure and it's drag force. In this paper flow control around the Ahmed body with the rear slant angle of 25° studied by using the plasma actuator system situated in middle of the rear slant surface. Experiments conducted in a wind tunnel in two free stream velocities of U = 10m/s and U = 20m/s using steady and unsteady excitations. Pressure distribution and total drag force were measured and smoke flow visualization carried out in this study. The results showed that at U = 10m/s using plasma actuator suppress the separated flow over the rear slant slightly and be effective on pressure distribution. Also, total drag force reduces in steady and unsteady excitations for 3.65% and 2.44%, respectively. At U = 20m/s, using plasma actuator had no serious effect on the pressure distribution and total drag force.

scholarly journals Wing flow control using pulse thermal plasma actuator

2018 ◽  
Author(s):  
A. A. Kornyakov ◽  
A. V. Voevodin ◽  
D. A. Petrov ◽  
A. S. Petrov ◽  
G. G. Soudakov
Keyword(s):  
Flow Control ◽  
Thermal Plasma ◽  
Plasma Actuator
Sign in / Sign up

Export Citation Format

Share Document