Mechanisms of SWBLI control by using a surface arc plasma actuator array

Author(s):  
Gan Tian ◽  
Wang Qiong
Keyword(s):  
2020 ◽  
Vol 29 (10) ◽  
pp. 105204
Author(s):  
Bing-Liang Tang ◽  
Shan-Guang Guo ◽  
Hua Liang ◽  
Meng-Xiao Tang

2015 ◽  
Vol 30 (2) ◽  
pp. 189
Author(s):  
LIU Shi-Xin ◽  
LI Xiao-Song ◽  
DENG Xiao-Qing ◽  
SUN Zhi-Guang ◽  
ZHU Ai-Min

2019 ◽  
Vol 12 (4) ◽  
pp. 180
Author(s):  
Harinaldi Harinaldi ◽  
Budiarso Budiarso ◽  
Fadli Cahya Megawanto ◽  
Riza Farrash Karim ◽  
Nely Toding Bunga ◽  
...  

Author(s):  
Milan Hrabovsky ◽  
M. Konrad ◽  
Vladimir Kopecky ◽  
J. Hlina ◽  
J. Benes ◽  
...  

Author(s):  
A. S. Anshakov ◽  
M. R. Predtechensky ◽  
V. S. Cherednichenko ◽  
O. M. Tukhto ◽  
E.K. Urbakh ◽  
...  
Keyword(s):  

2016 ◽  
Vol 47 (5) ◽  
pp. 495-512
Author(s):  
Alexander Petrovich Kuryachii ◽  
Sergey Viktorovich Manuilovich ◽  
Dmitriy Anatolyevich Rusyanov
Keyword(s):  

2020 ◽  
Vol 22 (4) ◽  
pp. 1047-1060
Author(s):  
S. Shadmani ◽  
S. M. Mousavi Nainiyan ◽  
R. Ghasemiasl ◽  
M. Mirzaei ◽  
S. G. Pouryoussefi

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.


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