Large Eddy Simulation of NACA 6421 Airfoil with Coflow Jet Flow Control

2022 ◽  
Author(s):  
Philip E. Morgan ◽  
Daniel J. Garmann ◽  
Miguel R. Visbal
2020 ◽  
Vol 196 ◽  
pp. 104342
Author(s):  
Feng Xu ◽  
Wen-Li Chen ◽  
Zhong-Dong Duan ◽  
Jin-Ping Ou

2020 ◽  
Vol 198 ◽  
pp. 104398 ◽  
Author(s):  
Yunchao Yang ◽  
William Bradford Bartow ◽  
Gecheng Zha ◽  
Heyong Xu ◽  
Jianlei Wang

2013 ◽  
Vol 135 (10) ◽  
Author(s):  
Xingsi Han ◽  
Siniša Krajnović

The numerical study reported here deals with the passive flow control around a two-dimensional D-shaped bluff body at a Reynolds number of Re=3.6×104. A small circular control cylinder located in the near wake behind the main bluff body is employed as a local disturbance of the shear layer and the wake. 3D simulations are carried out using a newly developed very large eddy simulation (VLES) method, based on the standard k − ε turbulence model. The aim of this study is to validate the performance of this method for the complex flow control problem. Numerical results are compared with available experimental data, including global flow parameters and velocity profiles. Good agreements are observed. Numerical results suggest that the bubble recirculation length is increased by about 36% by the local disturbance of the small cylinder, which compares well to the experimental observations in which the length is increased by about 38%. A drag reduction of about 18% is observed in the VLES simulation, which is quite close to the experimental value of 17.5%. It is found that the VLES method is able to predict the flow control problem quite well.


2016 ◽  
Vol 8 ◽  
pp. 10-12 ◽  
Author(s):  
B.T. Kannan ◽  
P. Ssheshan ◽  
Sundararaj Senthilkumar

2010 ◽  
Vol 98 (10-11) ◽  
pp. 618-627 ◽  
Author(s):  
M. Salinas-Vázquez ◽  
W. Vicente ◽  
C. González-Rodríguez ◽  
E. Barrios-Bonilla ◽  
A. Espinosa-Gayosso

Author(s):  
Djavad Kamari ◽  
Mehran Tadjfar ◽  
Ali Tarokh

Abstract Large Eddy Simulation for active flow control (AFC) by employing synthetic and continuous blowing is done to investigate their effects on resizing separation. The flow around an SD7003 airfoil at Reynolds number of 60,000 and angles of attack of 13° is considered where a widespread separation occurs at post stall. In this work, the Dynamic Smagorinsky model is used as to calculate the turbulent viscosity.


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