scholarly journals Active Flow Separation Control on a High-Lift Wing-Body Configuration Part 1: Baseline Flow and Constant Blowing

2011 ◽  
Author(s):  
Timo Kühn ◽  
Vlad Ciobaca ◽  
Ralf Rudnik ◽  
Burkhard Gölling ◽  
Wiebke Breitenstein
Keyword(s):  
Flow Separation ◽  
Separation Control ◽  
High Lift ◽  
Flow Separation Control ◽  
Baseline Flow ◽  
Active Flow

Active Flow-Separation Control on a High-Lift Wing-Body Configuration

2013 ◽  
Vol 50 (1) ◽  
pp. 56-72 ◽  
Author(s):  
Vlad Ciobaca ◽  
Timo Kühn ◽  
Ralf Rudnik ◽  
Matthias Bauer ◽  
Burkhard Gölling ◽  
...  
Keyword(s):  
Flow Separation ◽  
Separation Control ◽  
High Lift ◽  
Flow Separation Control ◽  
Active Flow

scholarly journals Active flow separation control at the outer wing

2019 ◽  
Vol 11 (4) ◽  
pp. 823-836 ◽  
Author(s):  
J. P. Rosenblum ◽  
P. Vrchota ◽  
A. Prachar ◽  
S. H. Peng ◽  
S. Wallin ◽  
...  
Keyword(s):  
Flow Separation ◽  
Separation Control ◽  
Flow Separation Control ◽  
Active Flow

Numerical study of passive and active flow separation control over a NACA0012 airfoil

2008 ◽  
Vol 37 (8) ◽  
pp. 975-992 ◽  
Author(s):  
Hua Shan ◽  
Li Jiang ◽  
Chaoqun Liu ◽  
Michael Love ◽  
Brant Maines
Keyword(s):  
Flow Separation ◽  
Numerical Study ◽  
Separation Control ◽  
Flow Separation Control ◽  
Naca0012 Airfoil ◽  
Active Flow

Coupled Blowing and Suction for Flow Separation Control

2019 ◽  
Author(s):  
M. Tadjfar ◽  
D. J. Kamari
Keyword(s):  
Boundary Layer ◽  
Reynolds Number ◽  
Flow Field ◽  
Turbulence Model ◽  
Flow Separation ◽  
Active Flow Control ◽  
Suction Side ◽  
Separation Control ◽  
Flow Separation Control ◽  
Active Flow

Abstract The effects of applying a coupled unsteady blowing and suction combination over SD7003 airfoil at Reynolds number of 60,000 at an angle of attack of 13°, where a large separation on the suction side of the airfoil existed, was considered to investigate active flow control (AFC) mechanism. URANS equations were employed to solve the flow field and k–ω SST was used as the turbulence model. The unsteady blowing and suction were implemented at an angle to the surface crossing the boundary layer (CBL). The influence of location and frequency of the blowing/suction jets were examined.

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