An implicit large-eddy simulation is carried out to study turbulent boundary-layer separation from a backward-facing rounded ramp with active wall actuation control. This method, called spanwise alternating distributed strips control, is imposed onto the flat plate surface upstream of a rounded ramp by alternatively applying out-of-phase control and in-phase control to the wall-normal velocity component in the spanwise direction. As a result, the local turbulence intensity is alternatively suppressed and enhanced, leading to the creation of vertical shear-layers, which is responsible for the presence of large-scale streamwise vortices. These vortices exert a predominant influence on the suppression of the flow separation. The interaction between the large-scale vortices and the downstream recirculation zone and free shear-layer is studied by examining flow statistics. It is found that in comparison with the non-controlled case, the flow separation is delayed, the reattachment point is shifted upstream, and the length of the mean recirculation zone is reduced up to 8.49%. The optimal control case is achieved with narrow in-phase control strips. An in-depth analysis shows that the delay of the flow separation is attributed to the activation of the near-wall turbulence by the in-phase control strips and the improvement of the reattachment location is mainly due to the large-scale streamwise vortices, which enhance the momentum transport between the main flow and separated region.
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January 2019
Research Article|
January 04 2019
Flow separation control over a rounded ramp with spanwise alternating wall actuation Available to Purchase
Weidan Ni (倪玮丹)
;
Weidan Ni (倪玮丹)
1
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University
, Beijing 100191, China
2
Scientific Computing Department, Science and Technology Facilities Council (STFC), Daresbury Laboratory
, Warrington WA4 4AD, United Kingdom
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Lipeng Lu (陆利蓬);
Lipeng Lu (陆利蓬)
1
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University
, Beijing 100191, China
3
Collaborative Innovation Center of Advanced Aero-Engine
, Beijing 100191, China
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Jian Fang (方剑)
;
Jian Fang (方剑)
2
Scientific Computing Department, Science and Technology Facilities Council (STFC), Daresbury Laboratory
, Warrington WA4 4AD, United Kingdom
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Charles Moulinec;
Charles Moulinec
2
Scientific Computing Department, Science and Technology Facilities Council (STFC), Daresbury Laboratory
, Warrington WA4 4AD, United Kingdom
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David R. Emerson
;
David R. Emerson
2
Scientific Computing Department, Science and Technology Facilities Council (STFC), Daresbury Laboratory
, Warrington WA4 4AD, United Kingdom
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Yufeng Yao (姚宇峰)
Yufeng Yao (姚宇峰)
4
Faculty of Environment and Technology, Department of Engineering Design and Mathematics, University of the West of England
, Bristol BS16 1QY, United Kingdom
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Lipeng Lu (陆利蓬)
1,3
Charles Moulinec
2
David R. Emerson
2
Yufeng Yao (姚宇峰)
4
1
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University
, Beijing 100191, China
2
Scientific Computing Department, Science and Technology Facilities Council (STFC), Daresbury Laboratory
, Warrington WA4 4AD, United Kingdom
3
Collaborative Innovation Center of Advanced Aero-Engine
, Beijing 100191, China
4
Faculty of Environment and Technology, Department of Engineering Design and Mathematics, University of the West of England
, Bristol BS16 1QY, United Kingdom
Physics of Fluids 31, 015101 (2019)
Article history
Received:
September 12 2018
Accepted:
December 06 2018
Citation
Weidan Ni, Lipeng Lu, Jian Fang, Charles Moulinec, David R. Emerson, Yufeng Yao; Flow separation control over a rounded ramp with spanwise alternating wall actuation. Physics of Fluids 1 January 2019; 31 (1): 015101. https://doi.org/10.1063/1.5055948
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