Closed-loop plasma flow control of a turbulent cylinder wake flow using machine learning at Reynolds number of 28 000

被引:35
作者
Chen, Jie [1 ]
Zong, Haohua [2 ]
Song, Huimin [1 ]
Wu, Yun [2 ]
Liang, Hua [2 ]
Su, Zhi [1 ]
机构
[1] Air Force Engn Univ, Natl Key Lab Aerosp Power Syst & Plasma Technol, Xian 710038, Peoples R China
[2] Xi An Jiao Tong Univ, Sch Mech Engn, Inst Aeroengine, Xian 710049, Peoples R China
基金
中国国家自然科学基金;
关键词
WAVE/BOUNDARY LAYER INTERACTION; CONTROL STRATEGIES; CIRCULAR-CYLINDER; FEEDBACK-CONTROL; OPTIMIZATION; ACTUATORS; MICROJETS;
D O I
10.1063/5.0186524
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Machine learning is increasingly used for active flow control. In this experimental study, alternating-current dielectric barrier discharge plasma actuators are deployed for the closed-loop intelligent control of the flow around a cylinder at a Reynolds number of 28 000 based on the velocity feedback from two hot-wire sensors placed in the wake. Variations in the cylinder drag are monitored by a load cell, and the temporal response of the wake flow field is visualized by a high-speed particle image velocimetry system working at 1 kHz. The high-speed control law is operated using a field programmable gate array optimized by genetic programing (GP). The results show that the peak drag reduction achieved by machine learning is of similar magnitude to that of conventional steady actuation (similar to 15%), while the power saving ratio is 35% higher than with conventional techniques because of the reduced power consumption. Analysis of the best GP control laws shows that the intensity of plasma actuation should be kept at a medium level to maximize the power-saving ratio. When compared with the baseline uncontrolled flow, the best controlled cases constrain the meandering motion of the cylinder wake, resulting in a narrow stabilized velocity deficit zone in the time-averaged sense. According to the results of proper orthogonal decomposition and dynamic mode decomposition, Karman vortex shedding is promoted under the best GP control.
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页数:17
相关论文
共 53 条
[1]   Experimental study on response of hot wire and cylindrical hot film anemometers operating under varying fluid temperatures [J].
Ardekani, M. A. ;
Farhani, F. .
FLOW MEASUREMENT AND INSTRUMENTATION, 2009, 20 (4-5) :174-179
[2]   Identification-Based Closed-Loop Control Strategies for a Cylinder Wake Flow [J].
Atam, Ercan ;
Mathelin, Lionel ;
Cordier, Laurent .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2017, 25 (04) :1488-1495
[3]   ON STREAMWISE VORTICES IN TURBULENT WAKES OF CYLINDERS [J].
BAYSMUCHMORE, B ;
AHMED, A .
PHYSICS OF FLUIDS A-FLUID DYNAMICS, 1993, 5 (02) :387-392
[4]   THE TRANSITION TO TURBULENCE IN THE WAKE OF A CIRCULAR CYLINDER [J].
BLOOR, MS .
JOURNAL OF FLUID MECHANICS, 1964, 19 (02) :290-&
[5]   Machine Learning for Fluid Mechanics [J].
Brunton, Steven L. ;
Noack, Bernd R. ;
Koumoutsakos, Petros .
ANNUAL REVIEW OF FLUID MECHANICS, VOL 52, 2020, 52 :477-508
[6]   Closed-Loop Turbulence Control: Progress and Challenges [J].
Brunton, Steven L. ;
Noack, Bernd R. .
APPLIED MECHANICS REVIEWS, 2015, 67 (05)
[7]   Variants of Dynamic Mode Decomposition: Boundary Condition, Koopman, and Fourier Analyses [J].
Chen, Kevin K. ;
Tu, Jonathan H. ;
Rowley, Clarence W. .
JOURNAL OF NONLINEAR SCIENCE, 2012, 22 (06) :887-915
[8]   Issues in active flow control: theory, control, simulation, and experiment [J].
Collis, SS ;
Joslin, RD ;
Seifert, A ;
Theofilis, V .
PROGRESS IN AEROSPACE SCIENCES, 2004, 40 (4-5) :237-289
[9]   SDBD plasma enhanced aerodynamics: concepts, optimization and applications [J].
Corke, Thomas C. ;
Post, Martiqua L. ;
Orlov, Dmitry M. .
PROGRESS IN AEROSPACE SCIENCES, 2007, 43 (7-8) :193-217
[10]  
Corke TC, 2011, PHILOS T R SOC A, V369, P1459, DOI [10.1098/rsta.2010.0356, 10.1098/rsta.2010.0350]