Predetermined control of turbulent boundary layer with a piezoelectric oscillator

被引:0
|
作者
郑小波 [1 ]
姜楠 [1 ,2 ]
张浩 [1 ]
机构
[1] Department of Mechanics Tianjin University
[2] Tianjin Key Laboratory of Modern Engineering Mechanics
基金
中国国家自然科学基金;
关键词
turbulent boundary layer; predetermined control; drag reduction; piezoelectric oscillator;
D O I
暂无
中图分类号
O357.5 [湍流(紊流)];
学科分类号
080103 ; 080704 ;
摘要
With a piezoelectric(PZT) oscillator, the predetermined controls of the turbulent boundary layer(TBL) are effective in reducing the drag force. The stream-wise velocities in the TBL are accurately measured downstream of the oscillator driven by an adjustable power source. The mean velocity profiles in the inner and outer scales are reported and the skin friction stresses with different voltage parameters are compared. Reduction of integral spatial scales in the inner region below y+of 30 suggests that the oscillator at work breaks up the near-wall stream-wise vortices responsible for high skin friction. For the TBL at Reθof 2183, the controls with a frequency of 160 Hz are superior among our experiments and a relative drag reduction rate of 26.83% is exciting. Wavelet analyses provide a reason why the controls with this special frequency perform best.
引用
收藏
页码:673 / 677
页数:5
相关论文
共 50 条
  • [1] Predetermined control of turbulent boundary layer with a piezoelectric oscillator
    Zheng, Xiao-Bo
    Jiang, Nan
    Zhang, Hao
    CHINESE PHYSICS B, 2016, 25 (01)
  • [2] Active control of turbulent boundary layer based on a single piezoelectric oscillator
    Zhang H.
    Zheng X.
    Jiang N.
    Jiang, Nan (nanj@tju.edu.cn), 1600, Chinese Society of Theoretical and Applied Mechanics (48): : 536 - 544
  • [3] Turbulent boundary layer control by wall oscillations
    Zhou, Dongmei
    Ball, Kenneth S.
    PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER CONFERENCE - 2005, VOL 1, PTS A AND B, 2005, : 223 - 238
  • [5] System identification and control of a turbulent boundary layer
    Rathnasingham, R
    Breuer, KS
    PHYSICS OF FLUIDS, 1997, 9 (07) : 1867 - 1869
  • [6] Normal shock wave/turbulent boundary-layer interaction control using 'smart' piezoelectric actuators
    Couldrick, JS
    Gai, SL
    Milthorpe, JF
    Shankar, K
    AERONAUTICAL JOURNAL, 2005, 109 (1101): : 577 - 583
  • [7] A comparison of opposition control in turbulent boundary layer and turbulent channel flow
    Stroh, A.
    Frohnapfel, B.
    Schlatter, P.
    Hasegawa, Y.
    PHYSICS OF FLUIDS, 2015, 27 (07)
  • [8] Turbulent boundary layer control with DBD plasma actuators
    李跃强
    武斌
    高超
    郑海波
    王玉帅
    严日华
    Plasma Science and Technology, 2023, (04) : 207 - 217
  • [9] Turbulent boundary-layer control with plasma actuators
    Choi, Kwing-So
    Jukes, Timothy
    Whalley, Richard
    PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2011, 369 (1940): : 1443 - 1458
  • [10] Mechanisms and models of control of turbulent transfer in boundary layer
    Vladislav, Kovalnogov N.
    Ruslan, Fedorov, V
    Igor, Maleshin A.
    Dmitry, Suranov, V
    Larisa, Khakhaleva, V
    PROCEEDINGS OF THE INTERNATIONAL CONFERENCE ACTUAL ISSUES OF MECHANICAL ENGINEERING 2017 (AIME 2017), 2017, 133 : 357 - 362