Fluid Redistribution in the Turbulent Boundary Layer Under the Microramp Control

被引:8
|
作者
Wang, B. [1 ]
Liu, W. D. [1 ]
Sun, M. B. [1 ]
Zhao, Y. X. [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
LARGE-EDDY SIMULATION; VORTEX GENERATORS; MODEL; WAKE; LES;
D O I
10.2514/1.J054074
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Recent studies on boundary-layer control with microvortex generators suggest that the microramp should not be simply treated as a traditional streamwise vortex-inducing device. Here, the wake organization downstream of the microramp and its function of fluid redistribution are investigated with a large-eddy simulation at Mach 2.7. It is confirmed by passive scalar convection and streamline tracing that the fluid composing the wake is basically collected from a thin layer close to the wall, particularly beneath 20% of the boundary-layer thickness here, which is responsible for the momentum deficit and low-density features of the wake, as well as the later complex wake evolution. Thus, the microramp has actually worked as a novel near-wall fluid collector, depriving the inner part of the incoming boundary layer, and assembles it into the wake. When developing downstream, the shear induced Kelvin-Helmholtz vortex grows and pairs quickly upon the wake, giving birth to a train of large-scale hairpin vortices with a typical frequency of St = 0.57. The similarity between the local density and passive scalar distribution patterns suggests the advection of the collected low-momentum fluid along with the large-scale vortices is the main reason for the intermittent wake structures presented in the previous studies.
引用
收藏
页码:3777 / 3787
页数:11
相关论文
共 50 条
  • [21] Effect of hydrophobicity on turbulent boundary layer under water
    Hu Haibao
    Du Peng
    Zhou Feng
    Song Dong
    Wu Yang
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2015, 60 : 148 - 156
  • [22] A SUBLAYER THEORY FOR FLUID INJECTION INTO THE INCOMPRESSIBLE TURBULENT BOUNDARY LAYER
    TURCOTTE, DL
    JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (09): : 675 - +
  • [23] CALCULATION OF PRESSURE FLUCTUATIONS UNDER A TURBULENT BOUNDARY LAYER
    PANTON, RL
    LINEBARG.JH
    BULLETIN OF THE AMERICAN PHYSICAL SOCIETY, 1971, 16 (11): : 1331 - &
  • [24] 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
  • [25] 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
  • [26] 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
  • [27] Turbulent boundary layer control with DBD plasma actuators
    LI, Yueqiang
    Wu, Bin
    Gao, Chao
    Zheng, Haibo
    Wang, Yushuai
    Yan, Rihua
    PLASMA SCIENCE & TECHNOLOGY, 2023, 25 (04)
  • [28] Pulsed jet control of the turbulent boundary layer separation
    Béra, JC
    Comte-Bellot, G
    Sunyach, M
    COMPTES RENDUS DE L ACADEMIE DES SCIENCES SERIE II FASCICULE B-MECANIQUE PHYSIQUE ASTRONOMIE, 1998, 326 (12): : 859 - 865
  • [29] An integrated MEMS system for turbulent boundary layer control
    Tsao, T
    Jiang, FK
    Miller, R
    Tai, YC
    Gupta, B
    Goodman, R
    Tung, S
    Ho, CM
    TRANSDUCERS 97 - 1997 INTERNATIONAL CONFERENCE ON SOLID-STATE SENSORS AND ACTUATORS, DIGEST OF TECHNICAL PAPERS, VOLS 1 AND 2, 1997, : 315 - 318
  • [30] 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, 25 (04) : 207 - 217