An experimental study on flow separation control of hydrofoils with leading-edge tubercles at low Reynolds number

被引:117
|
作者
Wei, Zhaoyu [1 ]
New, T. H. [1 ]
Cui, Y. D. [2 ]
机构
[1] Nanyang Technol Univ, Sch Mech & Aerosp Engn, Singapore 639798, Singapore
[2] Natl Univ Singapore, Temasek Labs, Singapore 117411, Singapore
关键词
Hydrofoil; Passive flow control; Leading-edge tubercles; Flow visualization; Particle-image velocimetry; NACA634-021; BOUNDARY-LAYER; AIRFOIL; SURFACE; BEHAVIOR;
D O I
10.1016/j.oceaneng.2015.08.004
中图分类号
U6 [水路运输]; P75 [海洋工程];
学科分类号
0814 ; 081505 ; 0824 ; 082401 ;
摘要
Hydrodynamic characteristics of hydrofoils with leading-edge tubercles were experimentally investigated in a water tunnel at a Reynolds number of Re=1.4 x 10(4). Particle image velocimetry measurements and particle-streak visualizations reveal that the tubercles improve flow separation behaviour. In particular, hydrofoils with larger wave amplitudes and smaller wavelengths tend to perform significantly better in flow separation control. Cross-stream flow measurements indicate that streamwise counter-rotating vortex pairs are generated over the tubercles and mitigate flow separation. Analysis confirms. that the tubercles function as vortex generators, due to their comparable heights relative to the boundary layer thickness. The vortex pairs meander and interact with adjacent flows, causing the flow separation behaviour to be occasionally unstable, thus leading to variable flow separation region sizes. This suggests that measures may have to be taken to ensure the stability of the counter-rotating vortex pairs for more persistent and predictable improvements. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:336 / 349
页数:14
相关论文
共 50 条
  • [1] Experimental and numerical study of laminar separation bubble formation on low Reynolds number airfoil with leading-edge tubercles
    B. K. Sreejith
    A. Sathyabhama
    Journal of the Brazilian Society of Mechanical Sciences and Engineering, 2020, 42
  • [2] Experimental and numerical study of laminar separation bubble formation on low Reynolds number airfoil with leading-edge tubercles
    Sreejith, B. K.
    Sathyabhama, A.
    JOURNAL OF THE BRAZILIAN SOCIETY OF MECHANICAL SCIENCES AND ENGINEERING, 2020, 42 (04)
  • [3] Numerical and experimental study on flow separation control of airfoils with various leading-edge tubercles
    Fan, Menghao
    Dong, Xiangwei
    Li, Zengliang
    Sun, Zhaocheng
    Feng, Long
    OCEAN ENGINEERING, 2022, 252
  • [4] Leading-edge tubercles delay flow separation for a tapered swept-back wing at very low Reynolds number
    Wei, Zhaoyu
    New, T. H.
    Lian, Lian
    Zhang, Yanni
    OCEAN ENGINEERING, 2019, 181 : 173 - 184
  • [5] Effect of leading-edge tubercles on the flow over low-aspect-ratio wings at low Reynolds number
    Yang, Pengxin
    Zhu, Yichen
    Wang, Jinjun
    THEORETICAL AND APPLIED MECHANICS LETTERS, 2023, 13 (01)
  • [6] Numerical study of the evolution of unsteady cavitation flow around hydrofoils with leading-edge tubercles
    Fan, Menghao
    Sun, Zhaocheng
    Yu, Ran
    Li, Zengliang
    JOURNAL OF APPLIED PHYSICS, 2024, 135 (04)
  • [7] Effect of leading-edge tubercles on the flow over low-aspect-ratio wings at low Reynolds number
    Pengxin Yang
    Yichen Zhu
    Jinjun Wang
    Theoretical & Applied Mechanics Letters, 2023, 13 (01) : 41 - 49
  • [8] Prediction of leading-edge sheet cavitation inception on hydrofoils at low to moderate reynolds number flows
    Rusak, Zvi
    Morris, Wallace J., II
    Peles, Yoav
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2007, 129 (12): : 1540 - 1546
  • [9] Leading-Edge Suction Parameter in Turbulent Flow at a Low Reynolds Number
    Kay, Nicholas J.
    Richards, Peter J.
    Sharma, Rajnish N.
    AIAA JOURNAL, 2022, 60 (02) : 798 - 808
  • [10] LEADING-EDGE SEPARATION FROM A BLUNT PLATE AT LOW REYNOLDS-NUMBER
    LANE, JC
    LOEHRKE, RI
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 1980, 102 (04): : 494 - 496