Passive control of boundary layer flow separation on a wind turbine airfoil using vortex generators and slot

被引:4
|
作者
Nia, Bahador Bakhtiari [1 ]
Ja'fari, Mohammad [1 ]
Ranjbar, Adel Rezaei [2 ]
Jaworski, Artur J. [1 ]
机构
[1] Univ Huddersfield, Sch Comp & Engn, Dept Engn & Technol, Huddersfield HD1 3DH, England
[2] Ferdowsi Univ Mashhad, Dept Mech Engn, Mashhad, Iran
关键词
Boundary layer; Flow separation control; Wind turbine; Vortex generator; Slot treatment; Combined passive flow control; TRAILING-EDGE; BLADE; PERFORMANCE;
D O I
10.1016/j.oceaneng.2023.115170
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
Passive Flow Control (PFC) technique has been established as an effective approach in the mitigation/elimination of flow separation phenomenon to enhance the aerodynamic performance of the wind turbine blades. The paper sheds light on the working mechanism of slot and Vortex Generator (VG) in the transitional boundary layer which has received far less attention from researchers. Also, the idea of the combination of two PFC techniques including the slot and the VG treatments on the wind turbine blade has been tested. The lift to drag coefficient (CL/CD) improves up to 112% at incidence angle of 16.3 degrees using VG in comparison to uncontrolled case; however, this coefficient deteriorates down to 12.3% on average for pre-stall angles. The results revealed that the slot exit jet at the aft portion of chord length (70% C) improves the lift to drag coefficient (CL/CD) by 91% at the post-stall condition, a reduction of aerodynamic characteristics over the airfoil profile is detected for the lower inflow angles. The combined PFC method shows better performance than the slotted profile in terms of lift coefficient in most operating angles, but still has lower values than the controlled case with VG.
引用
收藏
页数:15
相关论文
共 50 条
  • [1] Flow control on the NREL S809 wind turbine airfoil using vortex generators
    Wang, Haipeng
    Zhang, Bo
    Qiu, Qinggang
    Xu, Xiang
    ENERGY, 2017, 118 : 1210 - 1221
  • [2] Airfoil-shaped vortex generators for separation control and drag reduction on wind turbine blades
    Palanivel, Hariprasanth
    Mukherjee, Rinku
    Acta Mechanica, 2024, 235 (12) : 7765 - 7787
  • [3] Controlling dynamic stall using vortex generators on a wind turbine airfoil
    De Tavernier, D.
    Ferreira, C.
    Vire, A.
    LeBlanc, B.
    Bernardy, S.
    RENEWABLE ENERGY, 2021, 172 : 1194 - 1211
  • [4] Controlling dynamic stall using vortex generators on a wind turbine airfoil
    De Tavernier, D.
    Ferreira, C.
    Viré, A.
    LeBlanc, B.
    Bernardy, S.
    Renewable Energy, 2021, 172 : 1194 - 1211
  • [5] Numerical Investigation of Passive Vortex Generators on a Wind Turbine Airfoil Undergoing Pitch Oscillations
    Zhu, Chengyong
    Wang, Tongguang
    Wu, Jianghai
    ENERGIES, 2019, 12 (04)
  • [6] PASSIVE CONTROL OF BOUNDARY LAYER SEPARATION USING SINGLE AND MULTIPLE SLATS ON THE AIRFOIL
    Kumar, Krishanu
    Kumar, Pankaj
    Singh, Santosh Kumar
    INTERNATIONAL JOURNAL OF FLUID MECHANICS RESEARCH, 2021, 48 (02) : 17 - 28
  • [7] Passive Flow Control Application Using Single and Double Vortex Generator on S809 Wind Turbine Airfoil
    Ozden, Mustafa
    Genc, Mustafa Serdar
    Koca, Kemal
    ENERGIES, 2023, 16 (14)
  • [8] Using vortex generators for flow separation control on tidal turbine profiles and blades
    Manolesos, M.
    Chng, L.
    Kaufmann, N.
    Ouro, P.
    Ntouras, D.
    Papadakis, G.
    RENEWABLE ENERGY, 2023, 205 : 1025 - 1039
  • [9] Comparison of flow structures for vane and rod type vortex generators on a wind turbine airfoil
    Tiwari, Nishchay
    Flaszynski, Pawel
    Suresh, Thanushree
    Szulc, Oskar
    INTERNATIONAL JOURNAL OF NUMERICAL METHODS FOR HEAT & FLUID FLOW, 2023, 33 (04) : 1458 - 1474
  • [10] Design optimization of the aerodynamic passive flow control on NACA 4415 airfoil using vortex generators
    Fouatih, Omar Madani
    Medale, Marc
    Imine, Omar
    Imine, Bachir
    EUROPEAN JOURNAL OF MECHANICS B-FLUIDS, 2016, 56 : 82 - 96