Computational evaluation of an optimum leading-edge slat deflection angle for dynamic stall control in a novel urban-scale vertical axis wind turbine for low wind speed operation

被引:41
|
作者
Ullah, Tariq [1 ]
Javed, Adeel [1 ]
Abdullah, Ali [1 ]
Ali, Majid [1 ]
Uddin, Emad [2 ]
机构
[1] Natl Univ Sci & Technol NUST, US Pakistan Ctr Adv Studies Energy USPCAS E, Dept Thermal Energy Engn, Islamabad, Pakistan
[2] Natl Univ Sci & Technol NUST, Sch Mech & Mfg Engn SMME, Dept Mech Engn, Islamabad, Pakistan
关键词
Vertical axis wind turbine; Dynamic stall; Passive flow control; Leading-edge slat; Computational fluid dynamics; AERODYNAMIC PERFORMANCE; SEPARATION CONTROL; FLOW SEPARATION; DOMAIN SIZE; AIRFOIL; SIMULATION; GUIDELINES; AEROFOIL;
D O I
10.1016/j.seta.2020.100748
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
This paper explores passive flow control via leading-edge (LE) slats to reduce the dynamic stall (DS) phenomenon and related blade-wake interaction in an H-Darrieus type vertical axis wind turbine (VAWT) operating under low wind speed conditions. A comprehensive 2D unsteady computational fluid dynamics (CFD) assessment has been carried out for the non-slatted baseline rotor and the advance slatted rotor (ASR) configurations. The unsteady Reynolds-averaged Navier-Stokes (URANS) approach with k-omega shear stress transport (SST) turbulence model and sliding mesh technique have been applied in Ansys Fluent. Optimum slat deflection angle delta has been evaluated using the single-blade oscillatory case with and without the LE slats. Results indicate a reduction in optimum delta from 16 degrees at rated wind speed of 10 ms(-1) to 12 degrees for low wind speed operation at 5 ms(-1). A significant increase in the maximum coefficient of lift C-L,C-max by approximately 32% and a delay in stall angle of attack alpha(max) by 3 degrees is obtained with ASR configuration compared to the baseline. Further assessment of the ASR configuration on the three-blade rotatory case demonstrates an increase in the power coefficient C-P by approximately 15% at the rated tip-speed ratio. compared to the baseline.
引用
收藏
页数:12
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