Design and Testing of a LUT Airfoil for Straight-Bladed Vertical Axis Wind Turbines

• Main Authors: Shoutu Li, Ye Li, Congxin Yang, Xuyao Zhang, Qing Wang, Deshun Li, Wei Zhong, Tongguang Wang
• Format: Article
• Language: English
• Published: MDPI AG 2018-11-01
• Series: Applied Sciences
• Subjects: airfoil design; aerodynamic; wind tunnel experiment; VAWTs (Vertical axis wind turbines)
• Online Access: https://www.mdpi.com/2076-3417/8/11/2266

The airfoil plays an important role in improving the performance of wind turbines. However, there is less research dedicated to the airfoils for Vertical Axis Wind Turbines (VAWTs) compared to the research on Horizontal Axis Wind Turbines (HAWTs). With the objective of maximizing the aerodynamic performance of the airfoil by optimizing its geometrical parameters and by considering the law of motion of VAWTs, a new airfoil, designated the LUT airfoil (Lanzhou University of Technology), was designed for lift-driven VAWTs by employing the sequential quadratic programming optimization method. Afterwards, the pressure on the surface of the airfoil and the flow velocity were measured in steady conditions by employing wind tunnel experiments and particle image velocimetry technology. Then, the distribution of the pressure coefficient and aerodynamic loads were analyzed for the LUT airfoil under free transition. The results show that the LUT airfoil has a moderate thickness (20.77%) and moderate camber (1.11%). Moreover, compared to the airfoils commonly used for VAWTs, the LUT airfoil, with a wide drag bucket and gentle stall performance, achieves a higher maximum lift coefficient and lift⁻drag ratios at the Reynolds numbers 3 × 10⁵ and 5 × 10⁵.