Author(s)

Sundaravadivel Arumugam¹, Nadaraja Pillai Subramania², Senthilkumar Chidambaram¹

¹Department of Aerospace Engineering, Madras Institute of Technology, Anna University, Chennai, India.
²School of Mechanical Engineering, SASTRA University, Thanjavur, India.

Even though wind energy is a deep-rooted technology, but not yet mature and hence there are bounteous scopes for improvement to reduce the cost of wind energy. An experimental investigation has been carried out on 1:25 scaled S809 aerofoil blade featuring boundary layer fence at various span wise location. Quantifying electrical power obtained by rotation of wind turbine rotor coupled with dynamic testing system. A baseline model with no flow control and an upgraded model with detachable boundary layer fence have been studied in the wind tunnel. For upgraded model, fences were placed along the location of 40% to 90% of the blade span. The rotor blades are then tested dynamically in wind tunnel at open terrain condition for 7 m/s, 9 m/s and 11 m/s velocities. In order to study the effect of boundary layer fence test has been carried out in the low speed wind tunnel having test section of size 0.9 m × 1.2 m × 2 m. Scope corder DL 750 is used to measure time varying voltage and proximity sensor with its compatible display unit is used to measure the rotor RPM. The flow behaviour was found to be considerably favourable from conventional rotor blades. Installation of fence has been found promising for increased energy extraction from air column by controlling the three dimensional span wise flow. Results demonstrate the potential of the proposed model which can obtain a maximum of about 11.8% increase in the power. In addition, the significance of the location of wing fence and blade pitch angle has been analysed.

HAWT, S809 Airfoil, Boundary Layer Fence, Wind Tunnel Testing

Arumugam, S. , Subramania, N. and Chidambaram, S. (2016) Effect of Boundary Layer Fence Location on HAWT Power Performance. Circuits and Systems, 7, 1177-1189. doi: 10.4236/cs.2016.78101.