Abstract:
In this study, a 2 kW small scale horizontal axis wind turbine with a rotor radius of 1.8 m and a Tip
Speed Ratio (λ) of 6 was designed to work at low wind speed for rural applications. Aerodynamic analysis
was performed on 10 airfoils, viz Aquila, BW-3, E387, FX63-137, NACA0012, NASA LS-0413, RG-15, S1223,
SD7080 and SG6043 using QBlade software. These airfoils were used to analyze lift coefficient (CL) and lift
to drag ratio (CL/CD), with different angles of attack (α) and compared with one another. From the analyzed
results, SD7080 airfoil was found to be the best due to its wide and maximum lift to drag ratio of 46.30 for
the angle of attack (α) of 5o and comparatively high power production at low wind speed operation. It
showed a high soft stall behaviour in the α range of 4-9o. The blades were specifically designed for various
airfoils by applying Blade Element Momentum Theory (BEMT). The power coefficient (Cp) of the selected
airfoils varied according to the values of tip speed ratio (λ). From the results, it was detected that the
SD7080 airfoil blade has an optimum power coefficient of Cp = 0.34, at λ = 6 for Reynolds number
(Re) = 81712. SD7080 airfoil blade was analysed for different Re values of 30642, 40856, 51070, 61284,
71498 and 81712 in comparison with tip speed ratio and power coefficient. A considerably high power
coefficient of 0.29 was produced when Re as low as 40856 at λ = 6. Therefore, from the numerical
simulation, it was found that SD7080 was the most suitable airfoil to start producing considerably high
power under low wind speed applications.
