The Helical- Blade- Vertical- Axis- Wind- Turbine (3-HB-VAWT) has a relatively uniform variation of generated power with its tip speed ratio (TSR) due to its special blade structure. Its required lower self-starting torque also justifies its application in low wind speed areas. By obtaining 3-D CFD (Computational Fluid Dynamic) results and by the use of these data as inputs to the Response Surface Method (RSM), the design/optimization of helical blade VAWT is performed for the first time in this research. As 3-D CFD simulations were very time consuming, RSM was applied due its smaller required number of CFD runs. Furthermore, an important feature of RSM is the ability to perform optimization in all possible points of decision variables in the allowed interval, which is a great advantage for this method. The objective-function ( C p − a v e ) and decision variables (blade- airfoil- chord, the angle- of- helix, and the blade- tip speed- ratio) after extensive 3-D CFD runs finally were selected. At the optimum point, 0.45 m, 30 ∘ , and 1.41 were obtained for turbine- blade- chord, angle- of- helix, and tip- speed- ratio, respectively. Also, at the optimum point, the objective-function ( C p − a v e ) was obtained 0.182, which showed 212% improvement in comparison with the ( C p − a v e ) max = 0.058 for the referenced turbine with TSR=1.77. Finally, 0.55% difference between the average-power-coefficients predicted by the response surface method and the 3-D CFD confirming test showed the proper procedure of estimation the VAWT power coefficient with assumption of three rigid helical blades.
Sanaye et al. (Sun,) studied this question.