March 2013
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4 Reads
The Proceedings of Conference of Kanto Branch
Wind turbines with a propeller-type rotor on a horizontal axis employ turbine blades have a thickness ratio δ(the ratio of chord length C against maximum thickness T), which is small at the blade tip (thin blade), and is large at the blade root (thick blade). In this study, we focused on the effects of vortex generator on allowing a significant expansion of the operable range to a higher angle of attack that causes a stall. And the flow visualization and velocity distribution around the airfoil were measured and compared with without of vortex generator. This paper examines in detail around the blades affects flow separation from the blade surface and aerodvnamic characteristics associated with stalls.