Abstract
The purposeof this study is to examine the aerodynamic correlation between separation bubble on a blade and wake of stator blade. Test model used is a flat plate with the semicircular leading edge, in consideration of the generation of the separation bubble. In this experiment the position of the stationary bar, which imitates upstream stator blade, was changed. Measuring instrument was hot-wire measurement system. This investigation shows that the present method has a possibility to effectively reduce loss associated with separation bubble.
