In turbine stages, there are a lot of vortices which can cause energy loss. The tip leakage vortex is one of these vortices, and it can lead to great energy loss in a turbine rotor passage. Many researchers have investigated various tip leakage control methods. In the present study, jet injection from the tip platform of a rotor blade is investigated as a promising control method of tip leakage.
... [Show full abstract] This method has the possibility that tip leakage loss is decreased even if relatively large tip clearance is applied. Three-dimensional turbulent flow field near the blade tip is numerically simulated varying the injection hole position to find out the optimum position to decrease tip leakage loss. The computed flow field, the mass flow rate of tip leakage flow and the total pressure at downstream of the blade are investigated, and it is found that the tip injection hole located at mid-chord can effectively suppress tip leakage loss.