抄録
The purpose of the present research is to suppress cavitation instabilities by using a circumferential groove. The circumferential
groove was designed based on CFD so that the tip leakage vortex is trapped by the groove and does not interact
with the next blade. Experimental results show that the groove can suppress rotating cavitation, asymmetric cavitation and
cavitation surge. However, weak instabilities with higher frequency occurred in a wide range of cavitation number. From
the analysis of pressure pattern similar to that for rotor-stator interaction, it was found that the higher frequency components
are caused by the interaction of backflow vortices with the inducer blades.
