Tip leakage flow has become one of the major triggers for rotating stall in tip region of high loading transonic compres......

The stable range of the gas engine compressors is reduced due to per stage maximum loading. The performance of the engin......

This paper considers effects of Rotating Inlet Distortion (RID) on a two-stage axial com-pressor and the stabilization e......

The mechanism of compressor stall margin enhancement using the tip air injection is explored. The transonic compressor, ......