Some Effects of Guide-vane Turning and Stators on the Rotating Stall Characteristics of a High Hub-tip Ratio Single-stage Compressor


Book Description

The rotating stall characteristics of several guide-vane - rotor and guide-vane - rotor - stator configurations were investigated. Guide vanes having turning angles of -22.5, 0 , 22.5, and 40 degrees were used. The stage hub-tip ratio was 0.9.