The flow at the stall line of a centrifugal compressor with vaneless diffuser was investigated at different speeds. A distinction between three kinds of stall phenomena could be made. One type of stall with regurgitation of fluid at the impeller inlet was of a nonperiodic character, whereas two different types of periodic stall appeared at higher speeds. The rotating nature of these two types of stall was verified from a comparison of signals of peripherally spaced pressure transducers. The low-frequency rotating stall exhibited features of diffuser generated stall and a lobe number of three was measured. From a detailed investigation of the high-frequency rotating stall, which included unsteady probe measurements upstream and downstream of the impeller, it can be shown that this type of rotating stall is generated in the impeller by a periodic breakdown of energy transfer from the rotor to the flow. This conclusion is supported by the distribution of shroud static pressures.
A Distinction Between Different Types of Stall in a Centrifugal Compressor Stage
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Ka¨mmer, N., and Rautenberg, M. (January 1, 1986). "A Distinction Between Different Types of Stall in a Centrifugal Compressor Stage." ASME. J. Eng. Gas Turbines Power. January 1986; 108(1): 83–92. https://doi.org/10.1115/1.3239890
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