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Improved High Pressure Ratio Centrifugal Compressor

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  • Institut Für Antriebstechnik

Abstract

The paper describes the development and the experimental as well as theoretical investigation of a new transonic, high specific speed centrifugal compressor rotor of 6.2:1 pressure ratio. Performance measurement results, laser measurements and calculated 3D results are shown for the new rotor and are compared with the corresponding data of a same type predecessor rotor.

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