Influence of Tip Clearance on the Flow Field and Aerodynamic Performance of the Centrifugal Impeller

Author:

GAO Li-min,XI Guang,WANG Shang-jin

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference7 articles.

1. Performance characteristics of shrouded and unshrouded impeller of a centrifugal compressor[J];Harada;ASME J of Engineering for Gas Turbine and Power,1985

2. Shun K, Hirsch C. Influences of tip leakage flow in centrifugal compressor [A]. In: 3rd International Symposium on Aerothermodynamics of Internal Flow[C]. Beijing, 1996.

3. The geometry data and the secondary vortex in the Krain's centrifugal impeller[J];Xi;J of Engineering Thermophysics,2000

4. Hathaway M D, Chriss R M, Wood J R, et al. Laser anemometer measurements of the three-dimensional rotor flow field in the NASA low-speed centrifugal compressor [R]. NASA TP-3527, 1995.

5. Experimental and computational investigation of the NASA Low-Speed centrifugal compressor flow field[J];Hathaway;ASME J of Turbomachinery,1993

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