Optimization of Centrifugal Impellers for Uniform Discharge Flow and Wide Operating Range
Author:
Affiliation:
1. Xi’an Jiaotong University, Xi’an, Shaanxi 710049, China
2. Hangyang Turbomachinery Company, Ltd., Hangzhou, Zhejiang 311305, China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34193
Reference25 articles.
1. Cumpsty, N. A., Compressor Aerodynamics, Longman, Essex, England, U.K., 1989.
2. Secondary Flows and Vortex Motion in a High-Efficiency Backswept Impeller at Design and Off-Design Conditions
3. Flow Study of a Redesigned High-Pressure-Ratio Centrifugal Compressor
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