Effect of Self-Recirculation-Casing Treatment on High Pressure Ratio Centrifugal Compressor-Reference-Cited by-同舟云学术

Effect of Self-Recirculation-Casing Treatment on High Pressure Ratio Centrifugal Compressor

Published:2016-05 Issue:3 Volume:32 Page:602-610
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Yang Mingyang¹,Martinez-Botas Ricardo²,Zhang Yangjun³,Zheng Xinqian³

Affiliation:

1. Shanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China

2. Imperial College, London, England, SW7 2AZ, United Kingdom

3. Tsinghua University, 100084 Beijing, People’s Republic of 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.B35438

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4. Flow Analysis in a Transonic Centrifugal Compressor Rotor Using 3-Component Laser Velocimetry

5. HamidR. H.XuL. P. “Role of Tip Leakage in Stall of Transonic Centrifugal Compressor,” American Soc. of Mechanical Engineers Paper GT2009-59327, Fairfield, NJ, 2009.

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