A General Theory of Flow-Instability Inception in Turbomachinery
Author:
Affiliation:
1. School of Jet Propulsion, Beihang University, 100191 Beijing, People’s Republic of China
2. Compressor Department, Shenyang Aeroengine Research Institute, 110015 Liaoning, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052186
Reference42 articles.
1. Surge and Rotating Stall in Axial Flow Compressors—Part I: Theoretical Compression System Model
2. Rotating Waves as a Stall inception Indication in Axial Compressors
3. Stall Inception in Axial Compressors
4. Stall Inception in Axial Flow Compressors
5. 1997 Best Paper Award—Turbomachinery Committee: A Study of Spike and Modal Stall Phenomena in a Low-Speed Axial Compressor
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