Flow Stability Model of Centrifugal Compressors Based on Eigenvalue Approach
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. Civil Aviation Administration of China, 100102 Beijing, 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.J054350
Reference45 articles.
1. Active stabilization of compressor surge
2. Computational Analysis of Centrifugal Compressor Surge Control Using Air Injection
3. Impeller Stalling as Influenced by Diffusion Limitations
4. A Distinction Between Different Types of Stall in a Centrifugal Compressor Stage
5. Application of Aerodynamically Induced Prewhirl to a Small Turbocharger Compressor
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