Numerical and Experimental Study of Rotating Stall in an Axial Compressor Stage
Author:
Affiliation:
1. Swiss Federal Institute of Technology, 8092 Zurich, Switzerland
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1106
Reference30 articles.
1. A Simple Model for Compressor Stall Cell Propagation
2. A Review of Non-Steady Flow Models for Compressor Stability
3. A Computational Model for Short-Wavelength Stall Inception and Development in Multistage Compressors
4. Computation of flow around wings based on the Euler equations
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