Numerical investigation on short length-scale disturbance generation in an eccentric axial compressor rotor at a stable condition
Author:
Funder
Nanjing University of Aeronautics and Astronautics
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference37 articles.
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2. A study of spike and modal stall phenomena in a low-speed axial compressor;Camp;J. Turbomach.,1998
3. Stall cell development in an axial compressor;Jackson;J. Turbomach.,1987
4. Modelling of multiple short-length-scale stall cells in an axial compressor using evolved GMDH neural networks;Amanifard;Energy Convers. Manag.,2008
5. Stall inception in axial flow compressors;Day;J. Turbomach.,1993
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