An improved prediction model for corner stall in axial compressors with dihedral effect
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference21 articles.
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2. Experimental investigations of the three-dimensional flow in an annular compressor cascade;Schulz;J Turbomach,1988
3. Development of hub corner stall and its influence on the performance of axial compressor blade row;Hah;J Turbomach,1999
4. Three-dimensional separations in axial compressors;Gbadebo;J Turbomach,2005
5. Variation of vortex structure in a compressor cascade at different incidences;Zhang;J Propul Power,2007
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