Aerodynamic characterization of a transonic axial flow compressor stage – with asymmetric tip clearance effects
Author:
Funder
Aeronautical Research and Development Board
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference26 articles.
1. Stall inception in axial flow compressors;Day;J. Turbomach.,1993
2. A study of spike and modal stall inception in a low-speed axial compressor;Camp;J. Turbomach.,1998
3. Unsteady Disturbance Structures in Axial Flow Compressor;Park,1994
4. Role of blade passage flow structures in axial compressor rotating stall inception;Hoying;J. Turbomach.,1999
5. The role of tip leakage vortex breakdown in compressor rotor aerodynamics;Furukawa;J. Turbomach.,1999
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