URANS analysis of the effect of realistic inlet distortions on the stall inception of a centrifugal compressor
Author:
Publisher
Elsevier BV
Subject
General Engineering,General Computer Science
Reference22 articles.
1. A study of spike and modal stall phenomena in a low-speed axial compressor;Camp;ASME J Turbomach,1998
2. Compressor aerodynamics;Cumpsty,1989
3. Distinction between types of impeller and diffuser rotating stall in centrifugal compressors with vaneless diffuser;Frigne;ASME J Eng Gas Turb Power,1984
4. Prestall behavior of a transonic axial compressor stage via time-accurate numerical simulations;Chen;ASME J Turbomach,2008
5. Vo HD. Role of tip clearance flow on axial compressor stability. Ph.D. thesis, Massachusetts Institute of Technology; 2001.
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