Performance enhancement of a centrifugal compressor stage using profiled end wall (PEW) treatments in the radial vaned diffuser
Author:
Funder
National Science and Technology Major Project
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference42 articles.
1. Experimental investigation of diffuser hub injection to improve centrifugal compressor stability;Skoch;J. Turbomach.,2005
2. Influence of unsteadiness on the control of a hub-corner separation within a radial vaned diffuser;Marsan;J. Turbomach.,2014
3. Spike and modal stall inception in an advanced turbocharger centrifugal compressor;Spakovszky;J. Turbomach.,2009
4. An investigation of the stability enhancement of a centrifugal compressor stage using a porous throat diffuser;Galloway;J. Turbomach.,2018
5. An investigation of stall inception in centrifugal compressor vaned diffuser;Everitt;J. Turbomach.,2012
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