Numerical Investigation of Rotating Instability Development in a Wide Tip Gap Centrifugal Compressor
Author:
Affiliation:
1. Liebherr-Aerospace Toulouse SAS, 408 Avenue des Etats Unis, 31016 Toulouse, France
2. ISAE-SUPAERO, 10 Av. Edouard Belin, 31400 Toulouse, France
Abstract
Funder
Liebherr-Aerospace Toulouse S.A.S
Publisher
MDPI AG
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering
Link
https://www.mdpi.com/2504-186X/8/3/25/pdf
Reference22 articles.
1. Structure of Tip Clearance Flow in an Isolated Axial Compressor Rotor;Inoue;J. Turbomach.,1989
2. Detection of a Rotating Stall Precursor in Isolated Axial Flow Compressor Rotors;Inoue;J. Turbomach.,1991
3. Propagation of Multiple Short-Length-Scale Stall Cells in an Axial Compressor Rotor;Inoue;J. Turbomach.,1999
4. Comparative Studies on Short and Long Length-Scale Stall Cell Propagating in an Axial Compressor Rotor;Inoue;J. Turbomach.,2000
5. An Experimental and Numerical Investigation into the Mechanisms of Rotating Instability;Hah;J. Turbomach.,2002
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1. Numerical Investigation of Rotating Instability Development in a Wide Tip Gap Centrifugal Compressor;International Journal of Turbomachinery, Propulsion and Power;2023-08-01
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