On the aero acoustic and internal flows structure in a centrifugal compressor with hub side cavity operating at off design condition-Reference-Cited by-同舟云学术

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On the aero acoustic and internal flows structure in a centrifugal compressor with hub side cavity operating at off design condition

Published:2017-01 Issue: Volume:60 Page:68-83
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Shahin Ibrahim,Alqaradawi Mohamed,Gadala Mohamed,Badr Osama

Funder

Qatar National Research Fund

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference57 articles.

1. Regulations for community noise;Gottlob;Noise News Int.,1995

2. Aeroacoustic phenomena in high-pressure centrifugal compressors—a possible root cause for impeller failures;König,2009

3. Rotating stall and surge;Stenning;J. Fluids Eng.,1980

4. Compressor surge and stall propagation;Emmons;Trans. Am. Soc. Mech. Eng.,1955

5. Coordinates for a High Performance 4:1 Pressure Ratio Centrifugal Compressor;McKain,1997

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