Optimization of Discrete Cavities with Guide Vanes in A Centrifugal Compressor based on A Comparative Analysis of Optimization Techniques-Reference-Cited by-同舟云学术

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Optimization of Discrete Cavities with Guide Vanes in A Centrifugal Compressor based on A Comparative Analysis of Optimization Techniques

Published:2021-01-04 Issue:3 Volume:22 Page:514-530
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Ma Sang-Bum,Roh Min-Su,Kim Kwang-Yong^ORCID

Funder

Korea Institute of Science and Technology Information

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42405-020-00341-z.pdf

Reference42 articles.

1. Yang M, Ricardo MB, Zhang Y (2013) Inlet duct treatment for stability improvement on a high pressure ratio centrifugal compressor. Proc ASME Turbo Expo. https://doi.org/10.1115/GT2013-95189

2. Greitzer EM (1976) Surge and rotating stall in axial flow compressors—Part II: experimental results and comparison with theory. J Eng Power 98(2):199–211

3. Mohtar H, Chesse P, Yammine A, Hetet JF (2008) Variable inlet guide vanes in a turbocharger centrifugal compressor: local and global study. SAE Tech Paper. https://doi.org/10.4271/2008-01-0301

4. Coppinger M, Swain E (2000) Performance prediction of an industrial centrifugal compressor inlet guide vane system. Proc Inst Mech Eng Part A J Power Energy 214(2):153–164. https://doi.org/10.1243/0957650001538254

5. Yang M, Ricardo MB, Zhang Y (2013) Inlet duct treatment for stability improvement on a high pressure ratio centrifugal compressor. Proc ASME Turbo Expo. https://doi.org/10.1115/GT2013-95189.

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