Numerical model of predicting surge boundaries in high-speed centrifugal compressors-Reference-Cited by-同舟云学术

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Numerical model of predicting surge boundaries in high-speed centrifugal compressors

Published:2023-10 Issue: Volume:141 Page:108518
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Zhang Meijie^ORCID,Wu Wangxia^ORCID,Zhou Chao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

1. Experimental investigations on effects of the self-circulation casing treatment on acoustic and surge characteristics in a centrifugal compressor;Zhao;Aerosp. Sci. Technol.,2022

2. Design considerations for the final-stage centrifugal compressor in aeroengines;Lou;J. Propuls. Power,2020

3. Investigation of stall inception behavior in a centrifugal compressor with bent pipe/volute coupling effect;Zhang;J. Propuls. Power,2019

4. Impact of exit duct dynamic response on compressor stability;Zhang;J. Turbomach.,2020

5. Surge and rotating stall in axial flow compressors—part I: theoretical compression system model;Greitzer;J. Eng. Power,1976

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1. A combinatorial prediction model for the performance of fuel cell air compressor with air bearings considering accelerated decay characteristics;Applied Thermal Engineering;2024-09

2. Aerodynamic performance enhancement of centrifugal compressor using numerical techniques;F1000Research;2024-05-17

3. Dynamic numerical simulation method and flow characteristic analysis on the mode transition in variable cycle compression system;Aerospace Science and Technology;2023-12

4. Dynamic mode characteristics of flow instabilities in a centrifugal compressor impeller;Aerospace Science and Technology;2023-11

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