Numerical investigation of centrifugal compressor stability enhancement using vaned diffuser endwall contouring technology
Author:
Affiliation:
1. Department of Fluid Machinery and Engineering, School of Energy and Power Engineering Xi'an Jiaotong University Xi'an People's Republic of China
2. Shenyang Blower Works Group Corporation Shenyang People's Republic of China
Publisher
Wiley
Subject
General Energy,Safety, Risk, Reliability and Quality
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/ese3.1169
Reference25 articles.
1. HayamiH. Improvement of the flow range of transonic centrifugal compressors with a low‐solidity cascade diffuser. Turbo Expo: Power for Land Sea and Air. 2000. 2000‐GT2002‐0465.
2. ZangenehM VogtD RodunerC. Improving a vaned diffuser for a given centrifugal impeller by 3D inverse design. Turbo Expo: Power for Land Sea and Air. 2002. GT2002‐30621 pp.1111‐1122.
3. Backward Traveling Rotating Stall Waves in Centrifugal Compressors
4. Spike and Modal Stall Inception in an Advanced Turbocharger Centrifugal Compressor
5. An Investigation of Stall Inception in Centrifugal Compressor Vaned Diffuser1
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Investigation of mechanisms on leading edge vortex generation and suppression in vaned diffuser of a centrifugal compressor;Physics of Fluids;2024-09-01
2. Investigation of vaned diffuser endwall contouring technology for improving the stable operating range of a centrifugal compressor with an asymmetric volute;Energy Science & Engineering;2024-08-25
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