Some shrouding and tip clearance effects in axial flow compressors1
Author:
Publisher
IOS Press
Subject
Mechanical Engineering,Ocean Engineering
Cited by 13 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. Effects of labyrinth seal with jet structure on the performance of a compressor cascade;Physics of Fluids;2024-08-01
2. Details of Shrouded Stator Hub Cavity Flow in a Multistage Axial Compressor Part 2: Leakage Flow Characteristics in Stator Wells;Journal of Engineering for Gas Turbines and Power;2021-11-02
3. Numerical analysis of hub cavity leakage;Aircraft Engineering and Aerospace Technology;2019-09-02
4. Interacting Flow Effects in the Stages of a Low-Speed Multistage Axial Compressor Using Shrouded and Cantilevered Stators;AIAA Propulsion and Energy 2019 Forum;2019-08-16
5. The Effects of Tip Leakage Flow on the Performance of Multistage Compressors Used in Small Core Engine Applications;Journal of Engineering for Gas Turbines and Power;2015-11-11
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