Experimental Investigation on the Layout of Tip Clearance for an Axial-Flow Compressor Rotor-Reference-Cited by-同舟云学术

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Experimental Investigation on the Layout of Tip Clearance for an Axial-Flow Compressor Rotor

Published:2005-01-10 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Zhu Junqiang¹,Sun Ling¹,Lu Xingen¹

Affiliation:

1. Northwestern Polytechnical University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-808

Reference20 articles.

1. Stalling Pressure Rise Capability of Axial Flow Compressor Stages

2. Loss Reduction in Axial-Flow Compressors Through Low-Speed Model Testing

3. Experimental Study of a High-Throughflow Transonic Axial Compressor Stage

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. Effect of circumferential non-uniform tip clearance on the dynamic stall process of a single-stage axial compressor with total pressure distortion;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-02-08

2. Impact Investigation of Stator Seal Leakage on Aerodynamic Performance of Multistage Compressor;Frontiers in Energy Research;2021-10-28

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