Numerical and experimental investigation of an impeller tip clearance variation in an aero-engine centrifugal compressor with close-coupled pipe-diffuser-Reference-Cited by-同舟云学术

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Numerical and experimental investigation of an impeller tip clearance variation in an aero-engine centrifugal compressor with close-coupled pipe-diffuser

Published:2014-02-12 Issue:2 Volume:5 Page:171-183
ISSN:1869-5582
Container-title:CEAS Aeronautical Journal
language:en
Short-container-title:CEAS Aeronaut J

Author:

Wilkosz Benjamin,Kunte Robert,Schwarz Philipp,Jeschke Peter,Smythe Caitlin

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Link

http://link.springer.com/content/pdf/10.1007/s13272-014-0098-z.pdf

Reference22 articles.

1. Brasz, J.: Investigation into the effect of tip clearance on centrifugal compressor performance. ASME 88-GT-190 (1988)

2. Eckert, B., Schnell, E.:Axial- und Radialkompressoren. Anwendung, Theorie, Berechnung, Springer (1961)

3. Turunen-Saaresti, T., Jaatinen, A.: Influence of the different design parameters to the centrifugal compressor tip clearance loss. In: Proceedings of ASME Turbo Expo 2011, GT2011-46627 (2011)

4. Bansod, P., Rhie, C.: Computation of flow through a centrifugal impeller with tip leakage. AIAA 90-2021 (1990)

5. Senoo, Y., Ishida, M.: Deterioration of compressor performance due to tip clearance of centrifugal impellers. ASME J. Turbomach. 109, 55–61 (1987)

Cited by 1 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. Influence of Internal Flow on the Performance of High-Speed Centrifugal Pumps with a Fully Sealed Structure;Applied Sciences;2022-05-23

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