Research Progress of Tip Winglet Technology in Compressor-Reference-Cited by-同舟云学术

Research Progress of Tip Winglet Technology in Compressor

Published:2020-12-03 Issue:1 Volume:30 Page:18-31
ISSN:1003-2169
Container-title:Journal of Thermal Science
language:en
Short-container-title:J. Therm. Sci.

Author:

Zhong Jingjun,Wu Wanyang,Han Shaobing

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Link

http://link.springer.com/content/pdf/10.1007/s11630-020-1402-3.pdf

Reference37 articles.

1. Freeman C., Tip clearance effects in axial turbomachines. Von Karman Institute lecture series, VKI-LS 1985-05.

2. Cumpsty N.A., Compressor aerodynamics. Longman Scientific and Technical, London, 1989.

3. Wisler D.C., Advanced compressor and fan systems design. General Electric Aircraft Engine Business Group, Cincinnati, 1988.

4. Baghdadi S., Modeling tip clearance effects in multistage axial compressors. ASME Journal of Turbomachinery, 1996, 118(4): 697–705.

5. Crook A.J., Greitzer E.M., Tan C.S, et al., Numerical simulation of compressor endwall and casing treatment flow phenomena. ASME Journal of Turbomachinery, 1990, 112(3): 868–894.

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