Effect of meridian plane dip angle of the variable pitch inducer blade on cavitation performance of high-speed centrifugal pump-Reference-Cited by-同舟云学术

Effect of meridian plane dip angle of the variable pitch inducer blade on cavitation performance of high-speed centrifugal pump

Published:2020-04-06 Issue:5 Volume:42 Page:
ISSN:1678-5878
Container-title:Journal of the Brazilian Society of Mechanical Sciences and Engineering
language:en
Short-container-title:J Braz. Soc. Mech. Sci. Eng.

Author:

Cheng Xiaorui^ORCID,Jia Ningning,Lv Boru,Chen Hongxing

Funder

the Chinese National Natural Science Foundation

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Link

http://link.springer.com/content/pdf/10.1007/s40430-020-02289-3.pdf

Reference20 articles.

1. Jichao Y, Ying P, Baoling C et al (2008) Flow field analysis and cavitation process simulation of high-speed fuel centrifugal pump. Comput Simul 25(06):70–74

2. Jie h, Haili Y, Min Y (2014) Research on inducer of high-speed centrifugal pump with low cavitation margin. Rocket Propuls 40(6):19–23

3. Fei T, Jiawen L, Dexin X et al (2008) Research on methods to improve cavitation performance of oxygen pump inducer. Aviat Dyn Daily 23(9):1743–1747

4. Fanyu K, Hongli Z, Xufeng Z, Zhiqiang W (2010) Design of variable pitch inducer based on numerical simulation of cavitation flow. J Drain Irrig Mach Eng 28(01):12–17

5. Wenting W, Hui C, Yongpeng L, Yujie D (2015) Matching of inducer and centrifugal impeller of high-speed centrifugal pump. J Drain Irrig Mach Eng 33(04):301–305

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