Investigating on performance parameters and flow field of centrifugal compressor based on the splitter blade leading edge’s location effect
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials
Link
https://link.springer.com/content/pdf/10.1007/s12206-022-0722-5.pdf
Reference33 articles.
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3. S. Li et al., Numerical study of the improvement in stability and performance by use of a partial vaned diffuser for a centrifugal compressor stage, Appl. Sci., 11 (15) (2021).
4. S. Li et al., Numerical investigation of transient flow characteristics in a centrifugal compressor stage with variable inlet guide vanes at low mass flow rates, Energies, 14 (23) (2021).
5. M. Casey, F. Gersbach and C. Robinson, An optimization technique for radial compressor impellers, Proceedings of the ASME Turbo Expo 2008: Power for Land, Sea, and Air, Volume 6: Turbomachinery, Parts A, B, and C, Berlin, Germany, June 9–13 (2008) 2401–2411.
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