Publisher
Springer Science and Business Media LLC
Reference19 articles.
1. Denton J.D., Loss mechanism in turbomachines. Journal of Turbomachinery, 1993, 115(04): 621–656. DOI: https://doi.org/10.1115/93-GT-435.
2. Han S.B., Numerical simulation of using blade tip winglet in plane compressor cascade. Dalian Maritime University, Dalian, China, 2009. (in Chinese)
3. Han S.B., Experimental and numerical investigation of compressor tip clearance flow control using blade tip winglet. Dalian Maritime University, Dalian, China, 2013. (in Chinese)
4. Zhong J.J., Wu W.Y., Han S.B., Research progress of tip winglet technology in compressor. Journal of Thermal Science, 2021, 30(01): 18–31. DOI: https://doi.org/10.1007/s11630-020-1402-3.
5. Wu W.Y., Zhong J.J., Han S.B., Effects of pressure side winglet on aerodynamic performance of high subsonic compressor cascade with different incidences. Journal of Propulsion Technology, 2018, 39(01): 76–85. DOI: https://doi.org/10.13675/j.cnki.tjjs.2018.01.008. (in Chinese)
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