Numerical Analysis on the Effects of splitter blade length on the performance of centrifugal compressor

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Journal of Shenyang Aerospace University ›› 2021, Vol. 38 ›› Issue (2) : 19-27.

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{{article.zuoZheEn_L}}. {{article.title_en}}. {{journal.qiKanMingCheng_EN}}. 2021, 38(2): 19-27

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Received	Revised	Published
2020-10-09	2020-10-26	2021-03-15
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2021-05-26

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