Effects of blade positive curving on aerodynamic performance of compressor cascades

被引：0
|
作者：
Wang, Hui-She [1 ]
Zhong, Jing-Jun [1 ]
Wang, Zhong-Qi [1 ]
Liu, Yan-Ming [1 ]
Yuan, Xin [1 ]
机构：
[1] Sch. of Energy Sci. and Eng., Harbin Inst. of Technol., Harbin 150001, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2002年 / 23卷 / 04期
关键词：
Blade airfoil - Compressor blade - Compressor cascade - Energy loss coefficient - Positive curving - Straight blades - Vorticity;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
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页码：321 / 324
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