Study on effects of thickness on airfoil-stall at low Reynolds numbers by cusp-catastrophic model based on GA(W)-1 airfoil

被引：0
|
作者：
LI, Zhiping [1 ,2 ,3 ]
ZHANG, Peng [1 ,2 ,3 ]
PAN, Tianyu [1 ,2 ,3 ]
LI, Qiushi [1 ,2 ,3 ,4 ]
ZHANG, Jian [3 ]
机构：
[1] National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, Beihang University, Beijing,100083, China
[2] Collaborative Innovation Center for Advanced Aero-Engine, Beihang University, Beijing,100083, China
[3] School of Energy and Power Engineering, Beihang University, Beijing,100083, China
[4] Key Laboratory of Fluid and Power Machinery, Ministry of Education, Xihua University, Chengdu,610039, China
来源：
Chinese Journal of Aeronautics | 2020年 / 33卷 / 05期
关键词：
30;
D O I：
暂无
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学科分类号：
摘要：
Journal article (JA)
引用
收藏
页码：1444 / 1453
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