| 分布式粗糙前缘对NACA0012翼型失速特性的影响 | 
| 李艺, 白俊强, 张彦军, 赵轲 | 
| Influence of Distributed Leading-Edge Roughness on Stall Characteristics of NACA0012 Airfoil | 
| LI Yi, BAI Junqiang, ZHANG Yanjun, ZHAO Ke | 
| 图19 α=10° 翼型前缘附近流线图 | 
| Fig.19 Streamlines near leading edge for airfoils at α=10° | 
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