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3 光滑翼型0° 迎角表面摩擦因数分布

Fig.3 Distribution of surface friction coefficient at an angle of attack of 0° for smooth airfoil