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11 α=10° 翼型压力系数分布和翼型表面摩擦因数分布

Fig.11 Pressure coefficients and surface friction coefficients of airfoils at α=10°