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
Tab.3
C
Lmax
and stall angle of airfoils
翼型名称
C
Lmax
α
'
C2
1.0482
10°
R3
1.3363
15°