WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL

Thickness: 11.0%
Camber: 2.3%
Trailing edge angle: 2.9o
Lower flatness: 7.5%
Leading edge radius: 3.0%
Efficiency: 31.0
Max CL: 1.209
Max CL angle: 15.0
Max L/D: 45.485
Max L/D angle: 3.0
Max L/D CL: 0.818
Stall angle: -0.5
Zero-lift angle: -4.5