BOEING 707 .19 SPAN AIRFOIL

Thickness: 12.2%
Camber: 0.7%
Trailing edge angle: 13.8o
Lower flatness: 5.7%
Leading edge radius: 2.7%
Efficiency: 39.4
Max CL: 1.114
Max CL angle: 15.0
Max L/D: 16.853
Max L/D angle: 7.0
Max L/D CL: 0.612
Stall angle: 1.5
Zero-lift angle: 0.0