BOEING 707 .08 SPAN AIRFOIL

Thickness: 11.4%
Camber: 0.2%
Trailing edge angle: 13.4o
Lower flatness: 5.1%
Leading edge radius: 2.9%
Efficiency: 34.0
Max CL: 0.897
Max CL angle: 15.0
Max L/D: 12.63
Max L/D angle: 7.5
Max L/D CL: 0.506
Stall angle: 1.5
Zero-lift angle: 0.5