BOEING 707 .54 SPAN AIRFOIL

Thickness: 9.0%
Camber: 2.0%
Trailing edge angle: 11.2o
Lower flatness: 14.7%
Leading edge radius: 1.7%
Efficiency: 30.4
Max CL: 0.876
Max CL angle: 11.0
Max L/D: 26.974
Max L/D angle: 0.0
Max L/D CL: 0.237
Stall angle: 0.5
Zero-lift angle: -2.0