AH 82-150 A

Althaus AH 82-150 A airfoil. See also Althaus, D., "Niedriggeschwindigkeitsprofile," Friedr. Vieweg & Sohn Verlagsgesellschaft mbH (publisher) Braunschweig/Weisbaden, Germany, 1996, 591 pages. ISBN 3-528-03820-9

Thickness: 15.0%
Camber: 3.3%
Trailing edge angle: 10.1o
Lower flatness: 36.2%
Leading edge radius: 1.3%
Max CL: 1.265
Max CL angle: 11.5
Max L/D: 52.829
Max L/D angle: 5.0
Max L/D CL: 1.148
Stall angle: -0.5
Zero-lift angle: -4.5