AH 81-K-144/17

Althaus AH 81-K-144/17 airfoil for use with flaps (K). See also Althaus, D., "Niedriggeschwindigkeitsprofile," Friedr. Vieweg & Sohn Verlagsgesellschaft mbH (publisher) Braunschweig/Weisbaden, Germany, 1996, 591 pages. ISBN 3-528-03820-9

Thickness: 14.5%
Camber: 4.2%
Trailing edge angle: 12.9o
Lower flatness: 61.9%
Leading edge radius: 1.4%
Max CL: 1.272
Max CL angle: 13.5
Max L/D: 42.133
Max L/D angle: 7.0
Max L/D CL: 1.132
Stall angle: -0.5
Zero-lift angle: -3.5