AH 63-K-127/24

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Althaus AH 63-K-127/24 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:	12.7%
Camber:	3.8%
Trailing edge angle:	11.2^o
Lower flatness:	68.6%
Leading edge radius:	1.1%

Max C_L:	1.202
Max C_L angle:	7.0
Max L/D:	46.37
Max L/D angle:	5.5
Max L/D C_L:	1.036
Stall angle:	-0.5
Zero-lift angle:	-4.5