AH 93-156

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Althaus AH 93-156 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:	15.7%
Camber:	3.7%
Trailing edge angle:	14.1^o
Lower flatness:	34.5%
Leading edge radius:	1.3%

Max C_L:	1.403
Max C_L angle:	10.5
Max L/D:	44.069
Max L/D angle:	7.0
Max L/D C_L:	1.111
Stall angle:	-0.5
Zero-lift angle:	-3.5