AH 88-K-130/20

Click plot for plotting control

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Althaus AH 88-K-130/20 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:	13.0%
Camber:	3.9%
Trailing edge angle:	9.2^o
Lower flatness:	66.2%
Leading edge radius:	1.0%

Max C_L:	1.255
Max C_L angle:	5.0
Max L/D:	65.495
Max L/D angle:	5.0
Max L/D C_L:	1.255
Stall angle:	-0.5
Zero-lift angle:	-5.5