AH 79-K-132/20

Click plot for plotting control

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Althaus AH 79-K-132/20 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:	13.2%
Camber:	3.7%
Trailing edge angle:	12.6^o
Lower flatness:	62.5%
Leading edge radius:	1.2%

Max C_L:	1.151
Max C_L angle:	11.5
Max L/D:	45.005
Max L/D angle:	6.0
Max L/D C_L:	0.984
Stall angle:	-0.5
Zero-lift angle:	-3.5