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AH 79-100 B
Click plot for plotting control
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Other formats
XML
DAT
Polar
Althaus AH 79-100B airfoil
Thickness:
10.0%
Camber:
6.4%
Trailing edge angle:
6.5
o
Lower flatness:
55.2%
Leading edge radius:
1.3%
Max C
L
:
1.725
Max C
L
angle:
7.0
Max L/D:
78.342
Max L/D angle:
4.0
Max L/D C
L
:
1.423
Stall angle:
7.0
Zero-lift angle:
-8.0