Quick search for an airfoil
Browse
|
Search
|
Compare
|
Templates
|
About
NASA/AMES 63A108 MOD C
Click plot for plotting control
Other Similar Airfoils
MH 30 7.84%
(
Compare
)
RG 14A-1.4/7.0
(
Compare
)
RAF 25
(
Compare
)
NLR-1T
(
Compare
)
RG 14 9.5%
(
Compare
)
GIII BL167
(
Compare
)
PMC19 Smoothed
(
Compare
)
HQ 0/9
(
Compare
)
NACA 1408
(
Compare
)
NACA 64-108
(
Compare
)
Other formats
XML
DAT
Polar
No description available
Thickness:
7.7%
Camber:
0.6%
Trailing edge angle:
4.8
o
Lower flatness:
57.1%
Leading edge radius:
2.3%
Max C
L
:
0.853
Max C
L
angle:
15.0
Max L/D:
51.293
Max L/D angle:
5.5
Max L/D C
L
:
0.629
Stall angle:
5.5
Zero-lift angle:
0.5