Quick search for an airfoil
Browse
|
Search
|
Compare
|
Templates
|
About
R140 (original)
Click plot for plotting control
Other Similar Airfoils
GIII BL0
(
Compare
)
NACA 64-012A
(
Compare
)
NPL 9626
(
Compare
)
EPPLER 297
(
Compare
)
NACA 63012A
(
Compare
)
R140 12.04% (smoothed)
(
Compare
)
R140 12.04% (smoothed)
(
Compare
)
NACA 64(1)-112
(
Compare
)
NACA 0012-34
(
Compare
)
AH 85-L-120/17
(
Compare
)
Other formats
XML
DAT
Polar
No description available
Thickness:
12.0%
Camber:
0.5%
Trailing edge angle:
15.7
o
Lower flatness:
25.0%
Leading edge radius:
1.1%
Max C
L
:
0.6
Max C
L
angle:
9.5
Max L/D:
31.632
Max L/D angle:
3.0
Max L/D C
L
:
0.387
Stall angle:
3.0
Zero-lift angle:
0.0