Quick search for an airfoil
Browse
|
Search
|
Compare
|
Templates
|
About
GOE 316 (HANSA-BRANDENBURG IV.5)
Click plot for plotting control
Other Similar Airfoils
GOE 315 (HANSA-BRANDENBURG III.5)
(
Compare
)
NACA M14
(
Compare
)
GOE 167 (V.KARMAN PROP.2)
(
Compare
)
AG35
(
Compare
)
GOE 257
(
Compare
)
GOE 309 (MVA H.41)
(
Compare
)
GOE 385
(
Compare
)
naca-4208
(
Compare
)
GOE 137 (MVA H.15)
(
Compare
)
AQUILA 9.3% smoothed
(
Compare
)
Other formats
XML
DAT
Polar
No description available
Thickness:
9.1%
Camber:
4.2%
Trailing edge angle:
8.7
o
Lower flatness:
98.9%
Leading edge radius:
2.9%
Max C
L
:
1.307
Max C
L
angle:
10.5
Max L/D:
47.182
Max L/D angle:
5.0
Max L/D C
L
:
0.972
Stall angle:
10.5
Zero-lift angle:
-3.0