Quick search for an airfoil
Browse
|
Search
|
Compare
|
Templates
|
About
GOE 377
Click plot for plotting control
Other Similar Airfoils
AG38
(
Compare
)
GOE 143 (MVA H.20)
(
Compare
)
GOE 100 (SOPWITH)
(
Compare
)
GOE 122 (MVA H.2)
(
Compare
)
NACA M13
(
Compare
)
GOE 142 (MVA H.19)
(
Compare
)
GOE 276 (DAIMLER VII)
(
Compare
)
GOE 101
(
Compare
)
GOE 399
(
Compare
)
GOE 346 (FRIEDRICHSHAFEN-STAAKEN)
(
Compare
)
Other formats
XML
DAT
Polar
No description available
Thickness:
6.5%
Camber:
3.9%
Trailing edge angle:
7.8
o
Lower flatness:
97.3%
Leading edge radius:
2.5%
Max C
L
:
1.294
Max C
L
angle:
8.0
Max L/D:
61.111
Max L/D angle:
4.5
Max L/D C
L
:
0.915
Stall angle:
8.0
Zero-lift angle:
-3.5