Quick search for an airfoil
Browse
|
Search
|
Compare
|
Templates
|
About
GOE 324 (HANSA-BRANDENBURG)
Click plot for plotting control
Other Similar Airfoils
GOE 573
(
Compare
)
naca-6214
(
Compare
)
GOE 365
(
Compare
)
GOE 321 (HANSA-BRANDENBURG III.1)
(
Compare
)
USA 27
(
Compare
)
MH 83 13.29%
(
Compare
)
NACA M24
(
Compare
)
NACA M21
(
Compare
)
LNV109A
(
Compare
)
GOE 744
(
Compare
)
Other formats
XML
DAT
Polar
No description available
Thickness:
13.1%
Camber:
5.9%
Trailing edge angle:
11.9
o
Lower flatness:
97.5%
Leading edge radius:
3.9%
Max C
L
:
1.665
Max C
L
angle:
15.0
Max L/D:
27.359
Max L/D angle:
8.0
Max L/D C
L
:
1.14
Stall angle:
-0.5
Zero-lift angle:
-4.0