Quick search for an airfoil
Browse
|
Search
|
Compare
|
Templates
|
About
E174 (8.92%)
Click plot for plotting control
Other Similar Airfoils
S4110
(
Compare
)
GOE 235 (SCHATTE-LANZ)
(
Compare
)
GOE 318 (HANSA-BRANDENBURG VI.5)
(
Compare
)
HQ 3.0/9
(
Compare
)
naca-4410
(
Compare
)
GOE 403
(
Compare
)
SD7032-099-88
(
Compare
)
S4061-096-84
(
Compare
)
SD7034
(
Compare
)
GOE 286
(
Compare
)
Other formats
XML
DAT
Polar
No description available
Thickness:
8.9%
Camber:
3.8%
Trailing edge angle:
6.8
o
Lower flatness:
95.0%
Leading edge radius:
1.8%
Max C
L
:
1.15
Max C
L
angle:
7.0
Max L/D:
58.383
Max L/D angle:
5.0
Max L/D C
L
:
0.961
Stall angle:
7.0
Zero-lift angle:
-3.5