Quick search for an airfoil
Browse
|
Search
|
Compare
|
Templates
|
About
EPPLER E662
Click plot for plotting control
Other Similar Airfoils
FX 62-K-153/20
(
Compare
)
EPPLER 582
(
Compare
)
EPPLER 433
(
Compare
)
NASA/LANGLEY NLF(1)-0215F
(
Compare
)
EPPLER 431
(
Compare
)
EPPLER 668
(
Compare
)
EPPLER 432
(
Compare
)
EPPLER 585
(
Compare
)
EPPLER 657
(
Compare
)
NASA NLF1015
(
Compare
)
Other formats
XML
DAT
Polar
No description available
Thickness:
15.0%
Camber:
4.1%
Trailing edge angle:
15.8
o
Lower flatness:
59.6%
Leading edge radius:
2.1%
Max C
L
:
1.662
Max C
L
angle:
11.0
Max L/D:
55.6
Max L/D angle:
6.0
Max L/D C
L
:
1.273
Stall angle:
-0.5
Zero-lift angle:
-5.5