Quick search for an airfoil
Browse
|
Search
|
Compare
|
About
UAG 88-143/20
Click plot for plotting control
Other Similar Airfoils
USNPS4 (smoothed)
(
Compare
)
NACA 6412
(
Compare
)
MH 114 13.02%
(
Compare
)
GOE 711 AIRFOIL
(
Compare
)
GOE 611 AIRFOIL
(
Compare
)
GOE 573 AIRFOIL
(
Compare
)
GOE 562 AIRFOIL
(
Compare
)
GOE 446 AIRFOIL
(
Compare
)
GOE 8K AIRFOIL
(
Compare
)
FX 73-170 A
(
Compare
)
Other formats
XML
DAT
Polar
No description available
Thickness:
14.3%
Camber:
6.2%
Trailing edge angle:
23.4
o
Lower flatness:
94.2%
Leading edge radius:
1.4%
Max C
L
:
1.497
Max C
L
angle:
11.0
Max L/D:
56.814
Max L/D angle:
-0.5
Max L/D C
L
:
0.739
Stall angle:
-0.5
Zero-lift angle:
-6.5