Airfoils
.Pro
Browse
Search
Detail
Compare
⌕ jump to airfoil…
Browse
Search
Detail
Compare
☾
database
/
Other families
/
ARA-D 6% AIRFOIL
CAMBERED
OTHER FAMILIES
SELIG-DATABASE
THIN
ARA-D 6% AIRFOIL
Cambered · 6% thick · low-to-mid Re
+ Add to compare
↓ Download
PROFILE
ARA-D 6% AIRFOIL
surface
camber line
BEST-FIT POLAR
Re 102k · M 0.09 · final
10 solved points
M 0.09
(L/D)max
41.2
α @ (L/D)max
5.0°
Cd,min
0.0201
Cl @ Cd,min
0.69
Cd₀ (Cl=0)
0.0443
Cl,max
0.92
α @ Cl,max
5.0°
Cm,0
-0.06
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
▾
max thickness
6.0% @ 20%c
max camber
5.0% @ 45%c
LE radius
0.40%c
area upper / chord
0.0575
area lower / chord
0.0106
area camber / chord
0.0341
TE thickness
1.10%c
DOWNLOAD COORDINATES
Selig .dat ↓
Lednicer ↓
XFOIL ↓
CSV coords ↓
DXF ↓
Cl–α
Cl–Cd
L/D–α
Cm–α
10 solved points
M 0.09
−
+
fit
0.0
0.2
0.4
0.6
0.8
-4
-2
0
2
4
angle of attack α [deg]
Cl
POLARS
Re 102k · M 0.09 · 10
best-fit
SOLVER WORK
0 conditions · 0 engine jobs
All 0
Attention 0
Solving 0
Re ↑
attention first
recent
Loading solver work…