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ARA-D 10% AIRFOIL
CAMBERED
OTHER FAMILIES
SELIG-DATABASE
ARA-D 10% AIRFOIL
Cambered · 10% thick · low-to-mid Re
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PROFILE
ARA-D 10% AIRFOIL
surface
camber line
BEST-FIT POLAR
Re 102k · M 0.09 · final
15 solved points
M 0.09
(L/D)max
19.0
α @ (L/D)max
2.0°
Cd,min
0.0211
Cl @ Cd,min
0.37
Cd₀ (Cl=0)
0.0439
Cl,max
0.75
α @ Cl,max
15.0°
Cm,0
-0.04
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
▾
max thickness
10.0% @ 25%c
max camber
4.0% @ 35%c
LE radius
1.10%c
area upper / chord
0.0637
area lower / chord
-0.0100
area camber / chord
0.0268
TE thickness
1.50%c
DOWNLOAD COORDINATES
Selig .dat ↓
Lednicer ↓
XFOIL ↓
CSV coords ↓
DXF ↓
Cl–α
Cl–Cd
L/D–α
Cm–α
15 solved points
M 0.09
−
+
fit
0.0
0.2
0.4
0.6
0.8
-5
0
5
10
15
angle of attack α [deg]
Cl
POLARS
Re 102k · M 0.09 · 15
best-fit
post-stall → URANS
SOLVER WORK
0 conditions · 0 engine jobs
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Attention 0
Solving 0
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