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AH-6-40-7 AIRFOIL
CAMBERED
OTHER FAMILIES
SELIG-DATABASE
THIN
AH-6-40-7 AIRFOIL
Cambered · 7% thick · low-to-mid Re
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PROFILE
AH-6-40-7 AIRFOIL
surface
camber line
BEST-FIT POLAR
Re 102k · M 0.09 · final
12 solved points
M 0.09
(L/D)max
52.4
α @ (L/D)max
8.0°
Cd,min
0.0186
Cl @ Cd,min
0.74
Cd₀ (Cl=0)
0.0509
Cl,max
1.31
α @ Cl,max
12.0°
Cm,0
-0.05
fit is derived from stored OpenFOAM evidence only
GEOMETRY · AREA METRICS
▾
max thickness
6.9% @ 20%c
max camber
5.5% @ 40%c
LE radius
0.52%c
area upper / chord
0.0607
area lower / chord
0.0155
area camber / chord
0.0381
TE thickness
0.70%c
DOWNLOAD COORDINATES
Selig .dat ↓
Lednicer ↓
XFOIL ↓
CSV coords ↓
DXF ↓
Cl–α
Cl–Cd
L/D–α
Cm–α
12 solved points
M 0.09
−
+
fit
-0.2
0.0
0.2
0.4
0.6
0.8
1.0
1.2
1.4
-5
0
5
10
15
angle of attack α [deg]
Cl
POLARS
Re 102k · M 0.09 · 12
best-fit
post-stall → URANS
SOLVER WORK
0 conditions · 0 engine jobs
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Attention 0
Solving 0
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