Airfoils.Pro
database / Other families / AH-6-40-7 AIRFOIL
CAMBEREDOTHER FAMILIESSELIG-DATABASETHIN

AH-6-40-7 AIRFOIL

Cambered · 7% thick · low-to-mid Re
Compare↓ Download
PROFILEAH-6-40-7 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.9% @ 20%c
max camber5.5% @ 40%c
LE radius0.52%c
area upper / chord0.0607
area lower / chord0.0155
area camber / chord0.0381
TE thickness0.70%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.01808-50.58143.3331.18111.671.7820ClAngle of attack (°)
Why this curve

This is a NeuralFoil prediction from the stored profile coordinates and the selected flow condition, with AeroSandbox compressibility corrections. It is not a completed OpenFOAM calculation.

Prediction error has not been calibrated for this condition. No accuracy interval is claimed.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.05362% of chord; maximum error 0.2303%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
163.6
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006705
Maximum Cl
1.631
Angle at maximum Cl (°)
7
Cd at zero lift
—
Cm at zero angle
-0.1725
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…