Airfoils.Pro
database / Gottingen / GOE 406 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 406 AIRFOIL

Cambered · 12% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 406 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.7% @ 30%c
max camber5.5% @ 39%c
LE radius1.51%c
area upper / chord0.0782
area lower / chord-0.0058
area camber / chord0.0362
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2073-50.4333.3331.07311.671.71420ClAngle 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 0.07015% of chord; maximum error 0.3142%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
136.5
Angle at maximum lift / drag (°)
8
Minimum Cd
0.0069
Maximum Cl
1.553
Angle at maximum Cl (°)
11
Cd at zero lift
0.01529
Cm at zero angle
-0.08619
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…