Airfoils.Pro
database / Gottingen / GOE 405 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 405 AIRFOIL

Cambered · 11% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 405 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.1% @ 30%c
max camber6.5% @ 40%c
LE radius1.36%c
area upper / chord0.0819
area lower / chord0.0040
area camber / chord0.0429
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.006327-50.64443.3331.29511.671.94620ClAngle 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 0.07232% of chord; maximum error 0.2948%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
156.7
Angle at maximum lift / drag (°)
7
Minimum Cd
0.0068
Maximum Cl
1.783
Angle at maximum Cl (°)
10
Cd at zero lift
—
Cm at zero angle
-0.1565
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…