Airfoils.Pro
database / Gottingen / GOE 500 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 500 AIRFOIL

Cambered · 10% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 500 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 30%c
max camber6.0% @ 50%c
LE radius1.10%c
area upper / chord0.0716
area lower / chord0.0082
area camber / chord0.0399
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
0.03767-50.61753.3331.19711.671.77720ClAngle 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 0.05973% of chord; maximum error 0.2698%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
166.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006425
Maximum Cl
1.632
Angle at maximum Cl (°)
7
Cd at zero lift
—
Cm at zero angle
-0.1897
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…