Airfoils.Pro
database / Gottingen / GOE 10K AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 10K AIRFOIL

Cambered · 4% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 10K AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness3.9% @ 50%c
max camber1.4% @ 60%c
LE radius0.16%c
area upper / chord0.0245
area lower / chord-0.0049
area camber / chord0.0098
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5208-50.060683.3330.642211.671.22420ClAngle 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 0.05258% of chord; maximum error 0.2306%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
102.9
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006043
Maximum Cl
1.078
Angle at maximum Cl (°)
12
Cd at zero lift
0.006088
Cm at zero angle
-0.05423
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…