Airfoils.Pro
database / Gottingen / GOE 13K AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 13K AIRFOIL

Cambered · 15% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 13K AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.8% @ 50%c
max camber5.5% @ 60%c
LE radius2.41%c
area upper / chord0.0941
area lower / chord-0.0190
area camber / chord0.0375
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3668-50.24833.3330.863311.671.47820ClAngle 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 0.1383% of chord; maximum error 0.6375%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
76.02
Angle at maximum lift / drag (°)
8
Minimum Cd
0.008798
Maximum Cl
1.325
Angle at maximum Cl (°)
11
Cd at zero lift
0.008828
Cm at zero angle
-0.08311
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…