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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 11K AIRFOIL

Cambered · 7% thick · low-to-mid Re
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PROFILEGOE 11K AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.4% @ 50%c
max camber2.7% @ 60%c
LE radius0.61%c
area upper / chord0.0474
area lower / chord-0.0096
area camber / chord0.0189
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3267-50.18463.3330.695911.671.20720ClAngle 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 0.09045% of chord; maximum error 0.405%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
132.6
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006093
Maximum Cl
1.079
Angle at maximum Cl (°)
7
Cd at zero lift
0.006131
Cm at zero angle
-0.09631
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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