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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 16K AIRFOIL

Cambered · 18% thick · low-to-mid Re
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PROFILEGOE 16K AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness18.1% @ 50%c
max camber4.1% @ 50%c
LE radius3.63%c
area upper / chord0.0958
area lower / chord-0.0428
area camber / chord0.0265
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5682-50.069383.3330.70711.671.34520ClAngle 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 0.1297% of chord; maximum error 0.545%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
55.61
Angle at maximum lift / drag (°)
10
Minimum Cd
0.01032
Maximum Cl
1.185
Angle at maximum Cl (°)
12
Cd at zero lift
0.01158
Cm at zero angle
-0.03413
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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