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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 372 AIRFOIL

Cambered · 6% thick · low-to-mid Re
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PROFILEGOE 372 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.2% @ 30%c
max camber4.3% @ 40%c
LE radius0.42%c
area upper / chord0.0487
area lower / chord0.0065
area camber / chord0.0276
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.2667-50.34263.3330.951911.671.56120ClAngle 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 0.05011% of chord; maximum error 0.2584%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
156.9
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005814
Maximum Cl
1.409
Angle at maximum Cl (°)
8
Cd at zero lift
0.006278
Cm at zero angle
-0.1095
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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