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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 385 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEGOE 385 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.9% @ 30%c
max camber4.1% @ 30%c
LE radius1.08%c
area upper / chord0.0608
area lower / chord-0.0063
area camber / chord0.0273
TE thickness0.42%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3411-50.31993.3330.980811.671.64220ClAngle 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 0.05603% of chord; maximum error 0.2867%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
154.1
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006391
Maximum Cl
1.476
Angle at maximum Cl (°)
9
Cd at zero lift
0.006633
Cm at zero angle
-0.08362
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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