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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 625 AIRFOIL

Cambered · 20% thick · low-to-mid Re
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PROFILEGOE 625 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness20.0% @ 30%c
max camber6.2% @ 39%c
LE radius4.41%c
area upper / chord0.1100
area lower / chord-0.0255
area camber / chord0.0423
TE thickness0.65%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.09043-50.54523.3331.18111.671.81720ClAngle 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 0.07643% of chord; maximum error 0.3233%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
104.8
Angle at maximum lift / drag (°)
5
Minimum Cd
0.008719
Maximum Cl
1.658
Angle at maximum Cl (°)
11
Cd at zero lift
—
Cm at zero angle
-0.1336
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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