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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 503 AIRFOIL

Cambered · 16% thick · low-to-mid Re
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PROFILEGOE 503 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.6% @ 30%c
max camber7.0% @ 39%c
LE radius2.68%c
area upper / chord0.0987
area lower / chord-0.0109
area camber / chord0.0439
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.05446-50.57243.3331.19911.671.82620ClAngle 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 0.06521% of chord; maximum error 0.263%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
111.4
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007482
Maximum Cl
1.669
Angle at maximum Cl (°)
13
Cd at zero lift
—
Cm at zero angle
-0.1105
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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