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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 54 AIRFOIL

Cambered · 6% thick · low-to-mid Re
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PROFILEGOE 54 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.5% @ 15%c
max camber3.5% @ 20%c
LE radius0.46%c
area upper / chord0.0379
area lower / chord0.0017
area camber / chord0.0198
TE thickness0.35%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3813-50.18513.3330.751411.671.31820ClAngle 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 0.06755% of chord; maximum error 0.3538%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
140.1
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005966
Maximum Cl
1.176
Angle at maximum Cl (°)
7
Cd at zero lift
0.006308
Cm at zero angle
-0.02992
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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