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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 506 AIRFOIL

Cambered · 16% thick · low-to-mid Re
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PROFILEGOE 506 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.5% @ 29%c
max camber4.7% @ 39%c
LE radius2.99%c
area upper / chord0.0897
area lower / chord-0.0239
area camber / chord0.0329
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1954-50.45213.3331.111.671.74720ClAngle 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 0.0618% of chord; maximum error 0.2961%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
112.4
Angle at maximum lift / drag (°)
8
Minimum Cd
0.007272
Maximum Cl
1.585
Angle at maximum Cl (°)
12
Cd at zero lift
0.007299
Cm at zero angle
-0.09771
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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