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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 522 AIRFOIL

Cambered · 22% thick · low-to-mid Re
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PROFILEGOE 522 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness21.8% @ 29%c
max camber5.2% @ 48%c
LE radius5.24%c
area upper / chord0.1071
area lower / chord-0.0342
area camber / chord0.0365
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.08719-50.51673.3331.12111.671.72420ClAngle 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 0.07719% of chord; maximum error 0.3433%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
104.1
Angle at maximum lift / drag (°)
5
Minimum Cd
0.008296
Maximum Cl
1.573
Angle at maximum Cl (°)
12
Cd at zero lift
—
Cm at zero angle
-0.1343
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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