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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 523 AIRFOIL

Cambered · 16% thick · low-to-mid Re
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PROFILEGOE 523 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.5% @ 29%c
max camber9.7% @ 50%c
LE radius2.99%c
area upper / chord0.1196
area lower / chord0.0201
area camber / chord0.0699
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
0.7037-51.2223.3331.7411.672.25820ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.08328% of chord; maximum error 0.2901%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
145.3
Angle at maximum lift / drag (°)
2
Minimum Cd
0.008189
Maximum Cl
2.129
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.3154
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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