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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 441 AIRFOIL

Cambered · 16% thick · low-to-mid Re
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PROFILEGOE 441 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.0% @ 29%c
max camber7.7% @ 40%c
LE radius2.81%c
area upper / chord0.1024
area lower / chord0.0046
area camber / chord0.0535
TE thickness0.27%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
0.3099-50.9243.3331.53811.672.15220ClAngle 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 0.07756% of chord; maximum error 0.3264%.

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
153.4
Angle at maximum lift / drag (°)
4
Minimum Cd
0.007586
Maximum Cl
1.999
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.2376
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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