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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 437 AIRFOIL

Cambered · 7% thick · low-to-mid Re
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PROFILEGOE 437 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.0% @ 30%c
max camber4.8% @ 40%c
LE radius0.55%c
area upper / chord0.0554
area lower / chord0.0085
area camber / chord0.0320
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.2026-50.41253.3331.02811.671.64320ClAngle 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 0.04724% of chord; maximum error 0.1914%.

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
162.7
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006044
Maximum Cl
1.489
Angle at maximum Cl (°)
8
Cd at zero lift
0.006936
Cm at zero angle
-0.1137
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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