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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 435 AIRFOIL

Cambered · 26% thick · low-to-mid Re
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PROFILEGOE 435 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness26.0% @ 28%c
max camber4.7% @ 48%c
LE radius7.47%c
area upper / chord0.1121
area lower / chord-0.0482
area camber / chord0.0320
TE thickness0.27%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1196-50.49563.3331.11111.671.72620ClAngle 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 0.08985% of chord; maximum error 0.3521%.

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
107.2
Angle at maximum lift / drag (°)
4
Minimum Cd
0.008874
Maximum Cl
1.572
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.1534
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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