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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 464 AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILEGOE 464 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.7% @ 7%c
max camber9.9% @ 30%c
LE radius0.65%c
area upper / chord0.0823
area lower / chord0.0465
area camber / chord0.0644
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
0.07666-50.60143.3331.12611.671.65120ClAngle 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 0.1051% of chord; maximum error 0.3745%.

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
43.07
Angle at maximum lift / drag (°)
6
Minimum Cd
0.0277
Maximum Cl
1.52
Angle at maximum Cl (°)
12
Cd at zero lift
—
Cm at zero angle
-0.1282
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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