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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 264 AIRFOIL

Cambered · 6% thick · low-to-mid Re
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PROFILEGOE 264 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.4% @ 21%c
max camber5.7% @ 30%c
LE radius0.46%c
area upper / chord0.0593
area lower / chord0.0135
area camber / chord0.0364
TE thickness0.64%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1506-50.49233.3331.13511.671.77820ClAngle 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 0.05858% of chord; maximum error 0.2794%.

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
164.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006647
Maximum Cl
1.617
Angle at maximum Cl (°)
8
Cd at zero lift
—
Cm at zero angle
-0.1346
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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