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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 456 AIRFOIL

Cambered · 7% thick · low-to-mid Re
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PROFILEGOE 456 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.2% @ 30%c
max camber5.2% @ 40%c
LE radius0.57%c
area upper / chord0.0588
area lower / chord0.0094
area camber / chord0.0341
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1196-50.49353.3331.10711.671.7220ClAngle 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 0.04107% of chord; maximum error 0.1591%.

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
145.1
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006769
Maximum Cl
1.566
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.1366
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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