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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 630 AIRFOIL

Cambered · 13% thick · low-to-mid Re
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PROFILEGOE 630 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.5% @ 30%c
max camber7.7% @ 39%c
LE radius1.73%c
area upper / chord0.0918
area lower / chord0.0089
area camber / chord0.0504
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
0.03063-50.70523.3331.3811.672.05420ClAngle 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 0.06919% of chord; maximum error 0.3289%.

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
151.2
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007162
Maximum Cl
1.886
Angle at maximum Cl (°)
12
Cd at zero lift
—
Cm at zero angle
-0.162
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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