Airfoils.Pro
database / Gottingen / GOE 63 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 63 AIRFOIL

Cambered · 8% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 63 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.3% @ 20%c
max camber6.7% @ 39%c
LE radius0.75%c
area upper / chord0.0725
area lower / chord0.0148
area camber / chord0.0437
TE thickness0.70%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1002-50.57673.3331.25411.671.9320ClAngle 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 0.07119% of chord; maximum error 0.4168%.

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
165.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007076
Maximum Cl
1.761
Angle at maximum Cl (°)
8
Cd at zero lift
—
Cm at zero angle
-0.1483
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…