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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 563 AIRFOIL

Cambered · 9% thick · low-to-mid Re
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PROFILEGOE 563 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.9% @ 30%c
max camber2.2% @ 49%c
LE radius0.87%c
area upper / chord0.0460
area lower / chord-0.0156
area camber / chord0.0152
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.5172-50.32723.3331.17211.672.01620ClAngle 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 0.05058% of chord; maximum error 0.2627%.

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
135
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006634
Maximum Cl
1.805
Angle at maximum Cl (°)
16
Cd at zero lift
0.006638
Cm at zero angle
-0.0572
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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