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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 533 AIRFOIL

Cambered · 14% thick · low-to-mid Re
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PROFILEGOE 533 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.7% @ 30%c
max camber4.7% @ 40%c
LE radius2.07%c
area upper / chord0.0748
area lower / chord-0.0092
area camber / chord0.0328
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1711-50.49173.3331.15511.671.81720ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 1 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 0.06611% of chord; maximum error 0.2807%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

  • · Converged

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
32.7
Angle at maximum lift / drag (°)
7
Minimum Cd
0.03183
Maximum Cl
1.652
Angle at maximum Cl (°)
9
Cd at zero lift
0.03782
Cm at zero angle
-0.113
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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