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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 532 AIRFOIL

Cambered · 12% thick · low-to-mid Re
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PROFILEGOE 532 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.5% @ 30%c
max camber4.8% @ 40%c
LE radius1.72%c
area upper / chord0.0721
area lower / chord-0.0050
area camber / chord0.0335
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1619-50.44423.3331.0511.671.65620ClAngle 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 0.06474% of chord; maximum error 0.3031%.

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
149.3
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006569
Maximum Cl
1.505
Angle at maximum Cl (°)
8
Cd at zero lift
0.008107
Cm at zero angle
-0.1152
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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