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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 570 AIRFOIL

Cambered · 34% thick · low-to-mid Re
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PROFILEGOE 570 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness33.7% @ 30%c
max camber9.7% @ 40%c
LE radius12.51%c
area upper / chord0.1792
area lower / chord-0.0495
area camber / chord0.0649
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.4254-50.10043.3330.626211.671.15220ClAngle 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 0.1015% of chord; maximum error 0.3095%.

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
10.43
Angle at maximum lift / drag (°)
9
Minimum Cd
0.01824
Maximum Cl
1.021
Angle at maximum Cl (°)
20
Cd at zero lift
0.02409
Cm at zero angle
0.008155
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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