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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 585 AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILEGOE 585 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.2% @ 21%c
max camber3.4% @ 40%c
LE radius0.74%c
area upper / chord0.0506
area lower / chord-0.0055
area camber / chord0.0226
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3578-50.23253.3330.822811.671.41320ClAngle of attack (°)
Why this curve

This is a NeuralFoil prediction from the stored profile coordinates and the selected flow condition, with AeroSandbox compressibility corrections. It is not a completed OpenFOAM calculation.

Prediction error has not been calibrated for this condition. No accuracy interval is claimed.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.0508% of chord; maximum error 0.2489%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
150.6
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006032
Maximum Cl
1.265
Angle at maximum Cl (°)
8
Cd at zero lift
0.006097
Cm at zero angle
-0.08305
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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