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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 591 AIRFOIL

Cambered · 11% thick · low-to-mid Re
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PROFILEGOE 591 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.2% @ 30%c
max camber5.0% @ 40%c
LE radius1.38%c
area upper / chord0.0714
area lower / chord-0.0044
area camber / chord0.0335
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1807-50.46793.3331.11611.671.76520ClAngle 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 0.05814% of chord; maximum error 0.2816%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
156.4
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006537
Maximum Cl
1.603
Angle at maximum Cl (°)
9
Cd at zero lift
0.007532
Cm at zero angle
-0.1154
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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