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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 561 AIRFOIL

Cambered · 25% thick · low-to-mid Re
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PROFILEGOE 561 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness24.9% @ 30%c
max camber10.2% @ 30%c
LE radius6.85%c
area upper / chord0.1497
area lower / chord-0.0187
area camber / chord0.0655
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.03829-50.44333.3330.924911.671.40620ClAngle 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 0.09807% of chord; maximum error 0.4147%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
46.42
Angle at maximum lift / drag (°)
2
Minimum Cd
0.01221
Maximum Cl
1.286
Angle at maximum Cl (°)
18
Cd at zero lift
—
Cm at zero angle
-0.05998
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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