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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 565 AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILEGOE 565 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.4% @ 30%c
max camber2.8% @ 50%c
LE radius0.78%c
area upper / chord0.0476
area lower / chord-0.0093
area camber / chord0.0191
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3684-50.2093.3330.786511.671.36420ClAngle 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 0.06017% of chord; maximum error 0.2473%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
142.7
Angle at maximum lift / drag (°)
5
Minimum Cd
0.00603
Maximum Cl
1.22
Angle at maximum Cl (°)
7
Cd at zero lift
0.006039
Cm at zero angle
-0.09193
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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