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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 534 AIRFOIL

Cambered · 14% thick · low-to-mid Re
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PROFILEGOE 534 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.1% @ 20%c
max camber5.2% @ 40%c
LE radius2.19%c
area upper / chord0.0758
area lower / chord-0.0044
area camber / chord0.0357
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1624-50.44723.3331.05711.671.66620ClAngle 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 0.0639% of chord; maximum error 0.2883%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
143.7
Angle at maximum lift / drag (°)
5
Minimum Cd
0.00683
Maximum Cl
1.514
Angle at maximum Cl (°)
8
Cd at zero lift
0.007351
Cm at zero angle
-0.1091
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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