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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 598 AIRFOIL

Cambered · 7% thick · low-to-mid Re
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PROFILEGOE 598 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.5% @ 39%c
max camber1.0% @ 50%c
LE radius0.47%c
area upper / chord0.0284
area lower / chord-0.0163
area camber / chord0.0061
TE thickness0.20%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6635-5-0.072433.3330.518711.671.1120ClAngle 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 0.03741% of chord; maximum error 0.1944%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
115.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005771
Maximum Cl
0.962
Angle at maximum Cl (°)
7
Cd at zero lift
0.005772
Cm at zero angle
-0.02996
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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