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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 358 AIRFOIL

Cambered · 11% thick · low-to-mid Re
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PROFILEGOE 358 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.8% @ 20%c
max camber5.7% @ 50%c
LE radius1.30%c
area upper / chord0.0676
area lower / chord0.0068
area camber / chord0.0372
TE thickness0.32%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.05359-50.53443.3331.12211.671.7120ClAngle 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 0.1163% of chord; maximum error 0.4818%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
161.5
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006588
Maximum Cl
1.563
Angle at maximum Cl (°)
7
Cd at zero lift
—
Cm at zero angle
-0.174
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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