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GOE 443 AIRFOIL

Symmetric · 5% thick · low-to-mid Re
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PROFILEGOE 443 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.0% @ 31%c
max camber0.0% @ 0%c
LE radius0.28%c
area upper / chord0.0169
area lower / chord-0.0169
area camber / chord0.0000
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.755-5-0.12253.3330.5111.671.14320ClAngle 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 0.0381% of chord; maximum error 0.1391%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
90.07
Angle at maximum lift / drag (°)
5
Minimum Cd
0.005476
Maximum Cl
0.9844
Angle at maximum Cl (°)
20
Cd at zero lift
0.005476
Cm at zero angle
5.638e-17
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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