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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 322 (HANSA-BRANDENBURG

Cambered · 13% thick · low-to-mid Re
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PROFILEGOE 322 (HANSA-BRANDENBURG
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.1% @ 30%c
max camber6.0% @ 30%c
LE radius1.88%c
area upper / chord0.0822
area lower / chord-0.0059
area camber / chord0.0381
TE thickness0.60%c
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Polars

Preliminary
NeuralFoil
-0.2001-50.51373.3331.22811.671.94120ClAngle 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 0.06547% of chord; maximum error 0.3571%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
147.9
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006989
Maximum Cl
1.763
Angle at maximum Cl (°)
10
Cd at zero lift
0.01285
Cm at zero angle
-0.1045
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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