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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 632 AIRFOIL

Cambered · 14% thick · low-to-mid Re
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PROFILEGOE 632 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.0% @ 30%c
max camber3.9% @ 39%c
LE radius2.16%c
area upper / chord0.0719
area lower / chord-0.0258
area camber / chord0.0230
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4246-50.20513.3330.834811.671.46420ClAngle 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 0.06888% of chord; maximum error 0.3652%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
119.6
Angle at maximum lift / drag (°)
8
Minimum Cd
0.006951
Maximum Cl
1.307
Angle at maximum Cl (°)
11
Cd at zero lift
0.006952
Cm at zero angle
-0.03967
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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