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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 123 AIRFOIL

Cambered · 5% thick · low-to-mid Re
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PROFILEGOE 123 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.4% @ 37%c
max camber5.7% @ 39%c
LE radius0.32%c
area upper / chord0.0585
area lower / chord0.0168
area camber / chord0.0377
TE thickness0.20%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1566-50.45813.3331.07311.671.68820ClAngle 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 0.0543% of chord; maximum error 0.265%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
154.5
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006691
Maximum Cl
1.534
Angle at maximum Cl (°)
8
Cd at zero lift
0.01742
Cm at zero angle
-0.1296
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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