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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 416A AIRFOIL

Cambered · 12% thick · low-to-mid Re
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PROFILEGOE 416A AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.7% @ 30%c
max camber1.3% @ 61%c
LE radius1.50%c
area upper / chord0.0445
area lower / chord-0.0266
area camber / chord0.0089
TE thickness0.27%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5969-50.015043.3330.62711.671.23920ClAngle 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 0.04632% of chord; maximum error 0.2105%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
124.6
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006443
Maximum Cl
1.086
Angle at maximum Cl (°)
7
Cd at zero lift
0.006459
Cm at zero angle
-0.04753
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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