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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 499 AIRFOIL

Cambered · 7% thick · low-to-mid Re
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PROFILEGOE 499 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.8% @ 30%c
max camber5.8% @ 50%c
LE radius0.51%c
area upper / chord0.0605
area lower / chord0.0174
area camber / chord0.0389
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
0.04732-50.62223.3331.19711.671.77220ClAngle 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 0.05676% of chord; maximum error 0.3166%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
173
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006147
Maximum Cl
1.628
Angle at maximum Cl (°)
7
Cd at zero lift
—
Cm at zero angle
-0.1986
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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