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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 619 AIRFOIL

Cambered · 14% thick · low-to-mid Re
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PROFILEGOE 619 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.8% @ 21%c
max camber4.5% @ 49%c
LE radius2.09%c
area upper / chord0.0752
area lower / chord-0.0153
area camber / chord0.0300
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.226-50.44443.3331.11511.671.78520ClAngle 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 0.067% of chord; maximum error 0.3428%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
147.5
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006808
Maximum Cl
1.618
Angle at maximum Cl (°)
10
Cd at zero lift
0.00687
Cm at zero angle
-0.1193
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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