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CAMBEREDSELIG-DATABASEWORTMANN FX

FX 63-110 AIRFOIL

Cambered · 11% thick · low-to-mid Re
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PROFILEFX 63-110 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 31%c
max camber4.3% @ 50%c
LE radius1.33%c
area upper / chord0.0650
area lower / chord-0.0018
area camber / chord0.0316
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.005086-50.54773.3331.111.671.65320ClAngle 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 0.05385% of chord; maximum error 0.2288%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
162.9
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006293
Maximum Cl
1.515
Angle at maximum Cl (°)
6
Cd at zero lift
—
Cm at zero angle
-0.1807
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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