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CAMBEREDSELIG-DATABASEWORTMANN FX

FX 63-100 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEFX 63-100 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.9% @ 31%c
max camber4.3% @ 50%c
LE radius1.09%c
area upper / chord0.0618
area lower / chord0.0015
area camber / chord0.0316
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.001763-50.54543.3331.09311.671.6420ClAngle 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 0.05065% of chord; maximum error 0.2266%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
162.8
Angle at maximum lift / drag (°)
4
Minimum Cd
0.006225
Maximum Cl
1.503
Angle at maximum Cl (°)
6
Cd at zero lift
—
Cm at zero angle
-0.1814
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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