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CAMBEREDSELIG-DATABASEWORTMANN FX

FX 63-143 AIRFOIL

Cambered · 14% thick · low-to-mid Re
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PROFILEFX 63-143 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.3% @ 34%c
max camber3.1% @ 31%c
LE radius2.26%c
area upper / chord0.0653
area lower / chord-0.0276
area camber / chord0.0189
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4054-50.26083.3330.92711.671.59320ClAngle 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 0.01811% of chord; maximum error 0.0722%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
143.7
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006763
Maximum Cl
1.427
Angle at maximum Cl (°)
9
Cd at zero lift
0.006767
Cm at zero angle
-0.07052
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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