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CAMBEREDSELIG-DATABASEWORTMANN FX

FX 63-147 AIRFOIL

Cambered · 15% thick · low-to-mid Re
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PROFILEFX 63-147 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.7% @ 35%c
max camber3.1% @ 34%c
LE radius2.40%c
area upper / chord0.0714
area lower / chord-0.0251
area camber / chord0.0232
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1951-50.45463.3331.10411.671.75420ClAngle 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 0.0158% of chord; maximum error 0.0541%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
153.6
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007083
Maximum Cl
1.592
Angle at maximum Cl (°)
8
Cd at zero lift
0.007115
Cm at zero angle
-0.1386
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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