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CAMBEREDSELIG-DATABASETHICKWORTMANN FX

FX 38-153 AIRFOIL

Cambered · 16% thick · low-to-mid Re
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PROFILEFX 38-153 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.5% @ 43%c
max camber2.1% @ 80%c
LE radius2.66%c
area upper / chord0.0718
area lower / chord-0.0367
area camber / chord0.0176
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3163-50.28713.3330.890511.671.49420ClAngle 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 0.01898% of chord; maximum error 0.05863%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
132.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007394
Maximum Cl
1.343
Angle at maximum Cl (°)
8
Cd at zero lift
0.007403
Cm at zero angle
-0.1121
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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