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CAMBEREDSELIG-DATABASETHICKWORTMANN FX

FX 66-S-161 AIRFOIL

Cambered · 16% thick · low-to-mid Re
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PROFILEFX 66-S-161 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.1% @ 34%c
max camber3.9% @ 43%c
LE radius2.86%c
area upper / chord0.0746
area lower / chord-0.0217
area camber / chord0.0264
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2752-50.40523.3331.08611.671.76620ClAngle 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 0.01193% of chord; maximum error 0.0437%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
147.1
Angle at maximum lift / drag (°)
8
Minimum Cd
0.006755
Maximum Cl
1.596
Angle at maximum Cl (°)
10
Cd at zero lift
0.006763
Cm at zero angle
-0.1087
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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