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CAMBEREDSELIG-DATABASETHICKWORTMANN FX

FX 67-K-170/17 AIRFOIL

Cambered · 17% thick · low-to-mid Re
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PROFILEFX 67-K-170/17 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness17.0% @ 40%c
max camber5.1% @ 44%c
LE radius3.19%c
area upper / chord0.0879
area lower / chord-0.0223
area camber / chord0.0328
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.1904-50.42983.3331.0511.671.6720ClAngle 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 0.01341% of chord; maximum error 0.04566%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
119.3
Angle at maximum lift / drag (°)
5
Minimum Cd
0.00703
Maximum Cl
1.515
Angle at maximum Cl (°)
11
Cd at zero lift
0.007063
Cm at zero angle
-0.1163
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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