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CAMBEREDSELIG-DATABASETHICKWORTMANN FX

FX 60-177 AIRFOIL

Cambered · 18% thick · low-to-mid Re
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PROFILEFX 60-177 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness17.7% @ 37%c
max camber2.7% @ 78%c
LE radius3.46%c
area upper / chord0.0810
area lower / chord-0.0387
area camber / chord0.0211
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2223-50.40423.3331.03111.671.65720ClAngle 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 0.01993% of chord; maximum error 0.05895%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
137.4
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007756
Maximum Cl
1.5
Angle at maximum Cl (°)
8
Cd at zero lift
0.007795
Cm at zero angle
-0.1424
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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