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CAMBEREDSELIG-DATABASETHICKWORTMANN FX

FX 66-S-196 AIRFOIL

Cambered · 20% thick · low-to-mid Re
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PROFILEFX 66-S-196 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness19.6% @ 37%c
max camber3.8% @ 43%c
LE radius4.25%c
area upper / chord0.0859
area lower / chord-0.0338
area camber / chord0.0260
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2757-50.44693.3331.16911.671.89220ClAngle 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.

Geometry fit: RMS error 0.02161% of chord; maximum error 0.1163%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
113.7
Angle at maximum lift / drag (°)
7
Minimum Cd
0.007949
Maximum Cl
1.711
Angle at maximum Cl (°)
15
Cd at zero lift
0.00795
Cm at zero angle
-0.1096
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…