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CAMBEREDOTHER FAMILIESSELIG-DATABASETHICK

UA(2)-180 smoothed, original

Cambered · 18% thick · low-to-mid Re
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PROFILEUA(2)-180 smoothed, original
surfacecamber line
GEOMETRY · AREA METRICS
max thickness18.2% @ 34%c
max camber7.0% @ 35%c
LE radius3.63%c
area upper / chord0.1008
area lower / chord-0.0150
area camber / chord0.0429
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.08321-50.55183.3331.18711.671.82220ClAngle 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 0.03952% of chord; maximum error 0.1554%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
127.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007894
Maximum Cl
1.663
Angle at maximum Cl (°)
13
Cd at zero lift
—
Cm at zero angle
-0.102
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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