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UAG 88-143/20

Cambered · 14% thick · low-to-mid Re
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PROFILEUAG 88-143/20
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.3% @ 43%c
max camber6.2% @ 47%c
LE radius2.25%c
area upper / chord0.0916
area lower / chord-0.0081
area camber / chord0.0417
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.03229-50.5583.3331.14811.671.73920ClAngle 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 0.01995% of chord; maximum error 0.07729%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
99.98
Angle at maximum lift / drag (°)
5
Minimum Cd
0.007228
Maximum Cl
1.591
Angle at maximum Cl (°)
11
Cd at zero lift
—
Cm at zero angle
-0.1328
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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