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LA2573A

Cambered · 14% thick · low-to-mid Re
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PROFILELA2573A
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.7% @ 28%c
max camber3.2% @ 26%c
LE radius2.07%c
area upper / chord0.0536
area lower / chord-0.0289
area camber / chord0.0124
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5831-50.064723.3330.712611.671.3620ClAngle 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 0.02517% of chord; maximum error 0.06826%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
123.1
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006569
Maximum Cl
1.198
Angle at maximum Cl (°)
9
Cd at zero lift
0.006582
Cm at zero angle
0.02205
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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