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CAMBEREDNACA 5-DIGITSELIG-DATABASETHICK

NACA 23024

Cambered · 24% thick · low-to-mid Re
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PROFILENACA 23024
surfacecamber line
GEOMETRY · AREA METRICS
max thickness24.0% @ 30%c
max camber1.9% @ 10%c
LE radius6.34%c
area upper / chord0.0927
area lower / chord-0.0710
area camber / chord0.0108
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.5716-5-0.015073.3330.541411.671.09820ClAngle 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 0.08468% of chord; maximum error 0.2973%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
89.88
Angle at maximum lift / drag (°)
7
Minimum Cd
0.008202
Maximum Cl
0.9588
Angle at maximum Cl (°)
9
Cd at zero lift
0.009364
Cm at zero angle
0.00499
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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