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NACA 4-DIGITSELIG-DATABASESYMMETRICTHICK

NACA 0024

Symmetric · 24% thick · low-to-mid Re
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PROFILENACA 0024
surfacecamber line
GEOMETRY · AREA METRICS
max thickness24.0% @ 30%c
max camber0.0% @ 0%c
LE radius6.35%c
area upper / chord0.0818
area lower / chord-0.0818
area camber / chord0.0000
TE thickness0.50%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.8-5-0.094453.3330.611111.671.31720ClAngle 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 0.06582% of chord; maximum error 0.3046%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
87.87
Angle at maximum lift / drag (°)
8
Minimum Cd
0.008914
Maximum Cl
1.14
Angle at maximum Cl (°)
11
Cd at zero lift
0.008914
Cm at zero angle
5.02e-17
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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