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CAMBEREDNACA OTHERSELIG-DATABASE

NACA 10

Cambered · 11% thick · low-to-mid Re
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PROFILENACA 10
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.2% @ 30%c
max camber5.6% @ 30%c
LE radius1.39%c
area upper / chord0.0790
area lower / chord0.0015
area camber / chord0.0403
TE thickness0.34%c
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Polars

Preliminary
NeuralFoil
-0.09919-50.47463.3331.04811.671.62220ClAngle 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 0.05986% of chord; maximum error 0.3311%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
150.9
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006512
Maximum Cl
1.479
Angle at maximum Cl (°)
7
Cd at zero lift
—
Cm at zero angle
-0.09824
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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