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CAMBEREDNACA OTHERSELIG-DATABASE

NACA 001264A08CLI0.2

Cambered · 11% thick · low-to-mid Re
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PROFILENACA 001264A08CLI0.2
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.0% @ 40%c
max camber1.8% @ 30%c
LE radius1.32%c
area upper / chord0.0526
area lower / chord-0.0270
area camber / chord0.0128
TE thickness0.22%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5612-50.00523.3330.571611.671.13820ClAngle 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 0.05001% of chord; maximum error 0.2328%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
109.2
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006735
Maximum Cl
0.9964
Angle at maximum Cl (°)
7
Cd at zero lift
0.006811
Cm at zero angle
-0.02613
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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