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CAMBEREDNACA OTHERSELIG-DATABASE

NACA 001034A08CLI0.2

Cambered · 10% thick · low-to-mid Re
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PROFILENACA 001034A08CLI0.2
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 40%c
max camber1.3% @ 50%c
LE radius1.10%c
area upper / chord0.0443
area lower / chord-0.0257
area camber / chord0.0093
TE thickness0.20%c
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Polars

Preliminary
NeuralFoil
-0.5824-50.014443.3330.611311.671.20820ClAngle 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 0.03055% of chord; maximum error 0.1259%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
124.8
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006295
Maximum Cl
1.059
Angle at maximum Cl (°)
8
Cd at zero lift
0.006305
Cm at zero angle
-0.04678
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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