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database / NACA 6-series / NACA 63(2)A-015
CAMBEREDNACA 6-SERIESSELIG-DATABASE

NACA 63(2)A-015

Cambered · 15% thick · low-to-mid Re
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PROFILENACA 63(2)A-015
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.0% @ 36%c
max camber1.7% @ 15%c
LE radius2.47%c
area upper / chord0.0587
area lower / chord-0.0399
area camber / chord0.0094
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.64-5-0.0068293.3330.626311.671.2620ClAngle 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 0.009097% of chord; maximum error 0.03297%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
119.2
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006714
Maximum Cl
1.101
Angle at maximum Cl (°)
8
Cd at zero lift
0.006788
Cm at zero angle
-0.0104
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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