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NACA 5-DIGITSELIG-DATABASESYMMETRICTHICK

NACA 16-015

Symmetric · 15% thick · low-to-mid Re
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PROFILENACA 16-015
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.0% @ 50%c
max camber0.0% @ 0%c
LE radius2.48%c
area upper / chord0.0549
area lower / chord-0.0549
area camber / chord0.0000
TE thickness0.30%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.682-5-0.13433.3330.413311.670.96120ClAngle 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 0.05971% of chord; maximum error 0.2501%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
83.49
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007429
Maximum Cl
0.8241
Angle at maximum Cl (°)
8
Cd at zero lift
0.007429
Cm at zero angle
-1.002e-16
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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