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NACA 5-DIGITSELIG-DATABASESYMMETRIC

NACA 16-012

Symmetric · 12% thick · low-to-mid Re
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PROFILENACA 16-012
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.0% @ 50%c
max camber0.0% @ 0%c
LE radius1.59%c
area upper / chord0.0439
area lower / chord-0.0439
area camber / chord0.0000
TE thickness0.24%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7366-50.072833.3330.882311.671.69220ClAngle 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.

Geometry fit: RMS error 0.05192% of chord; maximum error 0.2271%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
107.6
Angle at maximum lift / drag (°)
11
Minimum Cd
0.007523
Maximum Cl
1.489
Angle at maximum Cl (°)
17
Cd at zero lift
0.007523
Cm at zero angle
3.432e-17
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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