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NACA 5-DIGITSELIG-DATABASESYMMETRICTHICK

NACA 16-018

Symmetric · 18% thick · low-to-mid Re
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PROFILENACA 16-018
surfacecamber line
GEOMETRY · AREA METRICS
max thickness18.0% @ 50%c
max camber0.0% @ 0%c
LE radius3.57%c
area upper / chord0.0659
area lower / chord-0.0659
area camber / chord0.0000
TE thickness0.36%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5401-50.13373.3330.807511.671.48120ClAngle 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 0.06655% of chord; maximum error 0.2656%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
79.2
Angle at maximum lift / drag (°)
12
Minimum Cd
0.008939
Maximum Cl
1.313
Angle at maximum Cl (°)
17
Cd at zero lift
0.008939
Cm at zero angle
1.601e-16
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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