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NACA 4-DIGITSELIG-DATABASESYMMETRICTHICK

NACA 0015

Symmetric · 15% thick · low-to-mid Re
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PROFILENACA 0015
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.0% @ 30%c
max camber0.0% @ 0%c
LE radius2.48%c
area upper / chord0.0511
area lower / chord-0.0511
area camber / chord0.0000
TE thickness0.32%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.8151-50.089383.3330.993811.671.89820ClAngle 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 0.05713% of chord; maximum error 0.2837%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
120.9
Angle at maximum lift / drag (°)
12
Minimum Cd
0.007849
Maximum Cl
1.672
Angle at maximum Cl (°)
17
Cd at zero lift
0.007849
Cm at zero angle
1.144e-17
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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