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NACA 5-DIGITSELIG-DATABASESYMMETRIC

NACA 64015

Symmetric · 15% thick · low-to-mid Re
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PROFILENACA 64015
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.0% @ 35%c
max camber0.0% @ 0%c
LE radius2.47%c
area upper / chord0.0471
area lower / chord-0.0471
area camber / chord0.0000
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.8187-50.067633.3330.95411.671.8420ClAngle 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 0.02739% of chord; maximum error 0.1091%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
119.5
Angle at maximum lift / drag (°)
11
Minimum Cd
0.007387
Maximum Cl
1.619
Angle at maximum Cl (°)
16
Cd at zero lift
0.007387
Cm at zero angle
-9.723e-17
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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