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CAMBEREDNACA 6-SERIESSELIG-DATABASETHICK

NACA 64(3)-218

Cambered · 18% thick · low-to-mid Re
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PROFILENACA 64(3)-218
surfacecamber line
GEOMETRY · AREA METRICS
max thickness18.0% @ 35%c
max camber1.1% @ 50%c
LE radius3.55%c
area upper / chord0.0642
area lower / chord-0.0480
area camber / chord0.0081
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6327-50.20383.3331.0411.671.87720ClAngle 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 0.03177% of chord; maximum error 0.1236%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
121.4
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007887
Maximum Cl
1.668
Angle at maximum Cl (°)
16
Cd at zero lift
0.0079
Cm at zero angle
-0.04059
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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