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CAMBEREDNACA 5-DIGITSELIG-DATABASE

NACA 64-215 AIRFOIL

Cambered · 15% thick · low-to-mid Re
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PROFILENACA 64-215 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.0% @ 35%c
max camber1.1% @ 50%c
LE radius2.47%c
area upper / chord0.0551
area lower / chord-0.0390
area camber / chord0.0081
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6341-50.22633.3331.08711.671.94720ClAngle 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 0.02865% of chord; maximum error 0.1196%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
128.8
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007355
Maximum Cl
1.732
Angle at maximum Cl (°)
16
Cd at zero lift
0.007367
Cm at zero angle
-0.04162
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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