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CAMBEREDNACA 5-DIGITSELIG-DATABASETHIN

NACA 64-108 AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILENACA 64-108 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.0% @ 39%c
max camber0.6% @ 50%c
LE radius0.70%c
area upper / chord0.0294
area lower / chord-0.0215
area camber / chord0.0040
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7099-50.1663.3331.04211.671.91820ClAngle 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 0.01922% of chord; maximum error 0.09631%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
120.3
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006307
Maximum Cl
1.699
Angle at maximum Cl (°)
16
Cd at zero lift
0.006311
Cm at zero angle
-0.02158
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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