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CAMBEREDNACA 5-DIGITSELIG-DATABASETHIN

NACA 64-208

Cambered · 8% thick · low-to-mid Re
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PROFILENACA 64-208
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.0% @ 39%c
max camber1.1% @ 50%c
LE radius0.70%c
area upper / chord0.0334
area lower / chord-0.0175
area camber / chord0.0080
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.6188-50.24913.3331.11711.671.98520ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.01973% of chord; maximum error 0.09791%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
126.1
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006295
Maximum Cl
1.768
Angle at maximum Cl (°)
16
Cd at zero lift
0.006302
Cm at zero angle
-0.04314
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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