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CAMBEREDNACA 6-SERIESSELIG-DATABASE

NACA 64A210

Cambered · 10% thick · low-to-mid Re
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PROFILENACA 64A210
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 39%c
max camber1.3% @ 50%c
LE radius1.10%c
area upper / chord0.0424
area lower / chord-0.0237
area camber / chord0.0094
TE thickness0.04%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6146-50.24823.3331.11111.671.97420ClAngle 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 0.01898% of chord; maximum error 0.1067%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
127.1
Angle at maximum lift / drag (°)
9
Minimum Cd
0.006644
Maximum Cl
1.758
Angle at maximum Cl (°)
16
Cd at zero lift
0.006659
Cm at zero angle
-0.04176
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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