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CAMBEREDNACA 6-SERIESSELIG-DATABASETHICK

NACA 63(3)-218

Cambered · 18% thick · low-to-mid Re
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PROFILENACA 63(3)-218
surfacecamber line
GEOMETRY · AREA METRICS
max thickness18.0% @ 35%c
max camber1.1% @ 25%c
LE radius3.56%c
area upper / chord0.0641
area lower / chord-0.0477
area camber / chord0.0082
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6326-50.20453.3331.04211.671.87920ClAngle 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 0.04611% of chord; maximum error 0.2883%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
121.6
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007922
Maximum Cl
1.669
Angle at maximum Cl (°)
16
Cd at zero lift
0.007927
Cm at zero angle
-0.03913
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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