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CAMBEREDNACA 5-DIGITSELIG-DATABASETHICK

NACA 63215B

Cambered · 15% thick · low-to-mid Re
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PROFILENACA 63215B
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.0% @ 31%c
max camber1.5% @ 10%c
LE radius2.49%c
area upper / chord0.0587
area lower / chord-0.0388
area camber / chord0.0099
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6203-50.23273.3331.08611.671.93920ClAngle 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 0.01455% of chord; maximum error 0.04758%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
121.1
Angle at maximum lift / drag (°)
10
Minimum Cd
0.007434
Maximum Cl
1.726
Angle at maximum Cl (°)
16
Cd at zero lift
0.007439
Cm at zero angle
-0.02998
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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