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CAMBEREDNACA 4-DIGITSELIG-DATABASE

NACA 2415

Cambered · 15% thick · low-to-mid Re
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PROFILENACA 2415
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.0% @ 30%c
max camber2.0% @ 40%c
LE radius2.48%c
area upper / chord0.0649
area lower / chord-0.0377
area camber / chord0.0136
TE thickness0.31%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5521-50.30173.3331.15511.672.00920ClAngle 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 0.01873% of chord; maximum error 0.08251%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
130.2
Angle at maximum lift / drag (°)
11
Minimum Cd
0.007796
Maximum Cl
1.796
Angle at maximum Cl (°)
16
Cd at zero lift
0.007797
Cm at zero angle
-0.05241
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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