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CAMBEREDNACA OTHERSELIG-DATABASE

NACA 2-H-15 AIRFOIL

Cambered · 15% thick · low-to-mid Re
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PROFILENACA 2-H-15 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.7% @ 40%c
max camber4.5% @ 40%c
LE radius2.39%c
area upper / chord0.0712
area lower / chord-0.0269
area camber / chord0.0221
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.4977-50.13893.3330.775511.671.41220ClAngle 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.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.1063% of chord; maximum error 0.3959%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
66.29
Angle at maximum lift / drag (°)
5
Minimum Cd
0.007233
Maximum Cl
1.253
Angle at maximum Cl (°)
11
Cd at zero lift
0.007282
Cm at zero angle
0.003423
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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