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CAMBEREDNACA OTHERSELIG-DATABASETHICK

NACA 5-H-15 AIRFOIL

Cambered · 15% thick · low-to-mid Re
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PROFILENACA 5-H-15 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.4% @ 40%c
max camber2.9% @ 30%c
LE radius2.61%c
area upper / chord0.0641
area lower / chord-0.0376
area camber / chord0.0133
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6979-50.0048923.3330.707711.671.4120ClAngle 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 0.06767% of chord; maximum error 0.3638%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
115.9
Angle at maximum lift / drag (°)
8
Minimum Cd
0.006842
Maximum Cl
1.235
Angle at maximum Cl (°)
11
Cd at zero lift
0.006913
Cm at zero angle
0.01037
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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