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CAMBEREDOTHER FAMILIESSELIG-DATABASETHICK

NASA LRN 1015

Cambered · 15% thick · low-to-mid Re
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PROFILENASA LRN 1015
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.2% @ 40%c
max camber4.9% @ 43%c
LE radius2.54%c
area upper / chord0.0845
area lower / chord-0.0168
area camber / chord0.0338
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1257-50.45953.3331.04511.671.6320ClAngle 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 0.02388% of chord; maximum error 0.09362%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
143.9
Angle at maximum lift / drag (°)
6
Minimum Cd
0.00728
Maximum Cl
1.484
Angle at maximum Cl (°)
8
Cd at zero lift
—
Cm at zero angle
-0.1123
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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