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NACA OTHERSELIG-DATABASESYMMETRIC

NACA 14

Symmetric · 11% thick · low-to-mid Re
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PROFILENACA 14
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.5% @ 30%c
max camber0.0% @ 21%c
LE radius1.45%c
area upper / chord0.0412
area lower / chord-0.0408
area camber / chord0.0002
TE thickness0.00%c
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Polars

Preliminary
Combined estimate
-0.7522-50.093133.3330.938411.671.78420ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.05437% of chord; maximum error 0.2618%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
117.8
Angle at maximum lift / drag (°)
11
Minimum Cd
0.007226
Maximum Cl
1.572
Angle at maximum Cl (°)
17
Cd at zero lift
0.007227
Cm at zero angle
-0.001138
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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