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NACA OTHERSELIG-DATABASESYMMETRIC

NACA 12

Symmetric · 10% thick · low-to-mid Re
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PROFILENACA 12
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.5% @ 30%c
max camber0.2% @ 15%c
LE radius1.21%c
area upper / chord0.0366
area lower / chord-0.0357
area camber / chord0.0004
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.7624-50.10783.3330.977911.671.84820ClAngle 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 0.05371% of chord; maximum error 0.2514%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
120.1
Angle at maximum lift / drag (°)
11
Minimum Cd
0.006987
Maximum Cl
1.631
Angle at maximum Cl (°)
17
Cd at zero lift
0.006987
Cm at zero angle
-0.0004846
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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