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NACA M12

Cambered · 12% thick · low-to-mid Re
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PROFILENACA M12
surfacecamber line
GEOMETRY · AREA METRICS
max thickness11.9% @ 30%c
max camber2.0% @ 30%c
LE radius1.57%c
area upper / chord0.0537
area lower / chord-0.0297
area camber / chord0.0120
TE thickness0.40%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6369-50.23483.3331.10711.671.97820ClAngle 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 0.07596% of chord; maximum error 0.3475%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
130.4
Angle at maximum lift / drag (°)
11
Minimum Cd
0.007185
Maximum Cl
1.76
Angle at maximum Cl (°)
16
Cd at zero lift
0.007197
Cm at zero angle
-0.02506
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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