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NACA OTHERSELIG-DATABASESYMMETRIC

NACA 0012-64

Symmetric · 12% thick · low-to-mid Re
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PROFILENACA 0012-64
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.0% @ 40%c
max camber0.0% @ 0%c
LE radius1.58%c
area upper / chord0.0432
area lower / chord-0.0432
area camber / chord0.0000
TE thickness0.24%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7952-50.087413.3330.9711.671.85320ClAngle 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 0.05555% of chord; maximum error 0.2681%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
121
Angle at maximum lift / drag (°)
11
Minimum Cd
0.00734
Maximum Cl
1.632
Angle at maximum Cl (°)
17
Cd at zero lift
0.00734
Cm at zero angle
9.151e-17
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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