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CAMBEREDS/SC SERIESSELIG-DATABASE

NASA SC(2)-0612 AIRFOIL

Cambered · 12% thick · low-to-mid Re
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PROFILENASA SC(2)-0612 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.0% @ 37%c
max camber1.1% @ 80%c
LE radius1.59%c
area upper / chord0.0436
area lower / chord-0.0373
area camber / chord0.0032
TE thickness0.58%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3763-50.51563.3331.40811.672.29920ClAngle 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 0.01206% of chord; maximum error 0.04643%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
140.6
Angle at maximum lift / drag (°)
9
Minimum Cd
0.007602
Maximum Cl
2.076
Angle at maximum Cl (°)
16
Cd at zero lift
0.007608
Cm at zero angle
-0.1158
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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