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CAMBEREDS/SC SERIESSELIG-DATABASE

NASA SC(2)-0610 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILENASA SC(2)-0610 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness10.0% @ 38%c
max camber1.0% @ 80%c
LE radius1.10%c
area upper / chord0.0364
area lower / chord-0.0311
area camber / chord0.0027
TE thickness0.49%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3966-50.49023.3331.37711.672.26420ClAngle 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 0.01205% of chord; maximum error 0.04374%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
139.2
Angle at maximum lift / drag (°)
9
Minimum Cd
0.007197
Maximum Cl
2.042
Angle at maximum Cl (°)
16
Cd at zero lift
0.007197
Cm at zero angle
-0.1086
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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