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CAMBEREDS/SC SERIESSELIG-DATABASETHIN

S2060 8%

Cambered · 8% thick · low-to-mid Re
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PROFILES2060 8%
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.0% @ 30%c
max camber1.8% @ 49%c
LE radius0.70%c
area upper / chord0.0395
area lower / chord-0.0140
area camber / chord0.0128
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4875-50.082413.3330.652311.671.22220ClAngle 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.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.01514% of chord; maximum error 0.084%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
132.8
Angle at maximum lift / drag (°)
5
Minimum Cd
0.005875
Maximum Cl
1.08
Angle at maximum Cl (°)
7
Cd at zero lift
0.005889
Cm at zero angle
-0.06843
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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