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CAMBEREDS/SC SERIESSELIG-DATABASE

S6061 9%

Cambered · 9% thick · low-to-mid Re
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PROFILES6061 9%
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.0% @ 31%c
max camber1.8% @ 39%c
LE radius0.89%c
area upper / chord0.0412
area lower / chord-0.0180
area camber / chord0.0116
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5769-50.020033.3330.61711.671.21420ClAngle 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 0.01465% of chord; maximum error 0.08172%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
128.5
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005965
Maximum Cl
1.065
Angle at maximum Cl (°)
7
Cd at zero lift
0.005982
Cm at zero angle
-0.04081
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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