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CAMBEREDS/SC SERIESSELIG-DATABASE

S5010

Cambered · 10% thick · low-to-mid Re
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PROFILES5010
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.8% @ 27%c
max camber2.2% @ 28%c
LE radius1.06%c
area upper / chord0.0419
area lower / chord-0.0185
area camber / chord0.0117
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.7033-5-0.058523.3330.586311.671.23120ClAngle 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 0.01461% of chord; maximum error 0.08985%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
124.3
Angle at maximum lift / drag (°)
7
Minimum Cd
0.005999
Maximum Cl
1.07
Angle at maximum Cl (°)
8
Cd at zero lift
0.006007
Cm at zero angle
0.006923
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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