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CAMBEREDS/SC SERIESSELIG-DATABASETHIN

S2055

Cambered · 8% thick · low-to-mid Re
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PROFILES2055
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.0% @ 35%c
max camber1.7% @ 44%c
LE radius0.70%c
area upper / chord0.0398
area lower / chord-0.0163
area camber / chord0.0118
TE thickness-0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5277-50.051663.3330.63111.671.2120ClAngle 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 0.01409% of chord; maximum error 0.08008%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
126.9
Angle at maximum lift / drag (°)
5
Minimum Cd
0.005931
Maximum Cl
1.065
Angle at maximum Cl (°)
7
Cd at zero lift
0.005935
Cm at zero angle
-0.05251
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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