Airfoils.Pro
database / S/SC series / S2046
CAMBEREDS/SC SERIESSELIG-DATABASE

S2046

Cambered · 9% thick · low-to-mid Re
Compare↓ Download
PROFILES2046
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.0% @ 28%c
max camber2.6% @ 56%c
LE radius0.90%c
area upper / chord0.0469
area lower / chord-0.0099
area camber / chord0.0185
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.3533-50.20083.3330.754811.671.30920ClAngle 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 0.01283% of chord; maximum error 0.0623%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
146
Angle at maximum lift / drag (°)
5
Minimum Cd
0.005982
Maximum Cl
1.17
Angle at maximum Cl (°)
6
Cd at zero lift
0.005994
Cm at zero angle
-0.101
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…