Airfoils.Pro
database / S/SC series / S4083 (8%)
CAMBEREDS/SC SERIESSELIG-DATABASETHIN

S4083 (8%)

Cambered · 8% thick · low-to-mid Re
Compare↓ Download
PROFILES4083 (8%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.0% @ 23%c
max camber3.5% @ 35%c
LE radius0.70%c
area upper / chord0.0488
area lower / chord-0.0003
area camber / chord0.0242
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2837-50.32553.3330.934811.671.54420ClAngle 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 0.01378% of chord; maximum error 0.05073%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
157.4
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005934
Maximum Cl
1.392
Angle at maximum Cl (°)
8
Cd at zero lift
0.006007
Cm at zero angle
-0.1024
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…