Airfoils.Pro
database / S/SC series / S8064
CAMBEREDS/SC SERIESSELIG-DATABASE

S8064

Cambered · 12% thick · low-to-mid Re
Compare↓ Download
PROFILES8064
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.3% @ 39%c
max camber1.2% @ 53%c
LE radius1.68%c
area upper / chord0.0502
area lower / chord-0.0342
area camber / chord0.0080
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6375-5-0.036293.3330.564911.671.16620ClAngle 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 0.01434% of chord; maximum error 0.05948%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
115.4
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006548
Maximum Cl
1.016
Angle at maximum Cl (°)
8
Cd at zero lift
0.006569
Cm at zero angle
-0.03366
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…