Airfoils.Pro
database / S/SC series / S3016-095-87
CAMBEREDS/SC SERIESSELIG-DATABASE

S3016-095-87

Cambered · 10% thick · low-to-mid Re
Compare↓ Download
PROFILES3016-095-87
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.5% @ 29%c
max camber2.1% @ 38%c
LE radius1.00%c
area upper / chord0.0450
area lower / chord-0.0175
area camber / chord0.0137
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.5833-50.031383.3330.646111.671.26120ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.01659% of chord; maximum error 0.09358%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
131.9
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006062
Maximum Cl
1.107
Angle at maximum Cl (°)
8
Cd at zero lift
0.006065
Cm at zero angle
-0.03346
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…