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CAMBEREDS/SC SERIESSELIG-DATABASE

S4094 (root airfoil

Cambered · 10% thick · low-to-mid Re
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PROFILES4094 (root airfoil
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.9% @ 29%c
max camber2.4% @ 34%c
LE radius1.08%c
area upper / chord0.0506
area lower / chord-0.0193
area camber / chord0.0157
TE thickness2.48%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.5859-50.35073.3331.28711.672.22420ClAngle 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 0.0164% of chord; maximum error 0.0675%.

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
116.7
Angle at maximum lift / drag (°)
10
Minimum Cd
0.009078
Maximum Cl
1.99
Angle at maximum Cl (°)
16
Cd at zero lift
0.009084
Cm at zero angle
-0.04531
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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