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CAMBEREDS/SC SERIESSELIG-DATABASE

SIKORSKY SC1095 AIRFOIL

Cambered · 9% thick · low-to-mid Re
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PROFILESIKORSKY SC1095 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.5% @ 26%c
max camber0.8% @ 26%c
LE radius0.99%c
area upper / chord0.0383
area lower / chord-0.0274
area camber / chord0.0054
TE thickness0.35%c
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Polars

Preliminary
Combined estimate
-0.7401-50.1833.3331.10611.672.02920ClAngle 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 0.02816% of chord; maximum error 0.07852%.

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
129.4
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006816
Maximum Cl
1.798
Angle at maximum Cl (°)
17
Cd at zero lift
0.006823
Cm at zero angle
-0.01403
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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