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SIKORSKY SC2110 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILESIKORSKY SC2110 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.9% @ 37%c
max camber2.0% @ 15%c
LE radius1.08%c
area upper / chord0.0475
area lower / chord-0.0229
area camber / chord0.0123
TE thickness0.36%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7051-50.21583.3331.13711.672.05820ClAngle 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.

Geometry fit: RMS error 0.01822% of chord; maximum error 0.08875%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
130.3
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006842
Maximum Cl
1.827
Angle at maximum Cl (°)
16
Cd at zero lift
0.006844
Cm at zero angle
-0.00995
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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