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SIKORSKY SSC-A09 AIRFOIL

Cambered · 9% thick · low-to-mid Re
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PROFILESIKORSKY SSC-A09 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.0% @ 37%c
max camber1.2% @ 18%c
LE radius0.89%c
area upper / chord0.0396
area lower / chord-0.0237
area camber / chord0.0079
TE thickness0.32%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7526-50.16673.3331.08611.672.00520ClAngle 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 0.01166% of chord; maximum error 0.02922%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
126
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006692
Maximum Cl
1.776
Angle at maximum Cl (°)
16
Cd at zero lift
0.006721
Cm at zero angle
-0.006939
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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