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S/SC SERIESSELIG-DATABASESYMMETRIC

S9026 (9.5%)

Symmetric · 9% thick · low-to-mid Re
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PROFILES9026 (9.5%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.5% @ 27%c
max camber0.0% @ 0%c
LE radius0.99%c
area upper / chord0.0309
area lower / chord-0.0309
area camber / chord0.0000
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.8027-50.10643.3331.01511.671.92520ClAngle 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 0.01055% of chord; maximum error 0.03663%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
123.7
Angle at maximum lift / drag (°)
11
Minimum Cd
0.006667
Maximum Cl
1.697
Angle at maximum Cl (°)
17
Cd at zero lift
0.006667
Cm at zero angle
3.432e-17
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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