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S/SC SERIESSELIG-DATABASESYMMETRICTHICK

S1014

Symmetric · 17% thick · low-to-mid Re
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PROFILES1014
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.5% @ 42%c
max camber0.0% @ 0%c
LE radius3.00%c
area upper / chord0.0571
area lower / chord-0.0571
area camber / chord0.0000
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.763-50.043063.3330.849211.671.65520ClAngle 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 0.03367% of chord; maximum error 0.07166%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
100.9
Angle at maximum lift / drag (°)
10
Minimum Cd
0.008036
Maximum Cl
1.454
Angle at maximum Cl (°)
17
Cd at zero lift
0.008036
Cm at zero angle
-5.719e-17
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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