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S1016

Symmetric · 17% thick · low-to-mid Re
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PROFILES1016
surfacecamber line
GEOMETRY · AREA METRICS
max thickness17.5% @ 41%c
max camber0.0% @ 0%c
LE radius3.37%c
area upper / chord0.0613
area lower / chord-0.0613
area camber / chord0.0000
TE thickness0.00%c
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Polars

Preliminary
NeuralFoil
-0.7749-5-0.14213.3330.490711.671.12420ClAngle 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.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.02732% of chord; maximum error 0.06816%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
98.91
Angle at maximum lift / drag (°)
7
Minimum Cd
0.007628
Maximum Cl
0.9653
Angle at maximum Cl (°)
9
Cd at zero lift
0.007628
Cm at zero angle
-1.253e-17
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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