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CAMBEREDOTHER FAMILIESSELIG-DATABASE

GIIIL

Cambered · 9% thick · low-to-mid Re
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PROFILEGIIIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.5% @ 35%c
max camber1.6% @ 25%c
LE radius0.80%c
area upper / chord0.0390
area lower / chord-0.0199
area camber / chord0.0095
TE thickness0.04%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.6701-50.22573.3331.12111.672.01720ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.02717% of chord; maximum error 0.1203%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
133.7
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006381
Maximum Cl
1.793
Angle at maximum Cl (°)
17
Cd at zero lift
0.006392
Cm at zero angle
-0.01699
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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