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CAMBEREDSELIG-DATABASESG SERIESTHICK

SG6050

Cambered · 16% thick · low-to-mid Re
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PROFILESG6050
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.0% @ 32%c
max camber3.2% @ 46%c
LE radius2.83%c
area upper / chord0.0747
area lower / chord-0.0334
area camber / chord0.0207
TE thickness1.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4005-50.28493.3330.970211.671.65620ClAngle 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 0.02424% of chord; maximum error 0.07887%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
136.9
Angle at maximum lift / drag (°)
7
Minimum Cd
0.007321
Maximum Cl
1.484
Angle at maximum Cl (°)
9
Cd at zero lift
0.007333
Cm at zero angle
-0.0977
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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