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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 408 AIRFOIL

Cambered · 8% thick · low-to-mid Re
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PROFILEGOE 408 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.8% @ 30%c
max camber4.1% @ 30%c
LE radius0.66%c
area upper / chord0.0561
area lower / chord-0.0008
area camber / chord0.0276
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.2694-50.30893.3330.887211.671.46620ClAngle 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 0.06415% of chord; maximum error 0.2714%.

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
146.3
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006249
Maximum Cl
1.321
Angle at maximum Cl (°)
8
Cd at zero lift
0.007704
Cm at zero angle
-0.08449
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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