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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 490 AIRFOIL

Cambered · 9% thick · low-to-mid Re
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PROFILEGOE 490 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.8% @ 20%c
max camber3.8% @ 39%c
LE radius0.85%c
area upper / chord0.0560
area lower / chord-0.0061
area camber / chord0.0249
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.333-50.30963.3330.952211.671.59520ClAngle 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 0.05557% of chord; maximum error 0.3017%.

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
150.5
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006209
Maximum Cl
1.434
Angle at maximum Cl (°)
9
Cd at zero lift
0.006262
Cm at zero angle
-0.08491
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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