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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 802 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEGOE 802 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.8% @ 30%c
max camber6.2% @ 39%c
LE radius1.06%c
area upper / chord0.0760
area lower / chord0.0074
area camber / chord0.0417
TE thickness0.40%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1081-50.56043.3331.22911.671.89720ClAngle 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 0.06815% of chord; maximum error 0.3912%.

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
144.7
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007426
Maximum Cl
1.73
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.1389
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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