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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 505 AIRFOIL

Cambered · 14% thick · low-to-mid Re
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PROFILEGOE 505 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness14.0% @ 20%c
max camber5.9% @ 40%c
LE radius2.15%c
area upper / chord0.0890
area lower / chord-0.0131
area camber / chord0.0379
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1527-50.47463.3331.10211.671.72920ClAngle 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 0.068% of chord; maximum error 0.3555%.

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
116.3
Angle at maximum lift / drag (°)
8
Minimum Cd
0.007121
Maximum Cl
1.572
Angle at maximum Cl (°)
12
Cd at zero lift
—
Cm at zero angle
-0.09962
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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