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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 595 AIRFOIL

Cambered · 10% thick · low-to-mid Re
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PROFILEGOE 595 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness9.5% @ 30%c
max camber3.0% @ 40%c
LE radius1.00%c
area upper / chord0.0543
area lower / chord-0.0119
area camber / chord0.0212
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.3589-50.24243.3330.843711.671.44520ClAngle 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 0.04527% of chord; maximum error 0.2409%.

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
143.5
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006232
Maximum Cl
1.295
Angle at maximum Cl (°)
8
Cd at zero lift
0.006299
Cm at zero angle
-0.08388
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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