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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 195 AIRFOIL

Cambered · 9% thick · low-to-mid Re
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PROFILEGOE 195 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.6% @ 20%c
max camber5.1% @ 50%c
LE radius0.81%c
area upper / chord0.0608
area lower / chord0.0082
area camber / chord0.0345
TE thickness0.20%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1058-50.48243.3331.07111.671.65920ClAngle 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 0.05991% of chord; maximum error 0.3014%.

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
162.8
Angle at maximum lift / drag (°)
5
Minimum Cd
0.0063
Maximum Cl
1.512
Angle at maximum Cl (°)
7
Cd at zero lift
—
Cm at zero angle
-0.1553
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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