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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 92 AIRFOIL

Cambered · 9% thick · low-to-mid Re
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PROFILEGOE 92 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.8% @ 30%c
max camber5.5% @ 30%c
LE radius0.85%c
area upper / chord0.0657
area lower / chord0.0071
area camber / chord0.0364
TE thickness0.16%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.1896-50.50253.3331.19511.671.88720ClAngle 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 0.05453% of chord; maximum error 0.3011%.

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
161.1
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006353
Maximum Cl
1.714
Angle at maximum Cl (°)
10
Cd at zero lift
0.008908
Cm at zero angle
-0.1046
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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