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CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 101 AIRFOIL

Cambered · 7% thick · low-to-mid Re
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PROFILEGOE 101 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.9% @ 30%c
max camber4.0% @ 31%c
LE radius0.52%c
area upper / chord0.0477
area lower / chord0.0040
area camber / chord0.0258
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.3286-50.28093.3330.890311.671.520ClAngle 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 0.04996% of chord; maximum error 0.2842%.

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
155.1
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005824
Maximum Cl
1.347
Angle at maximum Cl (°)
8
Cd at zero lift
0.006166
Cm at zero angle
-0.08238
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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