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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 767 AIRFOIL

Cambered · 12% thick · low-to-mid Re
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PROFILEGOE 767 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.0% @ 20%c
max camber1.5% @ 20%c
LE radius1.59%c
area upper / chord0.0437
area lower / chord-0.0298
area camber / chord0.0070
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.7224-50.18253.3331.08711.671.99220ClAngle 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 0.05916% of chord; maximum error 0.3229%.

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
129.2
Angle at maximum lift / drag (°)
11
Minimum Cd
0.006994
Maximum Cl
1.766
Angle at maximum Cl (°)
17
Cd at zero lift
0.006999
Cm at zero angle
0.001398
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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