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CAMBEREDGOTTINGENSELIG-DATABASE

GOE 766 AIRFOIL

Cambered · 12% thick · low-to-mid Re
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PROFILEGOE 766 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.0% @ 26%c
max camber1.5% @ 20%c
LE radius1.59%c
area upper / chord0.0460
area lower / chord-0.0322
area camber / chord0.0069
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.7246-50.16693.3331.05811.671.9520ClAngle of attack (°)
Why this curve

This is a NeuralFoil prediction from the stored profile coordinates and the selected flow condition, with AeroSandbox compressibility corrections. It is not a completed OpenFOAM calculation.

Prediction error has not been calibrated for this condition. No accuracy interval is claimed.

Geometry fit: RMS error 0.05767% of chord; maximum error 0.3054%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
127.8
Angle at maximum lift / drag (°)
11
Minimum Cd
0.00708
Maximum Cl
1.727
Angle at maximum Cl (°)
17
Cd at zero lift
0.007091
Cm at zero angle
0.003213
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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