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CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 770 AIRFOIL

Cambered · 21% thick · low-to-mid Re
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PROFILEGOE 770 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness21.0% @ 30%c
max camber4.0% @ 30%c
LE radius4.85%c
area upper / chord0.0922
area lower / chord-0.0417
area camber / chord0.0253
TE thickness0.26%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.4474-50.2953.3331.03711.671.7820ClAngle 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 0.07695% of chord; maximum error 0.3324%.

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
115.9
Angle at maximum lift / drag (°)
7
Minimum Cd
0.00789
Maximum Cl
1.594
Angle at maximum Cl (°)
11
Cd at zero lift
0.007891
Cm at zero angle
-0.04898
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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