Airfoils.Pro
database / Gottingen / GOE 611 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 611 AIRFOIL

Cambered · 13% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 611 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness12.9% @ 30%c
max camber5.8% @ 39%c
LE radius1.83%c
area upper / chord0.0844
area lower / chord-0.0056
area camber / chord0.0394
TE thickness0.65%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.07087-50.60763.3331.28611.671.96520ClAngle 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.

The compressibility correction is a low-fidelity estimate, not a resolved shock or compressible CFD solution.

Geometry fit: RMS error 0.07746% of chord; maximum error 0.3472%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
152.1
Angle at maximum lift / drag (°)
7
Minimum Cd
0.007169
Maximum Cl
1.795
Angle at maximum Cl (°)
10
Cd at zero lift
—
Cm at zero angle
-0.135
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…