Airfoils.Pro
database / Gottingen / GOE 617 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 617 AIRFOIL

Cambered · 14% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 617 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.8% @ 30%c
max camber2.2% @ 31%c
LE radius2.11%c
area upper / chord0.0617
area lower / chord-0.0340
area camber / chord0.0139
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5399-50.065513.3330.67111.671.27620ClAngle 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 0.06088% of chord; maximum error 0.2932%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
120.5
Angle at maximum lift / drag (°)
7
Minimum Cd
0.00692
Maximum Cl
1.125
Angle at maximum Cl (°)
9
Cd at zero lift
0.006924
Cm at zero angle
-0.03132
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…