Airfoils.Pro
database / Gottingen / GOE 590 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 590 AIRFOIL

Cambered · 6% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 590 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.7% @ 30%c
max camber4.0% @ 30%c
LE radius0.36%c
area upper / chord0.0423
area lower / chord0.0023
area camber / chord0.0223
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4412-50.15193.3330.74511.671.33820ClAngle 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 0.04528% of chord; maximum error 0.1765%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
143.7
Angle at maximum lift / drag (°)
6
Minimum Cd
0.005723
Maximum Cl
1.19
Angle at maximum Cl (°)
8
Cd at zero lift
0.005884
Cm at zero angle
-0.04535
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…