Airfoils.Pro
database / Gottingen / GOE 575 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 575 AIRFOIL

Cambered · 13% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 575 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness13.3% @ 30%c
max camber3.6% @ 39%c
LE radius1.96%c
area upper / chord0.0760
area lower / chord-0.0266
area camber / chord0.0247
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.5296-50.12883.3330.787211.671.44620ClAngle 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 0.07682% of chord; maximum error 0.2804%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
109.3
Angle at maximum lift / drag (°)
8
Minimum Cd
0.007743
Maximum Cl
1.281
Angle at maximum Cl (°)
10
Cd at zero lift
0.007796
Cm at zero angle
-0.02551
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…