Airfoils.Pro
database / Gottingen / GOE 535 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 535 AIRFOIL

Cambered · 16% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 535 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.1% @ 29%c
max camber5.8% @ 50%c
LE radius2.84%c
area upper / chord0.0884
area lower / chord-0.0074
area camber / chord0.0405
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.01106-50.62113.3331.25311.671.88520ClAngle 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 0.07293% of chord; maximum error 0.3264%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
149.5
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007327
Maximum Cl
1.727
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.154
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…