Airfoils.Pro
database / Gottingen / GOE 498 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 498 AIRFOIL

Cambered · 16% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 498 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.9% @ 29%c
max camber5.5% @ 49%c
LE radius2.79%c
area upper / chord0.0885
area lower / chord-0.0127
area camber / chord0.0379
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
0.005651-50.61153.3331.21711.671.82320ClAngle 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 0.06476% of chord; maximum error 0.2899%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
151.4
Angle at maximum lift / drag (°)
6
Minimum Cd
0.007376
Maximum Cl
1.672
Angle at maximum Cl (°)
8
Cd at zero lift
—
Cm at zero angle
-0.1713
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…