Airfoils.Pro
database / Gottingen / GOE 384 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 384 AIRFOIL

Cambered · 20% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 384 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness19.5% @ 30%c
max camber6.9% @ 39%c
LE radius4.21%c
area upper / chord0.1101
area lower / chord-0.0207
area camber / chord0.0447
TE thickness0.43%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.02855-50.61783.3331.26411.671.91120ClAngle 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 0.07483% of chord; maximum error 0.3295%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
121.2
Angle at maximum lift / drag (°)
5
Minimum Cd
0.007975
Maximum Cl
1.749
Angle at maximum Cl (°)
11
Cd at zero lift
—
Cm at zero angle
-0.1398
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…