Airfoils.Pro
database / Gottingen / GOE 432 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 432 AIRFOIL

Cambered · 8% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 432 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.7% @ 21%c
max camber4.3% @ 39%c
LE radius0.65%c
area upper / chord0.0551
area lower / chord0.0041
area camber / chord0.0296
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.2587-50.32453.3330.907611.671.49120ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 1 contributing CFD observations. History windows remain observations, not separate solver runs or automatically converged points.

Model uncertainty is conditional on the stated assumptions and has not been calibrated for this condition. It is not a validated accuracy guarantee.

Geometry fit: RMS error 0.05361% of chord; maximum error 0.258%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10 · Polar model progressive-polar-gp-v2

  • · Converged

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
58.49
Angle at maximum lift / drag (°)
6
Minimum Cd
0.01611
Maximum Cl
1.345
Angle at maximum Cl (°)
8
Cd at zero lift
0.01686
Cm at zero angle
-0.08307
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…