Airfoils.Pro
database / Gottingen / GOE 342 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 342 AIRFOIL

Cambered · 5% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 342 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness5.4% @ 20%c
max camber6.2% @ 40%c
LE radius0.32%c
area upper / chord0.0620
area lower / chord0.0239
area camber / chord0.0430
TE thickness0.30%c
DOWNLOAD COORDINATES

Polars

Preliminary
Combined estimate
-0.04926-50.54423.3331.13811.671.73120ClAngle of attack (°)
Why this curve

This curve combines the stored NeuralFoil prediction with 0 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 0.07595% of chord; maximum error 0.3657%.

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

Curve summary

Combined estimate · Within -5° to 20°

Maximum lift / drag
174.5
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006372
Maximum Cl
1.583
Angle at maximum Cl (°)
7
Cd at zero lift
—
Cm at zero angle
-0.1669
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…