Airfoils.Pro
database / Gottingen / GOE 55 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 55 AIRFOIL

Cambered · 6% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 55 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.2% @ 15%c
max camber2.0% @ 20%c
LE radius0.42%c
area upper / chord0.0303
area lower / chord-0.0054
area camber / chord0.0124
TE thickness0.75%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6406-50.29383.3331.22811.672.16320ClAngle 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.

Geometry fit: RMS error 0.0554% of chord; maximum error 0.2738%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
136.4
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006917
Maximum Cl
1.929
Angle at maximum Cl (°)
17
Cd at zero lift
0.006941
Cm at zero angle
-0.03061
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…