Airfoils.Pro
database / Gottingen / GOE 79 (PFALZ
CAMBEREDGOTTINGENSELIG-DATABASETHIN

GOE 79 (PFALZ

Cambered · 6% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 79 (PFALZ
surfacecamber line
GEOMETRY · AREA METRICS
max thickness6.2% @ 15%c
max camber6.0% @ 30%c
LE radius0.42%c
area upper / chord0.0604
area lower / chord0.0182
area camber / chord0.0393
TE thickness0.56%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1382-50.47383.3331.08611.671.69820ClAngle 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 0.07562% of chord; maximum error 0.3496%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
165.7
Angle at maximum lift / drag (°)
5
Minimum Cd
0.006663
Maximum Cl
1.545
Angle at maximum Cl (°)
7
Cd at zero lift
—
Cm at zero angle
-0.1247
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…