Airfoils.Pro
database / Gottingen / GOE 797 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASETHICK

GOE 797 AIRFOIL

Cambered · 16% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 797 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness16.0% @ 30%c
max camber5.0% @ 40%c
LE radius2.82%c
area upper / chord0.0903
area lower / chord-0.0224
area camber / chord0.0339
TE thickness0.80%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.2585-50.443.3331.13911.671.83720ClAngle 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 0.1076% of chord; maximum error 0.4139%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
123.8
Angle at maximum lift / drag (°)
7
Minimum Cd
0.008114
Maximum Cl
1.662
Angle at maximum Cl (°)
10
Cd at zero lift
0.008322
Cm at zero angle
-0.126
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…