Airfoils.Pro
database / Gottingen / GOE 174 (ALBATROS
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 174 (ALBATROS

Cambered · 9% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 174 (ALBATROS
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.6% @ 20%c
max camber5.6% @ 39%c
LE radius0.81%c
area upper / chord0.0651
area lower / chord0.0083
area camber / chord0.0367
TE thickness0.29%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.1191-50.52863.3331.17611.671.82420ClAngle 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 0.05581% of chord; maximum error 0.2226%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
165
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006332
Maximum Cl
1.662
Angle at maximum Cl (°)
9
Cd at zero lift
—
Cm at zero angle
-0.1314
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…