Airfoils.Pro
database / Gottingen / GOE 515 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 515 AIRFOIL

Cambered · 8% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 515 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.4% @ 30%c
max camber2.8% @ 40%c
LE radius0.79%c
area upper / chord0.0476
area lower / chord-0.0123
area camber / chord0.0177
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4583-50.11753.3330.693411.671.26920ClAngle 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 0.05247% of chord; maximum error 0.2604%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
136.3
Angle at maximum lift / drag (°)
6
Minimum Cd
0.006095
Maximum Cl
1.125
Angle at maximum Cl (°)
7
Cd at zero lift
0.006103
Cm at zero angle
-0.06557
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…