Airfoils.Pro
database / Gottingen / GOE 507 AIRFOIL
CAMBEREDGOTTINGENSELIG-DATABASE

GOE 507 AIRFOIL

Cambered · 9% thick · low-to-mid Re
Compare↓ Download
PROFILEGOE 507 AIRFOIL
surfacecamber line
GEOMETRY · AREA METRICS
max thickness8.6% @ 30%c
max camber2.9% @ 40%c
LE radius0.82%c
area upper / chord0.0488
area lower / chord-0.0113
area camber / chord0.0187
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.4748-50.35823.3331.19111.672.02420ClAngle 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 0.1026% of chord; maximum error 0.4566%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
137.6
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006653
Maximum Cl
1.816
Angle at maximum Cl (°)
16
Cd at zero lift
0.006656
Cm at zero angle
-0.06424
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…