Airfoils.Pro
database / Eppler / E502
CAMBEREDEPPLERSELIG-DATABASETHICK

E502

Cambered · 16% thick · low-to-mid Re
Compare↓ Download
PROFILEE502
surfacecamber line
GEOMETRY · AREA METRICS
max thickness15.7% @ 43%c
max camber1.5% @ 34%c
LE radius2.70%c
area upper / chord0.0608
area lower / chord-0.0428
area camber / chord0.0090
TE thickness0.00%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.6303-50.022063.3330.674511.671.32720ClAngle 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 0.02638% of chord; maximum error 0.05647%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
119.2
Angle at maximum lift / drag (°)
7
Minimum Cd
0.006873
Maximum Cl
1.164
Angle at maximum Cl (°)
9
Cd at zero lift
0.006877
Cm at zero angle
-0.02096
CFD points
SOLVER WORK0 conditions · 0 engine jobs
Loading solver work…