This page presents the S-N curves and fatigue limit of CX steel samples that underwent shot-peening, heat treatment and machining that removed allowance of 0.5mm (in that order), obtained using the bending tests of rotating bars with AM layers parallel to the axis of rotation.
| Build orientation of longitudinal axis | horizontal |
|---|---|
| Position with respect to inert gas flow | undefined |
| Post-processing | shot-peening → heat treatment → machining allowance 0.5mm |
| Fatigue limit (MPa) | 503 |
|---|---|
| Stress amplitude S (MPa) | S=5005⋅N<html>-0,147</html> |
| Number of cycles to failure N | N=1,47⋅10<html>25</html>⋅S<html>-6,80</html> |
Explanation of the terms are given at the page Fatigue strength description.
This page is a part of the section DMLS/SLM: Fatigue design rules.