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 angle 45° to the axis of rotation.
Build orientation of longitudinal axis | angle 45° |
---|---|
Position with respect to inert gas flow | undefined |
Post-processing | shot-peening → heat treatment → machining allowance 0.5mm |
Fatigue limit (MPa) | 556 |
---|---|
Number of cycles to failure N | N=7,45⋅1020⋅S-5,13 |
Stress amplitude S (MPa) | S=11750⋅N-0,195 |
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.