What is it about?
We create a number of example geometries to represent a test specimen. The surface is represented with a roughened profile, and a number of randomly positioned pores are included in the subsurface. A loading cycle is defined and the stresses arising from those loads are calculated for each geometry. The nominal stress level, being the level that would be seen in a similar geometry but with a perfectly smooth surface and no porosity, is set to be below the stress level for material failure, but the presence of roughness or porosity leads to localised regions that have higher stresses. These stresses cause localised plastic yielding, and on repeated loading, this yield develops. We compare the effects of surface roughness, different pore sizes and the proximity of pores, to understand how certain arrangements can be more detrimental than others.
Featured Image
Photo by John McArthur on Unsplash
Why is it important?
The way in which multiple load cycles leads to component failure is known as "fatigue". While fatigue is a well-known problem, and there are well defined testing strategies to determine the fatigue life of an engineering component, these tests are expensive to perform, and the cost of fatigue testing, and the necessary time needed to carry out that testing, is a major obstacle to the efficient design of high duty components. We are doing this work to obtain a phenomenological understanding, which should - eventually - mean that cheaper and shorter measurement and test programmes can be developed.
Perspectives
Read the Original
This page is a summary of: Combined effect of both surface finish and sub‐surface porosity on component strength under repeated load conditions, Engineering Reports, August 2020, Wiley,
DOI: 10.1002/eng2.12248.
You can read the full text:
Contributors
The following have contributed to this page