Hi,
I am trying to analyze the stress intensity factor (SIF) using contour integral of a 2D thick walled cylinder under plane stress with different wall ratios under internal pressure loading only and a single radial crack of varying length in Abaqus.
The wall ratio (inner & outer radius) I am interested in modelling is of ratio 6 (i.e. for inner radius of 1, outer radius is 6).
I have modelled ratios from 1-6 with crack length varying from 0.1-0.9 of the wall thickness. (i.e. for ratio 3, the wall thickness is 2, hence the crack varies from 0.1-0.9 x 2).
What I have discovered:
- for ratios (<5) the SIF at the crack tip monotonically increases as crack extends from 0.1-0.9 of the wall thickness.
- for ratios (>5) the SIF at the crack tip decreases as crack length extends from 0.1-0.6, and increases later on from crack length 0.7-0.9.
- the stress distribution for ratio (<5), the max stress always occur at the crack tip leading to the increase in SIF as crack extends.
- the stress distribution for ratio (>5), the max stress do not always occur at the crack tip but at the sometimes at the inner wall leading to a decrease in SIF but later on occurring at the crack tip as crack extends.
I have compared my results obtain with published literature for ratios (1-3) and are in good agreement (less than 2%). But there is no published data for ratios (>3) and I require the results for larger ratios.
I believe thre isn't any issue with my modelling procedure since I obtained results that are in good agreement for ratios (1-3) but however, I cannot explain why the issue of maximum stress not occurring at the crack tip for larger ratios. I applied a triangular mesh at the crack front converging at the crack tip and quad mesh on the remaining geometry.
So my questions are:
- Has anyone ever encountered a situation where SIF decreases with increasing crack length even though all other parameters remained the same?
- Is a decrease in SIF unreasonable? Because, in theory it should increase with crack length when stress remain constant.
- Why is the max stress not always occurring at the crack tip in the modelled and instead on the inner wall surface for ratios (>5).
Any advice/input/recommendation would be greatly appreciated. I can upload my model if required and can also be contacted through email at ianlau11 [at] gmail.com
Kind regards,
Ian