4.4 Article

The impact of modeling choices on the assessment of Ni-Ti fatigue properties through surrogate specimens

Publisher

WILEY
DOI: 10.1002/cnm.3753

Keywords

diamond-like specimen; finite element; self-expanding device; superelasticity

Ask authors/readers for more resources

The implantation of self-expandable Ni-Ti stents is a well-established medical practice for treating peripheral diseases. However, there is an open issue regarding the fatigue characterization of these devices, as reported failures in clinics have occurred. One common method for calculating the fatigue limit of Ni-Ti involves using surrogate specimens with simplified geometries to replicate the strain distributions of the final device. This study investigates how different choices in model preparation, such as mesh refinement and element formulation, affect the output of fatigue analysis.
The implant of self-expandable Ni-Ti stents for the treatment of peripheral diseases has become an established medical practice. However, the reported failure in clinics highlights the open issue of the fatigue characterization of these devices. One of the most common approaches for calculating the Ni-Ti fatigue limit (commonly defined in terms of mean and alternate strain for a fixed number of cycles) consists of using surrogate specimens which replicate the strain distributions of the final device but in simplified geometries. The main drawback lies in the need for computational models to determine the local distribution and, hence, interpret the experimental results. This study aims at investigating the role of different choices in the model preparation, such as the mesh refinement and the element formulation, on the output of the fatigue analysis. The analyses show a strong dependency of the numerical results on modeling choices. The use of linear reduced elements enriched by a layer of membrane elements is successful to increase the accuracy of the results, especially when coarser meshes are used. Due to material nonlinearity and stent complex geometries, for the same loading conditions and element type, (i) different meshes result in different couples of mean and amplitude strains and (ii) for the same mesh, the position of the maximum mean strain is not coincident with the maximum amplitude, making difficult the selection of the limit values.

Authors

I am an author on this paper
Click your name to claim this paper and add it to your profile.

Reviews

Primary Rating

4.4
Not enough ratings

Secondary Ratings

Novelty
-
Significance
-
Scientific rigor
-
Rate this paper

Recommended

No Data Available
No Data Available