| Literature DB >> 26184329 |
Mauro Ferraro1, Ferdinando Auricchio2, Elisa Boatti3, Giulia Scalet4, Michele Conti5, Simone Morganti6, Alessandro Reali7,8.
Abstract
Computer-based simulations are nowadays widely exploited for the prediction of the mechanical behavior of different biomedical devices. In this aspect, structural finite element analyses (FEA) are currently the preferred computational tool to evaluate the stent response under bending. This work aims at developing a computational framework based on linear and higher order FEA to evaluate the flexibility of self-expandable carotid artery stents. In particular, numerical simulations involving large deformations and inelastic shape memory alloy constitutive modeling are performed, and the results suggest that the employment of higher order FEA allows accurately representing the computational domain and getting a better approximation of the solution with a widely-reduced number of degrees of freedom with respect to linear FEA. Moreover, when buckling phenomena occur, higher order FEA presents a superior capability of reproducing the nonlinear local effects related to buckling phenomena.Entities:
Keywords: carotid artery stents; finite element analysis; shape memory alloys; stent flexibility
Year: 2015 PMID: 26184329 PMCID: PMC4598672 DOI: 10.3390/jfb6030585
Source DB: PubMed Journal: J Funct Biomater ISSN: 2079-4983
Figure 1Stent model generation: (a) detail of a high resolution micro-CT performed on the real stents within the delivery system; (b) planar CAD geometry reproducing the stent design pattern; (c) 3D CAD stent model; (d) h- (top) and p- (bottom) finite element analysis (FEA) mesh generation.
Figure 2Stent refinement levels: top p-FEA; bottom h-FEA.
Stent bending analyses: the relative errors are evaluated with respect to the finest P-FEA simulation, labeled as P-FEA-4. The symbols p, q and r indicate the circumferential, longitudinal and thickness polynomial orders of the FEA meshes, respectively.
| Mesh Label | DOF | Order | Reaction Force (N) | Critical Load (N) | ||||
|---|---|---|---|---|---|---|---|---|
| FEA-1 | 606,276 | 1 | 1 | 1 | 1.0102 | 60.21% | 1.3354 | 47.76 % |
| FEA-2 | 1,635,960 | 1 | 1 | 1 | 0.91935 | 51.85% | 1.1671 | 29.14 % |
| FEA-3 | 2,118,096 | 1 | 1 | 1 | 0.89916 | 42.60 % | 1.1300 | 25.03 % |
| FEA-4 | 3,246,480 | 1 | 1 | 1 | 0.79611 | 26.25 % | 1.0754 | 18.99 % |
| FEA-5 | 5,281,740 | 1 | 1 | 1 | 0.73349 | 16.32 % | 0.99991 | 10.64 % |
| FEA-6 | 10,622,016 | 1 | 1 | 1 | 0.68897 | 9.26 % | 0.97022 | 7.35 % |
| p-FEA-1 | 598,212 | 3 | 3 | 2 | 0.7725 | 22.51 % | 1.0342 | 14.31 % |
| p-FEA-2 | 1,844,820 | 3 | 3 | 2 | 0.6732 | 6.76% | 0.9544 | 5.49 % |
| p-FEA-3 | 3,469,668 | 3 | 3 | 2 | 0.6480 | 2.76 % | 0.91242 | 0.8 % |
| p-FEA-4 | 5,269,642 | 3 | 3 | 2 | 0.63054 | – | 0.90473 | – |
Figure 3Force-displacement diagrams for shape memory alloy (SMA) stent bending: (a) FEA; (b) p-FEA; (c) reaction force convergence plot.
Figure 4FEA versus p-FEA comparison: (a) force displacement curves obtained using the finest FEA mesh (FEA-8) and a coarse p-FEA mesh (p-FEA-2); (b) p-FEA-2 deformed configuration; (c) FEA-8 deformed configuration.
Computational times for p-FEA and h-FEA.
| Mesh Label | DOF | No. of CPUs | Solver | Total Analysis Time |
|---|---|---|---|---|
| p-FEA-2 | 1,844,820 | 1 | FEAP | 27 h 15 min |
| FEA-6 | 10,622,016 | 8 | Abaqus/Standard | 26 h 23 min |