| Literature DB >> 35067825 |
Joan D Laubrie1, S Jamaleddin Mousavi1, Stéphane Avril2,3.
Abstract
Evolution of mechanical and structural properties in the Ascending Thoracic Aorta (ATA) is the results of complex mechanobiological processes. In this work, we address some numerical challenges in order to elaborate computational models of these processes. For that, we extend the state of the art of homogenized constrained mixture (hCM) models. In these models, prestretches are assigned to the mixed constituents in order to ensure local mechanical equilibrium macroscopically, and to maintain a homeostatic level of tension in collagen fibers microscopically. Although the initial prestretches were assumed as homogeneous in idealized straight tubes, more elaborate prestretch distributions need to be considered for curved geometrical models such as patient-specific ATA. Therefore, we introduce prestretches having a three-dimensional gradient across the ATA geometry in the homeostatic reference state. We test different schemes with the objective to ensure stable growth and remodeling (G&R) simulations on patient-specific curved vessels. In these simulations, aneurysm progression is triggered by tissue changes in the constituents such as mass degradation of intramural elastin. The results show that the initial prestretches are not only critical for the stability of numerical simulations, but they also affect the G&R response. Eventually, we submit that initial conditions required for G&R simulations need to be identified regionally for ensuring realistic patient-specific predictions of aneurysm progression.Entities:
Keywords: Arterial growth and remodeling; Finite element method; Homogenized constrained mixture model; Layer-specific behavior; Prestretch; patient-specific
Mesh:
Year: 2022 PMID: 35067825 PMCID: PMC8940846 DOI: 10.1007/s10237-021-01544-3
Source DB: PubMed Journal: Biomech Model Mechanobiol ISSN: 1617-7940
Fig. 1Schematic of the hCM model, showing the different configurations. The reference configuration is reconstructed from the actual in vivo geometry of the artery. The configuration is obtained by applying the initial boundary conditions and by assigning initial prestretches to each constituent of . and should be the same as there should be equilibrium between the effects of the initial boundary conditions and the effects of the initial prestretches in the reference configuration. However, both are represented separately in the figure as the initial prestretches providing this equilibrium are found iteratively in our approach. The fictitious traction-free configuration is defined as a fictitious configuration at time t, without the effects of boundary conditions and of prestretches. The current configuration is obtained after equilibrium between the effects of the current boundary conditions and the effects of the updated prestretches obtained after growth and remodeling. The neighborhood of an arbitrary point in is related to by the transformation . At time zero, and . Similarly, the relationship between and the natural configuration is , and the natural configuration and are related by the inelastic deformation where the inelastic deformation evolves with time. The natural configurations can only be defined locally but are not compatible
Fig. 2a Lateral view of a cylinder with its diameter d and the cylindrical system () with perpendicular to the sheet. b Lateral and cross-sectional views of the idealized toric ATA model, where the luminal diameter is , the arch radius is R (middle curvature) and the total wall thickness is t. IC = inner curvature and OC = outer curvature of the arch; a linear gradient is assigned for the axial () and circumferential () prestretch of elastin in the reference homeostatic state. The torus is represented with the spherical coordinate system () with perpendicular to the sheet. c Schematic of the boundary conditions, with springs at the proximal () and at the distal () ends; the circle (with radius ) indicates the insult zone where a localized degradation of elastin is applied; the diameter d and the thickness along the same line are used to assess the initial distortions and displacements during the simulations. d Reconstructed geometry of the patient-specific aorta from the CT scan. In a and b, the media is filled with north west lines and the adventitia with north east lines, in c the media is filled with dots and the adventitia with vertical black thick lines
Fig. 3Flowchart for the homeostatic prestretch algorithm, showing how the prestretch gradient is found iteratively by solving forward FE problems successively. In the forward FE model, the prestretch gradient is held constant. After each forward analysis, the axial prestretch gradient () is updated if the thickness distortion () is larger than the thickness tolerance (), or the circumferential prestretch gradient () is updated if the diameter distortion () is larger than the diameter tolerance () (Maas et al. 2016)
Mechanical parameters used to verify our model against the results of Braeu et al. (2017) for the development of an aneurysm in an idealized cylindrical geometry
| Symbol | Value | |
|---|---|---|
| Radius | 10mm | |
| Length | 90mm | |
| Thickness | 1.41mm | |
| Pressure | 100mmHg | |
| Neo-Hookean | 72J/kg | |
| Bulk-modulus | 100 | |
| Fung-quadratic, collagen | 568J/kg | |
| 11.2 | ||
| Passive, SMC | 7.6J/kg | |
| 11.4 | ||
| Active, SMC | 54kPa | |
| 0.8 | ||
| 1.4 | ||
| 1.0 | ||
| Elastin | 241.5kg/m | |
| SMC | 157.5kg/m | |
| Collagen(0 and | 65.1kg/m | |
| Collagen( | 241.5kg/m | |
| Elastin longitudinal | ||
| Elastin circumferential | ||
| SMC | ||
| Collagen | ||
| Collagen and SMC | 101days | |
| Elastin | 101years | |
Fig. 4Evolution of the maximum radius for the cylinder benchmark case. 4 comparison between the radius predicted by our model (solid lines) with the three-dimensional model (dashed lines) of Braeu et al. (2017). 4 comparison between the radius predicted by our model (solid lines) with the membrane hCM model of Braeu et al. (2017)
Comparison of our results with results from (Braeu et al. 2017) for the development of an aneurysm in an idealized cylindrical geometry following an initial insult (localized elastin degradation)
| Literature (Braeu et al. | This work | Error | |||||
|---|---|---|---|---|---|---|---|
| Minimum | Maximum | Minimum | Maximum | Minimum (%) | Maximum (%) | ||
| Stress | 80kPa | 320kPa | 44kPa | 291kPa | – 45 | – 9 | |
| 80kPa | 120kPa | 95kPa | 105kPa | 19 | – 12 | ||
| Collagen | 0.8 | 6.1 | 0.73 | 5.03 | – 9 | – 18 | |
| 1.0 | 1.6 | 1.00 | 1.44 | 0 | – 10 | ||
Gain-parameter and turnover time from the equation of rate mass degradation and deposition (details in supplemental materials, section C)
Material parameters used in our models to simulate G&R in an idealized toric aortic arch and in a patient-specific ATA geometry
| Symbol | Value | |
|---|---|---|
| Thickness | 2.38mm | |
| Pressure | 80mmHg | |
| Neo-Hookean | 80J/kg | |
| Bulk modulus | ||
| Fung-quadratic, collagen | 292.0J/kg | |
| 5.6 | ||
| Passive, SMC | 13.8J/kg | |
| 6.0 | ||
| Elastin | 169.0kg/m | |
| SMC | 735.0kg/m | |
| Collagen (0 and | 14.6kg/m | |
| Collagen ( | 58.4kg/m | |
| Elastin | 565.0kg/m | |
| SMC | 0.0kg/m | |
| Collagen (0 and | 48.5kg/m | |
| Collagen ( | 194.0kg/m | |
| SMC | ||
| Collagen | ||
| Turnover period | ||
| Collagen and SMC | 101days | |
| Elastin | 101years | |
The parameters are introduced with their respective models in the supplemental material, section B
Fig. 5Diameter (a) and thickness (b) evolution in the idealized ATA geometry in response to half-life elastin degradation. Diameter (c) and thickness (d) evolution of the idealized ATA in response to an initial insult (sharp elastin degradation).
Fig. 6Von Mises stress () evolution in response to half-life elastin degradation (a) and in response to an initial insult (sharp elastin degradation) (b) for the idealized ATA geometry. Normalized total collagen density () evolution in response to long-term elastin degradation (c) and localized elastin loss (d) for the idealized ATA geometry. Simulations were achieved with
Fig. 7Diameter (a) and thickness (b) evolution in the patient-specific ATA geometry in response to half-life elastin degradation. Diameter (c) and thickness (d) evolution of the patient-specific ATA in response to an initial insult (sharp elastin degradation)
Fig. 8Von Mises stress () evolution in response to half-life elastin degradation (a) and in response to an initial insult (sharp elastin degradation) (b) for the patient-specific ATA geometry. Normalized total collagen density () evolution in response to long-term elastin degradation (c) and localized elastin loss (d) for the patient-specific ATA geometry. Simulations were achieved with