| Literature DB >> 33683514 |
Alberto Coccarelli1, Jason M Carson2,3,4, Ankush Aggarwal5, Sanjay Pant2.
Abstract
We present a novel framework for investigating the role of vascular structure on arterial haemodynamics in large vessels, with a special focus on the human common carotid artery (CCA). The analysis is carried out by adopting a three-dimensional (3D) derived, fibre-reinforced, hyperelastic structural model, which is coupled with an axisymmetric, reduced order model describing blood flow. The vessel transmural pressure and lumen area are related via a Holzapfel-Ogden type of law, and the residual stresses along the thickness and length of the vessel are also accounted for. After a structural characterization of the adopted hyperelastic model, we investigate the link underlying the vascular wall response and blood-flow dynamics by comparing the proposed framework results against a popular tube law. The comparison shows that the behaviour of the model can be captured by the simpler linear surrogate only if a representative value of compliance is applied. Sobol's multi-variable sensitivity analysis is then carried out in order to identify the extent to which the structural parameters have an impact on the CCA haemodynamics. In this case, the local pulse wave velocity (PWV) is used as index for representing the arterial transmission capacity of blood pressure waveforms. The sensitivity analysis suggests that some geometrical factors, such as the stress-free inner radius and opening angle, play a major role on the system's haemodynamics. Subsequently, we quantified the differences in haemodynamic variables obtained from different virtual CCAs, tube laws and flow conditions. Although each artery presents a distinct vascular response, the differences obtained across different flow regimes are not significant. As expected, the linear tube law is unable to accurately capture all the haemodynamic features characterizing the current model. The findings from the sensitivity analysis are further confirmed by investigating the axial stretching effect on the CCA fluid dynamics. This factor does not seem to alter the pressure and flow waveforms. On the contrary, it is shown that, for an axially stretched vessel, the vascular wall exhibits an attenuation in absolute distension and an increase in circumferential stress, corroborating the findings of previous studies. This analysis shows that the new model offers a good balance between computational complexity and physics captured, making it an ideal framework for studies aiming to investigate the profound link between vascular mechanobiology and blood flow.Entities:
Keywords: Axial stretching; Common carotid artery; Hyperelasticity; One-dimensional blood flow modelling; Pulse wave velocity; Tube law
Mesh:
Year: 2021 PMID: 33683514 PMCID: PMC8298378 DOI: 10.1007/s10237-021-01437-5
Source DB: PubMed Journal: Biomech Model Mechanobiol ISSN: 1617-7940
Fig. 1Haemodynamic circuit representing the CCA and its boundary conditions: at the inlet inflow = is prescribed, whilst outflow conditions are modelled by a three element (,C,) Windkessel model
Fig. 2Configurations considered for the system under analysis: stress-free , load-free and loaded
Fitting parameters for CCA SEF (16), reported from Auricchio et al. (2014). In both cases two families of fibres are considered (=2)
| Experiment | ||||||||
|---|---|---|---|---|---|---|---|---|
|
Delfino et al. ( | 0.09 | 0.446 | 100.0 | 15.9 | 158.3 | 9.8 | 0.0 | ± 90.0 |
|
Sommer et al. ( | 0.117 | 0.431 | 80.9 | 26.6 | 20.9 | 56.5 | 0.97 | ± 24.9 |
Fig. 3Structural response of hyperelastic wall model under biaxial testing conditions. The panels on the left side are relative to the “Pressure-diameter test”, whilst the panels on the right side are associated with the “Force-length test”. The outer radius in the loaded configuration is defined as =
Fig. 4a: luminal pressure against cross-sectional area for different tube laws; b, c, d: area, pressure and flow waveforms recorded in time at z=l/2 for different tube laws
Fig. 5a, b: compliance and wave speed against cross-sectional area for different tube laws; c, d: compliance and wave speed recorded in time at z=l/2 for different tube laws
Fig. 6Contour plots of Cauchy stress components against wall thickness and time at z=l/2
Fig. 7PWV variances associated with H variation against number of virtual arteries
Global sensitivity indices for a sample of =50,000 virtual arteries obtained by varying the input parameters within a box ± 5 of data reported in Table 1 corresponding to Sommer’s experiment. value is rounded to 0.0000 when values are smaller than
| 0.0000 | 0.1446 | 0.0036 | 0.0000 | 0.0000 | 0.0000 | 0.0000 | 0.0000 | |
| 0.1864 | 0.9896 | 0.7693 | 0.5849 | 0.4024 | 0.5647 | 0.5254 | 0.6366 |
Variances of the parameters, correlation with PWV and associated regression coefficients
| Parameter | Variance | Std. dev. | Correlation with PWV | Regression Coefficient (slope) |
|---|---|---|---|---|
| 1.0 | 3.4 | −0.006 | −90.36963 | |
| 1.5 | 1.2 | 0.211 | 833.18354 | |
| 5.5 | 2.3 | −0.079 | −1.66925 | |
| 5.9 | 7.7 | −0.005 | −0.00003 | |
| 3.6 | 6.0 | −0.002 | −0.00002 | |
| 2.7 | 1.6 | −0.012 | −0.35579 | |
| 2.1 | 1.4 | 0.023 | 77.60300 | |
| 5.2 | 7.2 | −0.041 | −2.79135 | |
| PWV (cm/s) | 2.4 | 4.9 | 1.000 | 1.00000 |
Fig. 8Pressure recorded in time at z=l/2 for VA1, VA2 and VA3 under normal and increased flow conditions. For each virtual artery, three tube laws are considered
Haemodynamic quantities PWV (in m/s), (in mmHg), (in mmHg), (in cm) and (in cm) obtained through the current and tube laws for VA1, VA2 and VA3. Values are reported for both normal and increased flow conditions
| Normal | Increased | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| VA-tube law | PWV | PWV | ||||||||
| VA1-current | 6.09 | 131.23 | 78.57 | 0.2192 | 0.2059 | 7.00 | 171.98 | 101.10 | 0.2248 | 0.2129 |
| VA1- | 6.12 | 129.16 | 79.17 | 0.2253 | 0.2061 | 6.40 | 167.65 | 102.98 | 0.2407 | 0.2151 |
| VA1- | 6.70 | 130.72 | 78.28 | 0.2197 | 0.2059 | 6.89 | 169.79 | 101.77 | 0.2303 | 0.2120 |
| VA2-current | 7.33 | 130.51 | 78.78 | 0.2797 | 0.2644 | 8.18 | 171.26 | 101.24 | 0.2863 | 0.2725 |
| VA2- | 7.37 | 128.24 | 79.47 | 0.2865 | 0.2647 | 7.64 | 166.50 | 103.38 | 0.3042 | 0.2752 |
| VA2- | 7.97 | 129.97 | 78.44 | 0.2802 | 0.2644 | 8.13 | 168.84 | 102.00 | 0.2924 | 0.2715 |
| VA3-current | 9.92 | 129.30 | 79.41 | 0.4230 | 0.4037 | 11.05 | 170.05 | 101.79 | 0.4319 | 0.4141 |
| VA3- | 10.08 | 126.71 | 80.22 | 0.4308 | 0.4041 | 10.41 | 164.54 | 104.38 | 0.4531 | 0.4179 |
| VA3- | 10.68 | 128.69 | 78.99 | 0.4235 | 0.4036 | 10.96 | 167.19 | 102.73 | 0.4392 | 0.4130 |
Relative variation in PWV, , , and between the current and tube laws for VA1, VA2 and VA3. Values are reported for both normal and increased flow conditions
| VA- | Normal | Increased | ||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| VA1- | 0.49 | −1.58 | 0.77 | 2.78 | 0.10 | −8 | −2.52 | 1.85 | 7.07 | 1.03 |
| VA1- | 10.11 | −0.38 | −0.38 | 0.23 | 0.00 | −1.64 | −1.27 | 0.66 | 2.43 | −0.44 |
| VA2- | 0.58 | −1.74 | 0.87 | 2.44 | 0.11 | −6.67 | −2.78 | 2.11 | 6.23 | 0.99 |
| VA2- | 8.86 | −0.41 | −0.44 | 0.19 | −0.01 | −0.65 | −1.41 | 0.75 | 2.14 | −0.38 |
| VA3- | 1.60 | −2.00 | 1.03 | 1.84 | 0.10 | −5.79 | −3.24 | 2.55 | 4.90 | 0.90 |
| VA3- | 7.63 | −0.47 | −0.53 | 0.12 | −0.02 | −0.87 | −1.68 | 0.92 | 1.69 | −0.27 |
Fig. 9Contour plots of Cauchy Stress components against wall thickness and time at z=l/2 for VA1 under normal and increased flow conditions
Fig. 10Contour plots of Cauchy Stress components against wall thickness and time at z=l/2 for VA2 under normal and increased flow conditions
Fig. 11Contour plots of Cauchy Stress components against wall thickness and time at z=l/2 for VA3 under normal and increased flow conditions
Fig. 12a, b: pressure and compliance against cross-sectional area for different axial stretches; c: circumferential Cauchy stress component against circumferential stretch at for different axial stretches; d, e, f: pressure, area and wave speed recorded in time at z=l/2 for different axial stretches
Haemodynamic quantities for different total axial stretches. The values of pressure and area are recorded at z=l/2. and
| PWV (m/s) | ||||||||
|---|---|---|---|---|---|---|---|---|
| 1.2 | 9.47 | 78.71 | 51.63 | 0.3689 | 0.0183 | 0.0495 | 9.588 | 11.45 |
| 1.3 | 9.07 | 78.93 | 51.14 | 0.3519 | 0.0179 | 0.0509 | 9.945 | 11.25 |
| 1.4 | 8.57 | 79.07 | 50.82 | 0.3303 | 0.0173 | 0.0523 | 10.287 | 11.06 |
| 1.5 | 8.08 | 79.16 | 50.60 | 0.3031 | 0.0165 | 0.0545 | 10.767 | 10.81 |