| Literature DB >> 31802292 |
Christoph M Augustin1,2, Thomas E Fastl3, Aurel Neic2, Chiara Bellini4, John Whitaker5, Ronak Rajani5, Mark D O'Neill5, Martin J Bishop3, Gernot Plank2,6, Steven A Niederer7.
Abstract
The left atrium (LA) has a complex anatomy with heterogeneous wall thickness and curvature. The anatomy plays an important role in determining local wall stress; however, the relative contribution of wall thickness and curvature in determining wall stress in the LA is unknown. We have developed electromechanical finite element (FE) models of the LA using patient-specific anatomical FE meshes with rule-based myofiber directions. The models of the LA were passively inflated to 10mmHg followed by simulation of the contraction phase of the atrial cardiac cycle. The FE models predicted maximum LA volumes of 156.5 mL, 99.3 mL and 83.4 mL and ejection fractions of 36.9%, 32.0% and 25.2%. The median wall thickness in the 3 cases was calculated as [Formula: see text] mm, [Formula: see text] mm, and [Formula: see text] mm. The median curvature was determined as [Formula: see text] [Formula: see text], [Formula: see text], and [Formula: see text]. Following passive inflation, the correlation of wall stress with the inverse of wall thickness and curvature was 0.55-0.62 and 0.20-0.25, respectively. At peak contraction, the correlation of wall stress with the inverse of wall thickness and curvature was 0.38-0.44 and 0.16-0.34, respectively. In the LA, the 1st principal Cauchy stress is more dependent on wall thickness than curvature during passive inflation and both correlations decrease during active contraction. This emphasizes the importance of including the heterogeneous wall thickness in electromechanical FE simulations of the LA. Overall, simulation results and sensitivity analyses show that in complex atrial anatomy it is unlikely that a simple anatomical-based law can be used to estimate local wall stress, demonstrating the importance of FE analyses.Entities:
Keywords: Cardiac mechanics; Finite element simulation; Left atrium; Patient-specific modeling; Wall stress
Mesh:
Year: 2019 PMID: 31802292 PMCID: PMC7203597 DOI: 10.1007/s10237-019-01268-5
Source DB: PubMed Journal: Biomech Model Mechanobiol ISSN: 1617-7940
Fig. 1Constitutive law fitting. Comparison of model (solid) and experimental (dashed) passive material properties Experimental data from Bellini et al. (2013) for different tension ratios (P) in the 1 and 2 directions. is the stress in direction 1, is the stress in direction 2, is the Green strain in direction 1 and is the Green strain in direction 2
Fig. 2Comparison to Laplace estimates. a Geometric setup with R the inner radius and T the thickness of the spheres. A pressure was applied to the inner surface . b Dirichlet boundary conditions were enforced at the intersections of the Cartesian axes with the outer surface . Displacements at these points were restricted to be along the respective intersecting axes. c Transversely isotropic setup with one fiber family in the circumferential direction
Summary attributes of patient attributes
| Index | Sex | Age | Comorbidities |
|---|---|---|---|
| 1 | M | 35 | HLD |
| 2 | F | 48 | |
| 3 | F | 54 | PAF, SSS |
M male, F female, HLD hyperlipidemia, PAF paroxysmal atrial fibrillation, SSS sick sinus syndrome
Fig. 3Model anatomies and activation patterns. Anterior (top row) and posterior (bottom row) perspective of patients showing the local activation time for the universal electrophysiology reference simulations. Isochrones are provided in 10 ms intervals
Fig. 4Curvature and thickness. Anterior perspective of analyzed patients showing the left atrial wall thickness in the first and curvature in the second row. Brighter colors correspond to larger thickness and curvature values
Fig. 5Stress fields. Anterior perspective of analyzed patients showing the reference geometry and the first principal total Cauchy stress () for the biomechanics simulations at the inflated and maximally contracted state. To the right, the volume curve over time for the inflation to 10 mmHg, and subsequent active contraction and relaxation, for each patient
Summary LA volume changes during simulated atrial contraction
| IF (%) | EF (%) | ||||
|---|---|---|---|---|---|
| 1 | 101.03 | 156.47 | 98.81 | 154.9 | 36.9 |
| 2 | 61.04 | 99.31 | 67.57 | 162.2 | 32.0 |
| 3 | 51.11 | 83.36 | 62.32 | 163.1 | 25.2 |
i Case index; reference volume; volume after inflation, prior to atrial contraction; minimum atrial volume at contracted state; inflation fraction (IF) is ; and ejection fraction (EF) is (
Fig. 6Hexbin plots of (i) total stress () vs. the inverse of curvature, (ii) total stress versus the inverse of thickness and (iii) total stress versus the inverse of (curvature thickness) for the inflated and the maximal contracted state, respectively. Thickness, curvature and the first principal stress were interpolated on the nodes of the finite element mesh and analyzed. Regions close to the pulmonary vein inlets and the mitral valve were excluded from the statistical analysis and the plots since data there may be affected by the spring-type boundary conditions. Black lines show a linear regression model fit. Spearman’s values and values from the linear regression fit are given for each plot
Summary, Spearman’s correlations between the principle wall Cauchy stress and the curvature and wall thickness on the reference grid
| 1 | 0.556 | 0.437 | 0.227 | 0.186 | 0.525 | 0.412 | 0.005 |
| 2 | 0.615 | 0.384 | 0.199 | 0.162 | 0.603 | 0.402 | − 0.027 |
| 3 | 0.536 | 0.438 | 0.248 | 0.343 | 0.506 | 0.424 | 0.117 |
are Spearman’s correlations between stress and inverse of wall thickness, are Spearman’s correlations between stress and inverses of curvature, are Spearman’s correlations between stress and inverse of (curvature thickness). The subscripts and denote the inflated and maximal contracted state, respectively. are Spearman’s correlations between wall thickness and curvature. p-values were for all cases
Sensitivity to parameter modifications
| Parameter | IF (%) | EF (%) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Control | 83.4 | 62.3 | 142 | 163.1 | 25.2 | 0.536 | 0.438 | 0.248 | 0.343 | 0.506 | 0.522 |
| 85.7 | 69.7 | 144 | 167.6 | 18.6 | 0.540 | 0.488 | 0.250 | 0.346 | 0.510 | 0.553 | |
| 80.4 | 52.9 | 141 | 157.3 | 34.2 | 0.528 | 0.337 | 0.243 | 0.320 | 0.498 | 0.446 | |
| 83.4 | 54.6 | 140 | 163.1 | 34.4 | 0.536 | 0.372 | 0.248 | 0.334 | 0.506 | 0.477 | |
| 83.4 | 69.8 | 144 | 163.1 | 16.2 | 0.536 | 0.486 | 0.248 | 0.333 | 0.506 | 0.542 | |
| 81.9 | 61.6 | 141 | 160.3 | 24.8 | 0.541 | 0.440 | 0.245 | 0.342 | 0.506 | 0.523 | |
| 85.1 | 63.3 | 142 | 166.5 | 25.7 | 0.530 | 0.436 | 0.251 | 0.343 | 0.505 | 0.521 | |
| 82.6 | 62.3 | 142 | 161.6 | 24.6 | 0.535 | 0.436 | 0.252 | 0.342 | 0.508 | 0.520 | |
| 84.3 | 62.4 | 141 | 164.9 | 26.0 | 0.538 | 0.441 | 0.243 | 0.343 | 0.504 | 0.523 | |
| stiff. | 81.2 | 61.6 | 142 | 158.9 | 24.2 | 0.539 | 0.438 | 0.248 | 0.342 | 0.508 | 0.521 |
| stiff. | 86.1 | 63.4 | 141 | 168.5 | 26.4 | 0.531 | 0.438 | 0.247 | 0.343 | 0.503 | 0.522 |
| 85.7 | 67.0 | 143 | 167.7 | 21.8 | 0.547 | 0.474 | 0.232 | 0.339 | 0.501 | 0.540 | |
| 81.3 | 59.8 | 141 | 159.2 | 26.5 | 0.525 | 0.408 | 0.261 | 0.341 | 0.510 | 0.502 | |
| 83.4 | 52.4 | 140 | 163.1 | 37.2 | 0.537 | 0.346 | 0.248 | 0.327 | 0.507 | 0.457 | |
| 90.4 | 89.1 | 144 | 176.8 | 1.4 | 0.560 | 0.560 | 0.203 | 0.201 | 0.487 | 0.486 | |
| 83.5 | 62.5 | 142 | 163.3 | 25.1 | 0.553 | 0.457 | 0.251 | 0.348 | 0.519 | 0.538 | |
| 83.9 | 62.3 | 142 | 164.1 | 25.8 | 0.558 | 0.475 | 0.258 | 0.375 | 0.526 | 0.569 | |
| 84.5 | 62.1 | 142 | 165.3 | 26.5 | 0.562 | 0.482 | 0.261 | 0.382 | 0.530 | 0.579 |
Shown are inflated volume ; contracted volume ; time of maximal contraction ; inflation fraction (IF), ejection fraction (EF). Spearman- values for correlation: inverse of wall thickness (), inverse of curvature (), inverse of (thickness curvature) () each versus stress at inflation () and contraction (). For all models the initial volume was 51 mL since they are all based on the patient case 3 from Table 1.
Sensitivity to geometrical modifications
| Parameter | IF (%) | EF (%) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Control | 83.4 | 62.3 | 142 | 163.1 | 25.2 | 0.536 | 0.438 | 0.248 | 0.343 | 0.506 | 0.522 |
| Patch | 83.4 | 62.3 | 142 | 163.1 | 25.2 | 0.536 | 0.439 | 0.248 | 0.352 | 0.522 | 0.535 |
| Patch | 83.4 | 62.3 | 142 | 163.1 | 25.2 | 0.536 | 0.438 | 0.250 | 0.339 | 0.491 | 0.511 |
| Noised | 80.6 | 60.9 | 141 | 157.7 | 24.5 | 0.512 | 0.432 | 0.293 | 0.380 | 0.481 | 0.510 |
| Constant | 82.7 | 68.4 | 145 | 161.8 | 17.3 | – | – | 0.343 | 0.467 | – | – |
| 0% cutoff | 83.4 | 62.3 | 142 | 163.1 | 25.2 | 0.495 | 0.410 | 0.202 | 0.330 | 0.464 | 0.505 |
| 50% cutoff | 83.4 | 62.3 | 142 | 163.1 | 25.2 | 0.582 | 0.523 | 0.344 | 0.400 | 0.584 | 0.587 |
| 25/5% cutoff | 83.4 | 62.3 | 142 | 163.1 | 25.2 | 0.510 | 0.453 | 0.312 | 0.345 | 0.541 | 0.530 |
| 5/25% cutoff | 83.4 | 62.3 | 142 | 163.1 | 25.2 | 0.606 | 0.506 | 0.260 | 0.369 | 0.536 | 0.565 |
| 83.4 | 62.315 | 142 | 163.1 | 25.2 | 0.561 | 0.518 | 0.390 | 0.446 | 0.525 | 0.600 | |
| stim. | 83.358 | 72.176 | 162 | 163.1 | 13.4 | 0.536 | 0.498 | 0.238 | 0.326 | 0.506 | 0.544 |
Shown are inflated volume ; contracted volume ; time of maximal contraction ; inflation fraction (IF), ejection fraction (EF). Spearman- values for correlation: inverse of wall thickness (), inverse of curvature (), inverse of (thickness curvature) () each versus stress at inflation () and contraction ()
Sensitivity to stress measurements
| Stress type | Stress part | ||||||
|---|---|---|---|---|---|---|---|
| 1st principal stress | 0.536 | 0.438 | 0.248 | 0.343 | 0.506 | 0.522 | |
| 2nd principal stress | 0.415 | 0.290 | 0.323 | 0.320 | 0.495 | 0.419 | |
| 3rd principal stress | 0.041 | 0.089 | 0.192 | 0.178 | 0.170 | 0.186 | |
| fiber stress | 0.522 | 0.410 | 0.252 | 0.366 | 0.492 | 0.517 | |
| Stress magnitude | 0.578 | 0.480 | 0.266 | 0.370 | 0.547 | 0.574 | |
| Von Mises stress | 0.552 | 0.448 | 0.207 | 0.290 | 0.483 | 0.484 | |
| 1st principal stress | 0.536 | 0.310 | 0.248 | 0.307 | 0.506 | 0.424 | |
| 2nd principal stress | 0.415 | 0.288 | 0.323 | 0.251 | 0.495 | 0.352 | |
| 3rd principal stress | 0.041 | 0.273 | 0.192 | 0.266 | 0.170 | 0.378 | |
| Fiber stress | 0.522 | 0.402 | 0.252 | 0.299 | 0.492 | 0.471 | |
| Stress magnitude | 0.578 | − 0.244 | 0.266 | − 0.206 | 0.547 | − 0.322 | |
| Von Mises stress | 0.552 | 0.126 | 0.207 | 0.135 | 0.483 | 0.171 | |
| 1st principal stress | – | 0.222 | – | 0.172 | – | 0.259 | |
| 2nd principal stress | – | 0.086 | – | 0.063 | – | 0.077 | |
| 3rd principal stress | – | − 0.096 | – | − 0.034 | – | ||
| Fiber stress | – | 0.214 | – | 0.269 | – | 0.314 | |
| Stress magnitude | – | 0.401 | – | 0.317 | – | 0.462 | |
| Von Mises stress | – | 0.285 | – | 0.206 | – | 0.318 | |
| 1st principal stress | 0.553 | 0.374 | 0.249 | 0.333 | 0.517 | 0.483 | |
| 2nd principal stress | 0.388 | 0.315 | 0.308 | 0.280 | 0.469 | 0.399 | |
| 3rd principal stress | 0.041 | 0.145 | 0.149 | 0.266 | 0.133 | 0.289 | |
| Fiber stress | 0.532 | 0.390 | 0.272 | 0.358 | 0.515 | 0.504 | |
| Stress magnitude | 0.595 | 0.456 | 0.282 | 0.393 | 0.569 | 0.578 | |
| Von Mises stress | 0.576 | 0.375 | 0.174 | 0.185 | 0.474 | 0.365 |
Shown is total Cauchy stress (), passive Cauchy stress (), active Cauchy stress (), and total second Piola-Kirchhoff stress (). For each the stress magnitude, first, second, and third principal stress, fiber stress, and von Mises stress is computed. Spearman- values for correlation: inverse of wall thickness (), inverse of curvature (), inverse of (thickness curvature) () each versus stress at inflation () and contraction (). Active stress is 0 at the point of inflation, hence, results are omitted
Laplace law
| Fibers | IF (%) | EF (%) | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| isotropic | 20 | 0.5 | 2.6 | 33.5 | 59.7 | 58.6 | 178.0 | 1.8 | 53.3 | 52.8 | 45.9 | 46.6 | ||
| tr. iso. | 20 | 0.5 | 2.6 | 33.5 | 57.0 | 43.7 | 170.2 | 23.4 | 52.8 | 42.8 | 40.8 | 44.7 | ||
| ortho. | 20 | 0.5 | 2.6 | 33.5 | 56.0 | 49.9 | 167.3 | 11.0 | 50.5 | 44.8 | 39.0 | 43.9 | ||
| incomp. | 20 | 0.5 | 2.6 | 33.5 | 55.9 | 50.5 | 166.9 | 9.6 | 50.4 | 47.0 | 41.0 | 43.8 | ||
| isotropic | 20 | 2.5 | 14.2 | 33.5 | 48.6 | 47.7 | 145.0 | 1.7 | 8.7 | 7.9 | 6.7 | 7.2 | ||
| tr. iso. | 20 | 2.5 | 14.2 | 33.5 | 46.3 | 22.9 | 138.2 | 50.5 | 8.5 | 12.8 | 8.6 | 7.1 | ||
| ortho. | 20 | 2.5 | 14.2 | 33.5 | 45.5 | 22.0 | 136.0 | 51.7 | 8.1 | 5.1 | 3.2 | 7.0 | ||
| isotropic | 20 | 5.0 | 31.9 | 33.5 | 44.5 | 43.8 | 133.0 | 1.6 | 4.0 | 3.1 | 2.5 | 3.1 | ||
| tr. iso. | 20 | 5.0 | 31.9 | 33.5 | 42.5 | 21.7 | 126.9 | 48.9 | 3.9 | 13.0 | 4.2 | 3.2 | ||
| ortho. | 20 | 5.0 | 31.9 | 33.5 | 41.8 | 20.7 | 124.8 | 50.5 | 3.7 | 4.3 | − 1.1 | 3.1 | ||
| isotropic | 25 | 0.5 | 4.0 | 65.4 | 119.9 | 117.7 | 183.2 | 1.8 | 68.5 | 68.0 | 59.2 | 60.2 | ||
| tr. iso. | 25 | 0.5 | 4.0 | 65.4 | 114.5 | 98.4 | 175.0 | 14.1 | 67.9 | 60.7 | 57.5 | 57.5 | ||
| ortho. | 25 | 0.5 | 4.0 | 65.4 | 112.4 | 104.2 | 171.7 | 7.3 | 64.9 | 60.1 | 52.3 | 56.5 | ||
| incomp. | 25 | 0.5 | 4.0 | 65.4 | 112.0 | 104.8 | 171.2 | 6.4 | 64.8 | 61.9 | 54.0 | 56.3 | ||
| isotropic | 25 | 2.5 | 21.7 | 65.4 | 97.5 | 95.8 | 149.0 | 1.7 | 11.1 | 10.3 | 8.8 | 9.3 | ||
| tr. iso. | 25 | 2.5 | 21.7 | 65.4 | 93.0 | 45.7 | 142.2 | 50.8 | 10.9 | 13.3 | 10.3 | 9.2 | ||
| ortho. | 25 | 2.5 | 21.7 | 65.4 | 91.5 | 43.9 | 139.9 | 52.1 | 10.5 | 5.8 | 4.6 | 9.1 | ||
| isotropic | 25 | 5.0 | 47.6 | 65.4 | 89.5 | 87.0 | 136.8 | 1.7 | 5.1 | 4.2 | 3.5 | 4.1 | ||
| tr. iso. | 25 | 5.0 | 47.6 | 65.4 | 85.3 | 43.0 | 130.4 | 49.5 | 5.0 | 12.7 | 5.5 | 4.1 | ||
| ortho. | 25 | 5.0 | 47.6 | 65.4 | 83.8 | 41.2 | 128.2 | 50.8 | 4.7 | 4.5 | 0.3 | 4.1 | ||
| isotropic | 30 | 0.5 | 5.8 | 113.1 | 212.1 | 208.3 | 187.5 | 1.8 | 84.0 | 83.7 | 72.9 | 74.1 | ||
| tr. iso. | 30 | 0.5 | 5.8 | 113.1 | 202.3 | 183.3 | 178.9 | 9.4 | 83.4 | 78.0 | 73.7 | 70.7 | ||
| ortho. | 30 | 0.5 | 5.8 | 113.1 | 198.3 | 187.5 | 175.3 | 5.4 | 79.5 | 75.2 | 65.5 | 69.3 | ||
| incomp. | 30 | 0.5 | 5.8 | 113.1 | 197.5 | 188.2 | 174.7 | 4.7 | 79.5 | 76.9 | 67.0 | 69.1 | ||
| isotropic | 30 | 2.5 | 30.7 | 113.0 | 172.2 | 169.2 | 152.4 | 1.8 | 13.7 | 12.9 | 11.0 | 11.5 | ||
| tr. iso. | 30 | 2.5 | 30.7 | 113.0 | 164.4 | 80.9 | 145.5 | 50.8 | 13.4 | 14.1 | 11.9 | 11.3 | ||
| ortho. | 30 | 2.5 | 30.7 | 113.0 | 161.9 | 77.3 | 143.2 | 52.3 | 12.9 | 6.9 | 5.9 | 11.2 | ||
| isotropic | 30 | 5.0 | 66.5 | 113.0 | 158.2 | 155.5 | 139.9 | 1.7 | 6.3 | 5.4 | 4.5 | 5.1 | ||
| tr. iso. | 30 | 5.0 | 66.5 | 113.0 | 150.7 | 75.4 | 133.3 | 50.0 | 6.1 | 12.6 | 6.6 | 5.1 | ||
| ortho. | 30 | 5.0 | 66.5 | 113.0 | 148.2 | 72.3 | 131.1 | 51.2 | 5.8 | 4.7 | 1.4 | 5.0 |
Comparison of FE-based mean principal stresses (, ) and mean circumferential fiber stresses (, ) with Laplace estimations (, ) for the inflated (infl.) and the fully contracted (cont.) state. Radius (R), which is the inverse of curvature C, and thickness (T) of the spheres are varied. Three different fiber laws are applied to each of the resulting spheres: isotropic, transversely isotropic (tr. iso.), and orthotropic (ortho.). For the thinnest spheres, () a fully incompressible (incomp.) case is included. Additionally, wall volume , initial cavity volume , inflated cavity volume and cavity volume at contracted state are given as well as inflation fraction (IF) and ejection fraction (EF)
In bold are the circumferential fiber stresses and Laplace estimations for the inflated state; in these cases the Laplace laws are known to be almost exact
Fig. 7Statistical distribution of stress for all three patient cases. Boxplots show the distribution of the 1st principal Cauchy stress: in gray stresses at inflated (), in white stresses at contracted state (). The box represents the interquartile range (IQR) between lower quartile (25 %) and upper quartile (75 %); horizontal black line represents the median value; whisker ends represent the lowest and highest data points still within 1.5 IQR of the lower and upper quartiles, respectively
Laplace law
| Value | Unit | Patient 1 | Patient 2 | Patient 3 | |||
|---|---|---|---|---|---|---|---|
| infl. | cont. | infl. | cont. | infl. | cont. | ||
| Min | (kPa) | − 573.01 | − 336.46 | − 515.86 | − 635.81 | − 416.53 | − 381.09 |
| Max | (kPa) | 2304.60 | 422.54 | 869.39 | 749.39 | 389.49 | 357.67 |
| Mean | (kPa) | 21.01 | 25.51 | 19.92 | 28.16 | 30.93 | 33.69 |
| SD | (kPa) | 20.51 | 17.02 | 24.47 | 19.92 | 25.21 | 20.01 |
| (kPa) | 17.67 | 17.85 | 17.19 | 17.34 | 26.30 | 26.40 | |
Patient cases. Comparison of FE-based mean principal stresses (minimal, maximal, mean, and standard deviation) with Laplace estimations (), see Eqs. (16)–(18), for the inflated (infl.) and the fully contracted (cont.) state
Summary, Spearman’s correlations between the principle wall Cauchy stress and the curvature and wall thickness where we quantified local anatomy in the deformed anatomy, increased endocardial pressure, decreased active tension and only considered the middle 50% of the atria
| 1 | 0.550 | 0.636 | 0.402 | 0.407 | 0.642 | 0.669 |
| 2 | 0.600 | 0.616 | 0.411 | 0.406 | 0.682 | 0.639 |
| 3 | 0.598 | 0.644 | 0.367 | 0.480 | 0.608 | 0.699 |
Abbreviations: are Spearman’s correlations between stress and inverse of wall thickness, are Spearman’s correlations between stress and inverses of curvature, are Spearman’s correlations between stress and inverse of (curvature thickness). The subscripts and denote the inflated and maximal contracted state, respectively. p-values were for all cases