0172

Anisotropic stiffness of ex vivo swine heart estimated by transversely isotropic nonlinear inversion MRE at 2mm isotropic voxel resolution
Cyril Tous1,2, Guillaume Flé3, Matthew McGarry4, Philip Bayly5, Keith Paulsen4,6, Curtis Johnson7, Matthias Stuber1,2, and Elijah Van Houten8
1Diagnostic and Interventional Radiology, Lausanne University Hospital (CHUV), Lausanne, Switzerland, 2Center for Biomedical Imaging (CIBM), Lausanne, Switzerland, 3Université de Montréal, Montréal, QC, Canada, 4Thayer school of engineering, Dartmouth College, Hanover, NH, United States, 5McKelvey School of Engineering, Washington University, Saint Louis, MO, United States, 6Dartmouth-Hitchcock Medical Center, Lebanon, NH, United States, 7Biomedical Engineering, University of Delaware, Newark, DE, United States, 8Mechanical Engineering, Université de Sherbrooke, Sherbrooke, QC, Canada

Synopsis

Keywords: Heart, Elastography

MR elastography (MRE) must account for the anisotropic nature of myocardial tissue to accurately quantify stiffness. The constitutive matrix for this material was rotated to align with the fibers. One ex vivo swine heart was scanned with DTI and MRE sequences at 2 isotropic voxel resolution. Transversely isotropic viscoelastic stiffness was reconstructed using the Non-Linear Inversion (NLI) algorithm. Elastic properties (shear and Young’s modulus, tensile and shear anisotropy) were segment dependent, in agreement with the myocyte sheetlet formation, which varies in size and spacing according to the myocardial segment. Similarities between MRE and DTI metrics could be observed.

Introduction

MR elastography (MRE) can quantify stiffness in various cardiac pathologies1-3. However, to date, these approaches have not considered the anisotropic nature of the myoarchitecture, which is known to introduce variance in MRE results up to 30%4. High resolution studies of the cardiac microstructure by X-ray phase contrast5-7 showed that myocyte orientation and sheetlet size are segment dependent. Moreover, the collagen matrix of the myocardial wall forms a honeycomb arrangement8, constituting a deformable material of high tensile strength in order to maintain its structure8. The matrix assists in the lengthening of myocytes during diastole and prevents myocytes from over-stretching9,10. This collagen honeycomb is a "shape-memory" material that re-structures itself according to myocyte orientation 9, and forms laminar "sheetlets" which are separated by cleavage planes. The sheetlets thickness and their branching patterns vary transmurally to accommodate for sheetlet motion11. These myocyte angulations and sheetlet differences define the different biomechanical roles for each myocardial segment12. Better differentiation of the segmental variation of anisotropic stiffness could help to improve the characterization of this complex myocardial structure and understand the biomechanics of myocardial pathologies.

Methods

One freshly excised ex vivo porcine heart was scanned on a 3T MRI (Figure1-A). MRE data were collected using a Resoundant MRE actuator at 100Hz and encoding gradient amplitude at 40mT/m in a spin echo EPI sequence with parameters13: FOV=340 mm2; TR/TE=540/109 ms; BW=1730 Hz, 3 slices and 2 mm3 isotropic voxel; FOV=200 mm2; TR/TE=2300/132 ms; BW=962 Hz, 10 slices and 1 mm3 voxel; DTI data with resolution and FOV matched to the MRE scans were also acquired with 32 diffusion-encoding gradients at b=557 s/mm² (3 averages); TR/TE=1500/70ms. The angulation of the myocytes was calculated by projecting the first eigenvector (Figure1-B) onto the circumferential plane (Figure1-C). Anisotropic mechanical properties of the heart were treated by the NLI-MRE subzone post-processing method formulated with a finite element based, nearly incompressible, transverse isotropic material model14-17, where the axis of symmetry is rotated based on DTI data to align with the primary fiber axis. The constitutive equation for this material is given by:

$$$ \left(\begin{matrix}{\sigma^\prime}_{11}\\{\sigma^\prime}_{22}\\{\sigma^\prime}_{33}\\{\sigma^\prime}_{12}\\{\sigma^\prime}_{23}\\{\sigma^\prime}_{13}\\\end{matrix} \right)=\left[\begin{matrix}c_{11}&c_{12}&c_{13}&0&0&0\\c_{21}&c_{22}&c_{23}&0&0&0\\c_{31}&c_{32}&c_{33}&0&0&0\\0&0&0&c_{44}&0&0\\0&0&0&0&c_{55}&0\\0&0&0&0&0&c_{66}\\\end{matrix}\right] \left(\begin{matrix}{\epsilon^\prime}_{11}\\{\epsilon^\prime}_{22}\\{\epsilon^\prime}_{33}\\{2\epsilon^\prime}_{12}\\{2\epsilon^\prime}_{23}\\{2\epsilon^\prime}_{13}\\\end{matrix}\right) $$$,(1)

with the components of the 6x6 elasticity matrix, [C], given by, (2):

$$$\begin{matrix}c_{11}=\ \kappa+\frac{4}{3}\mu\left(1+\frac{4}{3}\zeta\right),&c_{22}=c_{33}=\ \kappa+\frac{4}{3}\mu\left(1+\frac{1}{3}\zeta\right),\end{matrix}$$$
$$$\begin{matrix}c_{44}=c_{66}=\mu\left(1+\phi\right),\end{matrix} \begin{matrix}c_{12}=c_{13}=c_{21}=c_{31}=\ \kappa-\frac{2}{3}\mu\left(1+\frac{4}{3}\zeta\right),\end{matrix}$$$
$$$\begin{matrix}c_{32}=c_{23}=\ \kappa-\frac{2}{3}\mu\left(1-\frac{2}{3}\zeta\right),&c_{55}=\mu\end{matrix}$$$

where μ is the shear modulus in the plane normal to the fiber axis, Φ is the shear anisotropy, ζ is the tensile anisotropy, and κ is the isotropic bulk modulus. From (2), it can be seen that the two axial shear moduli, $$${\mu_{ax}}$$$ corresponding to shearing in the along the fiber axis, are given by $$${c_{44}}$$$ and $$${c_{66}}$$$ while the transverse shear modulus, $$${\mu_{tr}}$$$, corresponding to shearing around the fiber axis (no fiber influence), is given by $$${c_{55}}$$$. Hence, $$${Φ=\frac{μ_{ax}}{μ_{tr}}-1}$$$ and $$${ζ=\frac{E_{ax}}{E_{tr}}-1}$$$, with E the Young’s modulus. Suitability of the MRE displacement data for the non-linear inversion was assessed using the Octahedral Shear Strain Signal to Noise Ratio18 (Figure1-D). To verify plausible dependency between structural organization and stiffness, the transverse angle and the transverse shear modulus were measured across the myocardial wall.

Results

In the LV, tensile anisotropy was $$${\zeta_{ax}=0.32±0.43}$$$, shear anisotropy was $$${\phi_{ax}=0.66±0.40}$$$, and shear modulus was $$${\mu_{tr}=6.9±2.15}$$$ KPa (Figure 2) which compares with previous studies considering isotropic tissue (3.84±0.4 KPa at end‐diastolic and 4.94±0.5 KPa at end‐systole)2. Sheetlets are 1.66 times more resistant to shear in the fiber planes compared to shearing through their plane ($$${\mu_{ax} versus \mu_{tr}}$$$). The axial Young’s modulus of the fiber was $$${E_{ax}=28.8±14.8}$$$ KPa (Figure3), or 2.43 stiffer than axial sheetlet shearing ($$${\mu_{ax}}$$$) and 1.32 times stiffer than Young’s modulus normal to the fiber axis ($$${E_{tr}}$$$). Segment wise, the axial Young’s modulus of the septum ($$${E_{ax}=31.8±14.3}$$$ KPa, Figure4) was significantly higher than the other segments while the lateral wall had the highest shear modulus along the fiber axis (resistance of sliding sheetlets, $$${\mu_{ax}=11.4±4.99}$$$ KPa). Sliding sheets experience more resistances ($$${\mu_{ax}}$$$, $$${\mu_{tr}}$$$) when they are parallel to the circumferential plane (Figure5).

Discussion

Stiffness values using MRE in the human LV was reported at 4.99±1.05KPa19, 20, based on isotropic models, while our anisotropic model shows much more stiffness, 7-8KPa. Fibers were ~1.3 times higher in axial tensile stiffness than transverse, which is in line with tension tests20. The septum has the highest sigmoidal gradient, mainly longitudinal fibers across the wall, with a quasi-absence of sheetlets from the mid-wall to the epicardium6, and correspondingly show more tensile anisotropy ($$${E_{ax}}$$$, resistance along the fiber) than shear anisotropy ($$${\mu_{ax}}$$$, resistance of the sliding sheetlets). The lateral and posterior walls have thick sheetlets, large cleavage planes, and a linear angulation of the myocytes6, corresponding to high $$${\mu_{ax}}$$$ and lower $$${E_{ax}}$$$. The transverse angle and shear modulus show reasonable agreement. In fact, these transverse patterns mean that the fiber field has a radial component adding a mechanical coupling between the posterior and anterior layers, therefore changing the distribution of shearing. However, our model cannot account for intersecting sheet orientations, which disagrees with the presence of orthogonal sheetlets6. The ability to differentiate stiffness across segments will help to better detect pathology and understand biomechanics.

Conclusion

Stiffness of myofibers and sheetlets can be differentiated in an ex vivo animal model. These stiffnesses vary across myocardial segments and are dependent on the microstructure organization.

Acknowledgements

No acknowledgement found.

References

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Figures

Experimental setup (A) showing the ex vivo swine heart with the MRE actuator. Diffusion tensor imaging (B, showing the first eigenvector) was acquired to consider tissue anisotropy in the stiffness estimation. Their respective helix angle (HA), i.e. angulation of the myocytes, are shown in (C). Octahedral shear strain based measure of the Signal to Noise Ratio (SNR) obtained for the MRE analysis (D).

Real ($$$\mu_{R}$$$, storage moduli) and imaginary ($$$\mu_{I}$$$, loss moduli) parts of the shear modulus in the left ventricle with their respective convergence and mapping in KPa. The shear anisotropy ($$$\phi$$$) informs on the amount of shearing the sheetlets endure by sliding on each other in the direction of the fiber. The real shear modulus, i.e. the transverse shear, relates to the transversal shearing a sheetlet imposes on top of another (normal to the sheet).

Axial ($$$E_{ax}$$$) and transversal ($$$E_{tr}$$$) Young's modulus characterize the tensile anisotropy ($$$\zeta$$$) in the direction of the fiber and perpendicular to the fiber, respectively. The stretched of the along the sheetlet and its constitutive fibers as well as the dilatation of the sheetlet perpendicular to the fibers are segment dependent.

Stiffness properties for each myocardial segments. Significance at P=0.001 (*).

Stiffness properties and structural organization. Eax increases when ||HA|| decreases, means that fibers have more resistance along the fiber (tensile anisotropy) when they are circumferential (HA=0°,TA=0° at mid wall). On the contrary, endocardial and epicardial fibers are more compliant to stretch (lower tensile anisotropy) while having higher HA contributing to longitudinal shortening. Sheetlet experience more shear resistance when they are parallel to the circumferential plane (TA=0 at mid wall) and less resistance when they are radial (higher TA at endo and epicardium).

Proc. Intl. Soc. Mag. Reson. Med. 31 (2023)
0172
DOI: https://doi.org/10.58530/2023/0172