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Effects of bileaflet mechanical heart valve orientation on fluid stresses and coronary flow

Published online by Cambridge University Press:  29 September 2016

Laura Haya
Affiliation:
Department of Mechanical Engineering, University of Ottawa, Ottawa, ON K1N 6N5, Canada
Stavros Tavoularis*
Affiliation:
Department of Mechanical Engineering, University of Ottawa, Ottawa, ON K1N 6N5, Canada
*
†Email address for correspondence: stavros.tavoularis@uottawa.ca

Abstract

The effects of the orientation of a bileaflet mechanical heart valve on the viscous and turbulent stresses in the flow past it and on the flow rate in the right coronary artery were investigated in vitro in a mock circulation loop, using a fluid that matched the kinematic viscosity of blood and the refractive index of the aorta model. Measurements were made past the valve mounted in three orientations at the base of an anatomical aorta model, within physiological aortic flow conditions. At peak flow, the turbulent stresses were on average 21 % higher and viscous stresses exceeding 10 Pa (namely of a level that has been associated with blood cell damage) were 30 % more frequent when the valve was oriented with its plane of symmetry normal to the aorta’s plane of curvature than when it was parallel to it. This was attributed to the impingement of a lateral jet on the concave wall of the aorta and to steeper velocity gradients resulting from the geometrical imbalance of the sinuses relative to the valve’s central jet when the valve was in the ‘normal’ orientation. Very high levels of turbulent stresses were found to occur distal to the corners of the valve’s lateral orifices. The bulk flow rate in the right coronary artery was highest when the valve was positioned with its central orifice aligned with the artery’s opening. The coronary flow rate was directly affected by the size, orientation and time evolution of the vortex in the sinus, all of which were sensitive to the valve’s orientation.

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Type
Papers
Copyright
© 2016 Cambridge University Press 
Figure 0

Figure 1. Sketch of a triradially symmetric aortic sinus with a bilaterally symmetric BMHV, viewed from downstream. RC – right coronary sinus; LC – left coronary sinus; NC – non-coronary sinus.

Figure 1

Figure 2. ‘Best’ BMHV orientations, as recommended by previous studies, with respect to the aortic root geometry; lines indicate the corresponding valve planes of symmetry; abbreviations as in figure 1.

Figure 2

Figure 3. The mock circulation loop.

Figure 3

Figure 4. Anatomical model of the aorta (a) and averaged PIV images of $x$–$z$ and $y$–$z$ centreplanes (b,c). White lines mark the boundaries of masked parts of the images, where measurements were discarded. Arterial branches are labelled as RCA (right coronary artery), LCA (left coronary artery), BRA (brachiocephalic artery), LCC (left common carotid artery and LSA (left subclavian artery).

Figure 4

Table 1. Hydrodynamic parameters for inlet conditions. Reynolds and Womersley numbers were calculated using the inlet diameter $d_{i}=25.4$ mm. $\unicode[STIX]{x1D714}$ is the pulse cycle frequency in $\text{rad}~\text{s}^{-1}$.

Figure 5

Figure 5. Aortic pressure $P_{a}$ and bulk flow rate $\langle Q\rangle$. Black squares and open circles indicate, respectively, ‘other phases’ and ‘key phases’ during which PIV measurements were taken.

Figure 6

Figure 6. Valve orientations with respect to the plane of aorta curvature: (a) ‘normal’; (b) ‘aligned’; (c) ‘inclined’. RC – right coronary sinus; LC – left coronary sinus; NC – non-coronary sinus; white dashed line – $xz$ centreplane; white dashed-dot line – $yz$ centreplane.

Figure 7

Figure 7. Phase-averaged (a) and root-mean-square fluctuations (b) of axial velocity at peak flow, and at $z/D_{i}=0.234$ in the axisymmetric channel, compared with similar measurements by Yun et al. (2014a) and by Dasi et al. (2007).

Figure 8

Figure 8. Phase-averaged planar velocity magnitude $q_{pl}$ in the anatomical model for the normal valve orientation at peak flow (phase C), for the $y$–$z$ (left) and $x$–$z$ (right) centreplanes. NC – non-coronary sinus; RC – right coronary sinus; LC – left coronary sinus.

Figure 9

Figure 9. Phase-averaged velocity $q_{xz}$ on the $x$–$z$ centreplane at phases B (a,c,e) and C (b,d,f), for normal (a,b), aligned (c,d) and inclined (e,f) valve orientations. Red dashed lines indicate the $x$–$z$ centreplane, viewed from downstream.

Figure 10

Figure 10. Phase-averaged axial velocity profiles on the $x$–$z$ centreplane at (a) $z/D=0.65$ and (b) $z/D=1.60$ for normal, inclined and aligned valve orientations at peak flow.

Figure 11

Figure 11. Phase-averaged velocity $q_{yz}$ on the $y$–$z$ centreplane at phases B (a,c,e) and C (b,d,f) for normal (a,b), aligned (c,d) and inclined (e,f) valve orientations. A circular area located at the top of the non-coronary sinus was masked from viewing because this area was optically blocked by the right coronary artery, which exited the model there.

Figure 12

Figure 12. Turbulent stress $\unicode[STIX]{x1D70F}_{max}^{\ast }$ at peak flow for valve orientations: normal (a,b), aligned (c,d) and inclined (e,f), in the $x$–$z$ centreplane (a,c,e) and the $y$–$z$ centreplane (b,d,f). Red arrows connect the planes that were perpendicular to the valve’s symmetry plane and the planes that were parallel to it. The region for the inclined orientation marked with cross-hatching was believed to be strongly affected by error, attributed to loss of optical access, and was not considered in the analysis.

Figure 13

Figure 13. Averaged $\unicode[STIX]{x1D70F}_{max}$ at peak flow for valve orientations: normal (a,b), aligned (c,d) and inclined (e,f), in the $x$–$z$ centreplane (a,c,e) and the $y$–$z$ centreplane (b,d,f). Red arrows connect the planes that were perpendicular to the valve’s symmetry plane and the planes that were parallel to it.

Figure 14

Figure 14. Normalized histogram of $\unicode[STIX]{x1D70F}_{max}$ for normal and aligned valve orientations from the $x$–$z$ and $y$–$z$ centreplanes (a) with a zoomed-in view about the threshold for platelet damage (b).

Figure 15

Figure 15. Phase-averaged planar ‘streamlines’ of flow in the right coronary artery for two phases during acceleration ($t/T=0.086$ – (a–c) and $t/T=0.108$ – (d–f)) and at peak flow ($t/T=0.214$ – (g–h)) for normal (a,d,g), aligned (b,e,h) and inclined (c,f,i) valve orientations.

Figure 16

Figure 16. Phase-averaged planar ‘streamlines’ of flow in the right coronary artery for decelerating phases $t/T=0.261$ (a–c) and $t/T=0.314$ (d–f), and $t/T=0.364$ (g–i) for normal (a,d,g), aligned (b,e,h) and inclined (c,f,i) valve orientations.

Figure 17

Figure 17. Radial direction in the right coronary artery (a) along which the phase-averaged variation of axial velocity $V_{RC}$ is shown (b) at $t/T=0.086$ for the aligned valve orientation.

Figure 18

Figure 18. (a) Phase-averaged flow rate in the aorta during the forward flow phase of the cycle; key phases are indicated by letters as: A – start of systole; B – mid-acceleration point; C – peak of the forward flow; D – mid-deceleration point; E – peak reverse flow, and F – valve closure. (b) Phase-averaged flow rate in the right coronary artery during the forward flow phase of the cycle for normal, aligned and inclined valve orientations.

Figure 19

Figure 19. Velocity projections on the planes parallel to the valve symmetry plane for normal (orange arrows) and aligned (blue arrows) valve orientations at peak flow and $z/D=0.40$; as a scale for velocity magnitudes, the figure shows a black arrow with a length equivalent to $1~\text{m}~\text{s}^{-1}$.

Figure 20

Figure 20. Sketch of inferred vortex ring shape without the effects of valve orientation.

Figure 21

Table 2. Summary of main results for the three valve orientations. The plane-averaged and the plane-maximum values of $\unicode[STIX]{x1D70F}_{max}^{\ast }$ are, respectively, shown outside and inside parentheses.

Figure 22

Figure 21. Instantaneous axial velocity $W$ at $z/D=0.35$, during phase B, in the axisymmetric model, calculated in four different ways: (i) using an $8\times 8$ pixel final interrogation window size, (ii) as in (i) but with a Gaussian filter applied, (iii) using a $12\times 12$ pixel final interrogation window size and (iv) as in (iii) but with a Gaussian filter applied.

Figure 23

Figure 22. Viscous shear stress mapping algorithm: (a) $\unicode[STIX]{x1D70F}_{max12}$ calculated from 12 $\times$ 12 pixel interrogation windows; (b) $\unicode[STIX]{x1D70F}_{max24}$ calculated from 24 $\times$ 24 pixel interrogation windows; (c) scaling factor versus $\unicode[STIX]{x1D70F}_{max24}$ and fitted polynomial; (d) corrected $\unicode[STIX]{x1D70F}_{max}$ mapped from $\unicode[STIX]{x1D70F}_{max24}$.