2012
DOI: 10.1016/j.compfluid.2012.08.007
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Effects of three geometrical parameters on pulsatile blood flow in complete idealised coronary bypasses

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Cited by 11 publications
(31 citation statements)
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“…As the degree of stenosis increased, the use of the bypass became more effective. These findings were consistent with those of Ko et al 14 and Vimmr et al, 19 who asserted that stenosis degree smaller than 50% was commonly described as hemodynamically insignificant because there was no impact on the blood supply to downstream tissues. Furthermore, according to Fan et al, 21 the resistance and induce a small pressure gradient from the inlet of a bypass, causing a competitive flow through it and reducing its long-term patency.…”
Section: Velocity Fieldssupporting
confidence: 92%
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“…As the degree of stenosis increased, the use of the bypass became more effective. These findings were consistent with those of Ko et al 14 and Vimmr et al, 19 who asserted that stenosis degree smaller than 50% was commonly described as hemodynamically insignificant because there was no impact on the blood supply to downstream tissues. Furthermore, according to Fan et al, 21 the resistance and induce a small pressure gradient from the inlet of a bypass, causing a competitive flow through it and reducing its long-term patency.…”
Section: Velocity Fieldssupporting
confidence: 92%
“…These results showed that the diameter ratio D 1 /D had a more significant effect on the pressure drop than α. The prominent influence of the D 1 /D ratio compared to the α angle had been confirmed experimentally 45 and numerically [17][18][19] in idealized steady and pulsatile stenotic flows. Tsukui et al 45 also confirmed that a smaller junction angle (α) yielded lower energy loss at bypass graft.…”
Section: Model Verificationmentioning
confidence: 72%
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“…The space discretisation of the system of Equations is performed with the cell‐centred finite volume method for hybrid unstructured tetrahedral grids . The hybrid grid system defines the values of pressure and Cartesian velocity components in the centre of the control volume Ω k , and the values of face‐normal velocity V m , which have the direction of outward unit vector nkm normal to the m th face Γkm of the control volume Ω k , are defined in the middle of the face Γkm (Figure ).…”
Section: Methodsmentioning
confidence: 99%