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ACME 2011 Proceedings of the 19 UK National Conference of the ...

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discontinuities are permitted to share <strong>the</strong> same location at <strong>the</strong> start <strong>of</strong> <strong>the</strong> branch in human arterial tree [4].<br />

2 METHODOLOGY<br />

The 1D first order hyperbolic governing equations <strong>of</strong> an elastic cylindrical vessel <strong>of</strong> incompressible and<br />

Newtonian fluid, based on <strong>the</strong> mass and momentum conservation laws can be written as [4]:<br />

where A is <strong>the</strong> cross-sectional area <strong>of</strong> <strong>the</strong> vessel, u is mean velocity <strong>of</strong> <strong>the</strong> fluid, p is <strong>the</strong> internal pressure<br />

<strong>of</strong> <strong>the</strong> cross-section , is <strong>the</strong> blood density (assumed to be constant due to incompressibility <strong>of</strong> blood) and<br />

is <strong>the</strong> shear stress where is <strong>the</strong> dynamic viscosity (constant), r is <strong>the</strong> radial direction in<br />

3D cylindrical coordinates and R is <strong>the</strong> vessel radius. In <strong>the</strong> shear stress term, <strong>the</strong> inertia component will<br />

be neglect while <strong>the</strong> viscous component is assumed as a fully developed Newtonian steady flow with a<br />

parabolic velocity pr<strong>of</strong>ile (Poiseuille flow) which can be expressed as:<br />

In order to close <strong>the</strong> system, equations (1) and (2) have to be supplemented with a commonly used<br />

pressure-area relation [7] which takes <strong>the</strong> form:<br />

where is <strong>the</strong> external pressure from <strong>the</strong> surrounding tissues, is <strong>the</strong> unstressed cross-sectional area<br />

<strong>of</strong> <strong>the</strong> vessel, is <strong>the</strong> material properties <strong>of</strong> <strong>the</strong> elastic vessel, h is <strong>the</strong> vessel wall thickness, E is <strong>the</strong><br />

Young’s modulus and is <strong>the</strong> Poisson’s ratio.<br />

The explicit semi-discrete form can <strong>the</strong>n be achieved by using <strong>the</strong> standard second-order Taylor series<br />

expansion and <strong>the</strong> partial differential equation is used to replace <strong>the</strong> time derivatives with spatial<br />

derivatives which can be shown as:<br />

where U, F and S are vectors <strong>of</strong> <strong>the</strong> primitive variables, conservative variables and source term<br />

respectively. The semi-discrete form will <strong>the</strong>n be fur<strong>the</strong>r discretised using <strong>the</strong> LCG finite element method.<br />

As with <strong>the</strong> global Galerkin method, each <strong>of</strong> <strong>the</strong> variables is approximated by <strong>the</strong> standard finite element<br />

spatial discretisation. The interface flux can be reintroduced via integration by parts and contained<br />

contributions from convective component. In order to achieve local conservation, a simple averaging<br />

post-processing procedure is introduced at each time step. The post-processing procedure uses <strong>the</strong> nodal<br />

values from <strong>the</strong> continuous solution obtained from <strong>the</strong> previous time-step to provide an accurate interface<br />

flux and also establishes connectivity between elements at <strong>the</strong> next time-step. Full discrete form <strong>of</strong> <strong>the</strong><br />

governing equations is shown in [4, 5, 6].<br />

,<br />

(1)<br />

(2)<br />

(3)<br />

(4)<br />

(5)<br />

30

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