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Life science special report 161215 IY opt

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LIFE SCIENCES VIRTUAL ABDOMINAL AORTIC ANEURYSM<br />

PRE-PROCESSING<br />

Different mesh topologies and<br />

grid refinements were assessed<br />

(Figure 3) using STAR-CCM+. These<br />

were based on polyhedral, nonconformal<br />

hexahedral and tetrahedral<br />

elements, all with boundary layer<br />

extrusion to accurately calculate<br />

the velocity gradient near the walls<br />

of the vessel. For the sensitivity<br />

analysis of the grid, the verification<br />

procedure proposed by Roache [1]<br />

was followed. The mesh size varied<br />

from 300,000 to roughly 1,400,000<br />

cells. In addition, the influence of<br />

the boundary layer was taken into<br />

account by comparing the solutions<br />

obtained with various dimensions of<br />

prisms layer, as shown on Figure 4.<br />

FIGURE 4: Prism layer infl uence<br />

investigation<br />

SOLVING<br />

The physics and the solver setups had<br />

to be determined in order to automate<br />

the solving process. Two different<br />

types of fluids were compared to<br />

model the behavior of the blood: (a) a<br />

simple Newtonian fluid with standard<br />

properties and (b) a non-Newtonian<br />

fluid with Power-law rheology. The<br />

influence of the time step and number<br />

of inner iterations was assessed<br />

using the same systematic approach<br />

as ad<strong>opt</strong>ed for the mesh study.<br />

While keeping the physics and the<br />

solver parameters unchanged,<br />

different numerical schemes<br />

were tested and compared:<br />

• Solvers: segregated (S), coupled<br />

implicit (Ci) and coupled explicit (Ce)<br />

• Pressure/velocity coupling: first-order<br />

and second-order upwind convection<br />

schemes (pv1 and pv2 respectively)<br />

• Temporal discretization: first-order<br />

and second-order upwind convection<br />

scheme (t1 and t2 respectively)<br />

Figure 5 shows a comparison of OSI<br />

values computed with the different<br />

numerical schemes. In Figure 6,<br />

the time history for the benchmark<br />

model and the final average<br />

value of the velocity magnitude<br />

inside the vessel are <strong>report</strong>ed.<br />

POST-PROCESSING<br />

To visualize the numerical solution, scalar<br />

plots that show the variations of a number<br />

of parameters were drawn on the surface<br />

and inside the vessel. Furthermore, by<br />

exporting the solution-in-time, it was<br />

possible to integrate the Wall Shear Stress<br />

(WSS) components and compute the<br />

hemodynamic risk indices. Figure 7 shows<br />

a sample of post-processing images.<br />

FIGURE 3: Example of grid topology.<br />

A: tetrahedral based; B: polyhedral<br />

based; C: hexahedral based.<br />

The investigation about grid<br />

generation led to the definition of<br />

a discretization strategy which is<br />

suitable to represent the physics as<br />

realistically as possible.<br />

CONCLUSION<br />

This study assessed how the choice of<br />

grid, solver models and features of the<br />

fl uid (blood) affects the computation<br />

of some specifi c parameters (such as<br />

pressure, fl uid velocity, tension and<br />

stress state of the vessel) in the case<br />

of an abdominal aortic aneurysm. The<br />

investigation about grid generation<br />

led to the defi nition of a discretization<br />

strategy which is suitable to represent<br />

the physics as realistically as possible.<br />

Non-conformal hexahedral grids allow<br />

the representation of the phenomenon<br />

FIGURE 5: Oscillatory Shear Index (OSI)<br />

computed using different numerical schemes<br />

with fewer numerical discretization errors<br />

than the other non-structural grids; as a<br />

consequence, the use of a polyhedral or<br />

tetrahedral mesh implies a more refi ned<br />

grid and therefore a higher number<br />

of cells, which in turn requires more<br />

computational time and resources . It is<br />

also necessary to have a good resolution<br />

of the boundary layer to compute the<br />

WSS accurately. For the solving phase,<br />

a suitable time step and number of<br />

inner iterations, numerical scheme<br />

and fl uid rheology were extracted as<br />

parameters for the automation process.<br />

6 SPECIAL REPORT

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