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Chapter 2 Implementation of a patient-specific cardiac model 87



















                     Figure 2.32. Cross-sectional flow variation with the peristaltic amplitude. An
                     excellent match with theory is obtained.


                     where R(x,t) is the vessel radius. In the simulations R 0 = 0.5 mm,
                     R max = 0.3 mm and the length of the vessel was 2 mm. The time
                     period was one second (see Fig. 2.33.)








                     Figure 2.33. Time variation of the geometry of the expanding and contracting
                     vessel.

                        Computations with the above described setup were performed
                     and flow rates were compared with analytical solutions. Since the
                     fluid is incompressible, the flow rate should be equal to the vol-
                     ume change. The volume change was calculated analytically from
                     the surface equations describing the geometry. Inlet and outlet
                     flow rates were computed on planes located at the inlet and outlet
                     section, respectively. Results in Fig. 2.34 show that the simulated
                     flow rates follow the analytical curve almost perfectly. Further-
                     more, the total flow rate (computed through a center cross sec-
                     tion) was within 2 percent of the total analytical volume change.


                     Output of the FSI system with patient-specific data
                        In Fig. 2.35 we visualize results from a typical FSI computation
                     using the presented algorithm, with cardiac geometry extracted
                     from MRI images and valve geometry from 3D Ultrasound. Three-
                     dimensional ventricular blood velocities and pressure fields, as
                     well as myocardial stresses are available at all the points in the do-
                     main. Velocity fields display realistic patterns, including posterior
                     jet deflection and mitral vortex appearance. The use of the kineto-
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