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8.5 PATIENT-SPECIFIC CARDIAC PODI COMPUTATION                    169

                           TABLE 8.8 Cube Grid With Different Mesh Discretizations
                           Cube grid     CG-1       CG-2      CG-3      CG-4       CG-5      CG-6
                           Nodes          294       336        448       504        720       990




                                            0.5
                                                                   Displacement
                                                                       LV-PV
                                           0.45
                                            0.4

                                         L 2  error   0.35
                                            0.3
                                           0.25

                                            0.2
                                           0.15
                                              200   300   400   500   600   700   800   900  1000
                                                          Num of grid nodes
           FIG. 8.31  Change in ε BV R -norm as the number of grid nodes increases.
                             ‘ 2

                         TABLE 8.9  Change in the Error and Calculation Time as the Number of Grid Nodes Increases
                                                  L 2 -error                     Calculation time (s)
                                       Displacement       Visual              Total         Projection
                         CG-2          0.45               Deformations        232          219
                         CG-6          0.36               Deformations        643          628



           as shown in Fig. 8.32, with the nodes lying inside the wall showing improvement while the lateral wall of the RV
           exhibits more expansion. However, when the deformed state is more closely investigated, the localized nonphysical
           deformations are still dominant on the surfaces of the geometry and the magnitude of the displacement field is notice-
           ably lower, as depicted in Fig. 8.30C. The most significant solution improvements can be found at the epicardium sur-
           face of the RV.
              Regarding the PODI calculation time, it is found to be increasing almost linearly because more grid nodes are pre-
           sent, as shown in Fig. 8.33. This is due to the fact that the PIP algorithm and the template projections require more time.
              The three most dominant POMs are found to be needed in order to reach the minimum specified energy limit for the
           displacement, strain and stress field data. Further investigation of the POVs reveals that the energy of the first, second,
           and third POMs is about 61.6%, 30.5%, and 7.8%, respectively. The fourth POM is below 1.04   10  14 %. This is in
           contrast to Rama et al. [34], where the first POM already accounted for about 99% of the energy. The cube standard-
           ization method obviously has a scattering effect leading to dataset matrices, U i , with disorganized data due to the



                                                                                            Displacement
                                                                                              1.588e+01
                                                                                              11.909
                                                                                              7.9394
                                                                                              3.9697
                                                                                              2.201e-05
                        (A)                    (B)                      (C)
           FIG. 8.32  PODI displacement field plot based on the cube template standardization method for different numbers of grid nodes. (A) PODI with
           294 grid nodes. (B) PODI with 990 grid nodes. (C) EFG.



                                                       I. BIOMECHANICS
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