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Table 2: Time required for the different parts of the simu- lation: detect the affected faces, project the feature points, adaptive mesh refinement, and the other parts of the sim- ulation.
"... In PAGE 7: ... This is an important advantage of our empirical method over physically based approaches: the user has intuitive control over the system and can interactively see the resulting aging effects. We can see from Table2 that the most time-consuming parts are finding the affected faces and adaptively refining the model. Since the tool is usually small relative to the object, we took great care to quickly identify and keep track of the small set of affected faces and vertices that go through each stage of a simulation step.... ..."
Table 4 FE results versus mesh refinement a 0)
1999
"... In PAGE 14: ... In addition, the three nodes along one of the sides of each of the quadrilateral element are collapsed at the crack tip and the two adjoining mid points are moved to the quarter distances, in order to produce 1=r1=2 type of singularity. Table4 shows that the FE results can converge to a particular value along with the mesh refinement. It can be seen from Fig.... ..."
Table 1. SED intensity factors versus mesh refinement
1999
"... In PAGE 6: ...f each crack. In Fig. 5 the coefficients of SED intensity factors bi at point A (see Fig. 4) are presented as a function of crack orientation angle a for N 40, where bi are de- fined by (Qin, 1998) KI A h0cc33b1 a pc p =k KIII A h0cc11b2 a pc p =k 70 KD A h0cv3bD a pc p =k with c11 c33 v3 8 lt; : 9 = ; C1111 C1133 e311 C1133 C3333 e333 e311 e333 j33 2 4 3 5 a11 a33 k3 8 lt; : 9 = ; 71 Table1 shows the results of SED intensity factors at point A versus mesh refinement for a 0. However, the nu- merical results for such a problem have not been available in the literature yet.... In PAGE 7: ...Table1 shows that the results of SED intensity factors from both BEM and FEM can con- verge to a particular value along with the mesh refinement. It is found from Fig.... ..."
Cited by 3
Table 1: Influence of mesh refinement on computed energy release rates
in Three Dimensional Finite Element Analysis of Multidirectional Composite DCB, SLB and ENF Specimens
1994
Cited by 5
Table 1: Pseudo-code for recursive mesh refinement and triangle stripping.
"... In PAGE 6: ....1.3 Run-Time Refinement With all the necessary pieces in hand, we now summarize the al- gorithm for top-down refinement and on-the-fly triangle strip con- struction. Pseudo-code for these steps is listed in Table1 . The re- finement procedure builds a triangle strip V =(v0;v1;v2;:::;vn), that is represented as sequence of vertex indices.... In PAGE 7: ... construction is the same as in [17]. A vertex v is appended to the strip using the procedure tstrip-append ( Table1 ). Line 5 is used to turn corners in the triangulation by effectively swapping the two most recent vertices, which results in a degenerate triangle that is discarded by the graphics system [9].... ..."
Table 1: Listing of number of nodes and cells for different mesh refinement levels
Table 1: Mesh refinement and coarsening times (in sec.) for the spherical harmonic data set
"... In PAGE 8: ... Even for those large compression fac- tors, the quality of the approximation is very good as it can be seen in Figure 3. In Table1 we give for various hierarchy levels the total number of vertices, (regular) tetrahedra, octahedra, and ir- regular elements for the spherical harmonic data set together with the CPU times for incremental mesh refinement and coarsening. In Table 2 the same information is given for the abdomen data set.... ..."
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