Skip to content

Elastic Static Analysis Examples Using Realistic Models

Analysis Models

Table 9.2.1 lists the verification examples using realistic models for elastic static analysis. The model geometries, with some exceptions, are also shown in Figures 9.2.1 through 9.2.5. A separate direct solver is required to run the examples using element types 731 and 741.

Table 9.2.1 Verification examples using realistic models for elastic static analysis

Case Name Element Type Verification Model Number of Nodes Degrees of Freedom
EX01A 342 Connecting rod (100,000 nodes) 94,074 282,222
EX01B 342 Connecting rod (330,000 nodes) 331,142 993,426
EX02 361 Block with a hole 37,386 112,158
EX03 342 Turbine blade 10,095 30,285
EX04 741 Cylindrical shell 10,100 60,600
EX05A 731 Wine glass (coarse) 7,240 43,440
EX05B 731 Wine glass (medium) 48,803 292,818
EX05C 731 Wine glass (fine) 100,602 603,612

Connecting rod (EX01A)

Figure 9.2.1 Connecting rod (EX01A)

Block with a hole (EX02)

Figure 9.2.2 Block with a hole (EX02)

Turbine blade (EX03, EX06)

Figure 9.2.3 Turbine blade (EX03, EX06)

Cylindrical shell (EX04, EX09)

Figure 9.2.4 Cylindrical shell (EX04, EX09)

Wine glass (EX05, EX10A)

Figure 9.2.5 Wine glass (EX05, EX10A)

Analysis Results

Example Analysis Results

Examples of the analysis results are shown in Figures 9.2.6 through 9.2.9.

EX01A analysis results (Mises stress and deformed shape; deformation scale factor: 10)

Figure 9.2.6 EX01A analysis results (Mises stress and deformed shape; deformation scale factor: 10)

EX02 analysis results (Mises stress and deformed shape; deformation scale factor: 100)

Figure 9.2.7 EX02 analysis results (Mises stress and deformed shape; deformation scale factor: 100)

EX03 analysis results (deformed shape; deformation scale factor: 10)

Figure 9.2.8 EX03 analysis results (deformed shape; deformation scale factor: 10)

EX04 analysis results (deformed shape; deformation scale factor: 100)

Figure 9.2.9 EX04 analysis results (deformed shape; deformation scale factor: 100)

Analysis Performance Verification Results Using Example EX02

A model equivalent to the EX02 block-with-a-hole verification model was analyzed using general-purpose commercial software. Figure 9.2.10 compares the maximum and minimum stress-component values with those obtained by FrontISTR. The figure shows that the stress components agree very closely.

Next, the effect of domain decomposition on the stress distribution was investigated. The RCB method was used to divide the model into two parts along each of the X, Y, and Z axes, for a total of eight domains. Figure 9.2.11 shows the decomposition. Figure 9.2.12 shows the stress distributions obtained using a single domain and an eight-domain decomposition.

Comparison of EX02 stress components with general-purpose commercial software

Figure 9.2.10 Comparison of EX02 stress components with general-purpose commercial software

EX02 divided into eight domains using the RCB method

Figure 9.2.11 EX02 divided into eight domains using the RCB method

Difference in Mises stress distribution due to domain decomposition

Figure 9.2.12 Difference in Mises stress distribution due to domain decomposition

Figure 9.2.12 shows no difference between the two results; they agree completely.

Table 9.2.2 compares execution times for the HEC-MW solver settings used. Figure 9.2.13 also shows the convergence history until the solution is obtained.

Table 9.2.2 Comparison of execution times using HEC-MW solvers

Solver Execution Time (s)
CGI 38.79
CGscale 52.75
BCGS 60.79
CG8 6.65

Comparison of convergence histories using HEC-MW solvers (convergence threshold: 1.0×10⁻⁸)

Figure 9.2.13 Comparison of convergence histories using HEC-MW solvers (convergence threshold: \(1.0 \times 10^{-8}\))

Computation Time Comparison Using Verification Example EX01A

Verification example EX01A (connecting rod) was used to evaluate the speedup in computation achieved by domain decomposition. The computation used a 24-node cluster computer with Xeon 2.8 GHz processors. The results are shown in Figure 9.2.14. The figure shows that computation speed increases in proportion to the number of domains.

Differences in computation time between computer environments were also investigated. The results are shown in Table 9.2.3.

Speedup from domain decomposition

Figure 9.2.14 Speedup from domain decomposition

Table 9.2.3 Comparison of computation times by computer (1 CPU)

CPU Frequency (GHz) OS CPU Time (s) solver time (s)
Xeon 2.8 Linux 850 817
Pentium III 0.866 Win2000 2008 1980
Pentium M 0.760 WinXP 1096 1070
Pentium 4 2.0 WinXP 802 785
Pentium 4 2.8 WinXP 738 718
Celeron 0.700 Win2000 2252 2215
Pentium 4 2.4 WinXP 830 804