Research Article
Validation of Hydraulic Mechanism during Blowout Trauma of Human Orbit Depending on the Method of Load Application
Table 2
Summary of the nonlinear transient analysis regarding the contact problem (MOBOSE).
| | Initiation points of the potential orbital wall fracture | Lower wall (1) (node no. 141) | Lower wall (2) (node no. 242) | Lower wall (3) (node no. 244) | Medial wall (4) (node no 116) |
| Time of reaching the ultimate stress threshold (150 MPa) (ms) | 16.4 | 15.2 | 16.3 | 10.3 | Averaged load value corresponding to the potential fracture (N) | 9500 | 8800 | 9400 | 5900 | Impact energy required to cause the fracture (J) | 41.0 | 35.4 | 40.6 | 16.4 |
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