Table 3 Summary of the analysis.
Model type | Time of the first fracture occurrence within the orbit (ms) | External load value corresponding to the first fracture occurrence (N) | Potential fracture area during the maximal load (mm2) |
|---|---|---|---|
Bones only model (MOBE) | 13.3 | 7,660 | 270 |
Contact model (MOBOSE) | 14.8 | 8,520 | 215 |