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)16.415.216.310.3
Averaged load value corresponding to the potential fracture (N)9500880094005900
Impact energy required to cause the fracture (J)41.035.440.616.4