A study has been undertaken to identify the fundamental mechanisms involved during non-penetrating thoracic impact and in particular to determine how energy is transfered from the contact point on the thoracic wall to other sites inside the thorax.
Modelling of the thorax has been performed using the dynamic finite element codes DYNA2D and DYNASD and the system modelling package GENDYN. Particular consideration has been given to the mechanisms by which pressure waves are generated, the propagation of these waves through the lung, parenchyma and the likely biophysical mechanisms involved in vascular injury.
The finite element method has been used to demonstrate the propagation of the pressure wave through the lung, including reflection at boundaries, and identifying regions where stress concentration and contusion damage may occur.