Bioengineering Center, Wayne State University, Detroit, MI 48201, USA.
Biomech Model Mechanobiol. 2012 Mar;11(3-4):341-53. doi: 10.1007/s10237-011-0314-2. Epub 2011 May 18.
A combined experimental and numerical study was conducted to determine a method to elucidate the biomechanical response of a head surrogate physical model under air shock loading. In the physical experiments, a gel-filled egg-shaped skull/brain surrogate was exposed to blast overpressure in a shock tube environment, and static pressures within the shock tube and the surrogate were recorded throughout the event. A numerical model of the shock tube was developed using the Eulerian approach and validated against experimental data. An arbitrary Lagrangian-Eulerian (ALE) fluid-structure coupling algorithm was then utilized to simulate the interaction of the shock wave and the head surrogate. After model validation, a comprehensive series of parametric studies was carried out on the egg-shaped surrogate FE model to assess the effect of several key factors, such as the elastic modulus of the shell, bulk modulus of the core, head orientation, and internal sensor location, on pressure and strain responses. Results indicate that increasing the elastic modulus of the shell within the range simulated in this study led to considerable rise of the overpressures. Varying the bulk modulus of the core from 0.5 to 2.0 GPa, the overpressure had an increase of 7.2%. The curvature of the surface facing the shock wave significantly affected both the peak positive and negative pressures. Simulations of the head surrogate with the blunt end facing the advancing shock front had a higher pressure compared to the simulations with the pointed end facing the shock front. The influence of an opening (possibly mimicking anatomical apertures) on the peak pressures was evaluated using a surrogate head with a hole on the shell of the blunt end. It was revealed that the presence of the opening had little influence on the positive pressures but could affect the negative pressure evidently.
一项联合实验和数值研究旨在确定一种方法,以阐明在空气冲击波加载下头部替代物理模型的生物力学响应。在物理实验中,将充满凝胶的蛋形颅骨/脑替代物暴露于冲击波管环境中的爆炸超压下,并在整个事件过程中记录冲击波管和替代物内的静态压力。使用欧拉方法开发了冲击波管的数值模型,并通过实验数据进行了验证。然后利用任意拉格朗日-欧拉(ALE)流固耦合算法来模拟冲击波与头部替代物的相互作用。在模型验证后,对蛋形替代物的有限元模型进行了全面的参数研究系列,以评估几个关键因素(例如壳的弹性模量、核的体积模量、头部方向和内部传感器位置)对压力和应变响应的影响。结果表明,在所研究的范围内增加壳的弹性模量会导致超压的显著升高。改变核心的体积模量从 0.5 到 2.0 GPa,超压增加了 7.2%。面向冲击波的表面曲率对正、负峰值压力都有显著影响。与尖端面向冲击波前缘的模拟相比,钝端面向冲击波前缘的头部替代物的模拟具有更高的压力。使用钝端外壳上有孔的替代头部评估了开口(可能模拟解剖孔)对峰值压力的影响。结果表明,开口的存在对正压力几乎没有影响,但可能对负压力有明显影响。