Assessing the effect of chest orientation on pulmonary pressure under free field shock waves: a numerical analysis.

Acta of bioengineering and biomechanics Pub Date : 2025-01-28 Print Date: 2024-06-01 DOI:10.37190/abb-02427-2024-04
Zhuangqing Fan, Shuangbo Zhang, Huifang Gan, Jing Chen, Changkai Dai, Benwen Zhang, Fangyun Lu, Jinlong Qiu, Jianyi Kang
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Abstract

Purpose: This study explores how thoracic orientation affects lung pressure and injury outcomes from shock waves, building on earlier research that suggested human posture impacts injury severity. Methods: A layered finite element model of the chest was constructed based on the Chinese Visual Human Dataset (CVH), including the rib and intercostal muscle layers. The dynamic response of the chest under 12 different angle-oriented shock waves under incident pressures of 200 kPa and 500 kPa was calculated. The correspondence between lung pressure at various angles, chest wall motion velocity and lung stress, and differences in pressure/stress of lung tissue behind ribs and intercostal muscle were analyzed. Results: The dynamic response of the chest can be roughly divided into four processes. High local intrapulmonary pressure areas were primarily in the anterior lobe margin and the lung's central region. A 500 kPa incident wave at 0° could cause slight lung injury, whereas at 240°, the pressure was non-harmful. Lung tissue pressure and stress induced by chest wall movement were significantly higher behind the intercostal muscles than behind the ribs, with a difference of about 2-3 times. Conclusions: This layered model provides a cost-effective tool for large-scale shock wave impact simulations on the chest. Chest wall movement velocity strongly correlates with lung stress distribution. The significant density and sound velocity differences among ribs, intercostal muscles and lungs cause an acoustic impedance mismatch, leading to "striped bleeding" marks in post-impact lungs. This research enhances understanding of chest and lung injury mechanisms and informs the development of protective measures.

评估胸廓朝向对自由场冲击波下肺压力的影响:数值分析。
目的:在早期研究表明人体姿势影响损伤严重程度的基础上,本研究探讨了胸椎方向如何影响肺压力和冲击波损伤结果。方法:基于中国视觉人体数据集(CVH)构建胸腔分层有限元模型,包括肋骨层和肋间肌层。计算了200 kPa和500 kPa入射压力下12种不同角度激波对胸部的动力响应。分析不同角度肺压力、胸壁运动速度与肺应力的对应关系,以及肋后肺组织和肋间肌的压力/应力差异。结果:胸部动态响应大致可分为四个过程。局部高肺内压区主要位于肺前叶边缘和肺中央区域。在0°时,500 kPa的入射波可造成轻微的肺损伤,而在240°时,入射波对肺无害。胸壁运动引起的肺组织压力和应激在肋间肌后明显高于肋骨后,差异约为2-3倍。结论:该分层模型为大规模胸部冲击波冲击模拟提供了一种经济有效的工具。胸壁运动速度与肺应力分布密切相关。肋骨、肋间肌肉和肺部之间的显著密度和声速差异导致声阻抗不匹配,导致撞击后肺部出现“条纹出血”痕迹。这项研究提高了对胸部和肺部损伤机制的理解,并为保护措施的制定提供了信息。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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