Numerical Analysis of Armored Fighting Vehicle Escape Hatch Subjected to Mine Blast Loading Using Coupled Eulerian-Lagrangian Technique

IF 0.6 Q4 TRANSPORTATION SCIENCE & TECHNOLOGY SAE International Journal of Materials and Manufacturing Pub Date : 2023-03-30 DOI:10.4271/05-16-03-0017
Sundaresan Parthasarathy, J. R. Kumar
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Abstract

This article describes the research work taken to compare the effect of air blast and surface-buried mine blast loading on an armored fighting vehicle (AFV) escape hatch, using the coupled Eulerian-Lagrangian (CEL) technique. Two types of escape hatch were considered for the study, namely, the flat plate version and double-side curved-plate version. To evaluate the research methodology used in this investigation, initially, a published experimental work on a circular plate subjected to air blast was chosen and a benchmark simulation was carried out using the CEL technique to establish the simulation procedure. Then the established procedure was utilized for further analysis. It was observed that the variation in the deformation between the published literature and the simulation work was well within the acceptable engineering limits. After that, numerical studies were conducted on the flat and double-side curved hatch by subjecting it to both air blast and surface-buried mine blast loading using the previously established CEL technique. The results of the peak central deflection of the hatch and the transmitted impulse to the base structure were compared for each type of loading case. It was systematically established that the double-side curved hatch gives better protection to the crew against both air blast loading and surface-buried mine blast loading situations.
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利用欧拉-拉格朗日耦合技术对地雷爆炸载荷作用下装甲战车逃生舱口进行数值分析
本文采用耦合欧拉-拉格朗日(CEL)方法,比较了空气爆炸和地埋地雷爆炸载荷对装甲战车(AFV)逃生舱口的影响。本研究考虑了两种类型的逃生舱口,即平板型和双面弯板型。为了评估本研究中使用的研究方法,首先选择了一份已发表的关于空气爆炸作用下圆形板的实验工作,并使用CEL技术进行基准模拟,以建立模拟程序。然后利用所建立的程序进行进一步分析。观察到,已发表的文献和模拟工作之间的变形变化完全在可接受的工程范围内。在此基础上,利用已有的CEL技术,对平面和双面弯曲舱口进行了空气爆炸和地表矿井爆炸载荷的数值研究。对比了不同载荷情况下舱口中心挠度峰值和传递给基础结构的冲击。系统地证实了双面弧形舱口对机组人员在空气爆炸载荷和地雷爆炸载荷下都有较好的保护作用。
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来源期刊
SAE International Journal of Materials and Manufacturing
SAE International Journal of Materials and Manufacturing TRANSPORTATION SCIENCE & TECHNOLOGY-
CiteScore
1.30
自引率
12.50%
发文量
23
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