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Large transverse deformation of double-layered rectangular plates subjected to gas mixture detonation load

机译:双层矩形板在混合气体爆轰作用下的大横向变形

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A series of twenty experimental tests were first carried out to assess the large transverse deformation of double-layered rectangular plates subjected to gas mixture detonation load. Specimens were made from a combination of an aluminum alloy front layer (the impulse-receiving face) and a mild steel back layer. Four different types of thickness configurations, namely, 1 mm + 1 mm, 2 mm + 1 mm, 1 mm + 2 mm, and 2 mm + 2 mm were selected to bring an insight into the influence of back and front layer thicknesses on the deformation resistance of double-layered plates. Each specimen group was subjected to five different pre-detonation pressures of acetylene and oxygen mixture. Quantitative experimental results were obtained and discussed in detail. The experimental results showed that the back layer deflection was approximately equal to the front layer deflection when there was no gap between the layers and the front layer had a lower strength and density than the back layer. A closed-form analytical model based on energy method was developed for double-layered plates subjected to the uniform impulsive loading. Furthermore, empirical design formulae were derived based on new dimensionless numbers to predict the maximum permanent deflection of back and front layers. The influence of strain rate sensitivity of materials was considered in both analytical and empirical models. An encouraging agreement between the experimental, analytical and empirical results in terms of the normalized deflection was achieved.
机译:首先进行了一系列的二十项实验测试,以评估双层矩形板在混合气体爆轰载荷作用下的大横向变形。样品由铝合金前层(脉冲接收面)和低碳钢后层的组合制成。选择了四种不同类型的厚度配置,即1 mm + 1 mm,2 mm + 1 mm,1 mm + 2 mm和2 mm + 2 mm,以洞察背面和正面层厚度对厚度的影响。双层板的抗变形性。每个标本组均经受五个不同的乙炔和氧气混合物的爆轰压力。获得了定量的实验结果并进行了详细讨论。实验结果表明,当各层之间没有间隙时,背层挠度大约等于前层挠度,并且前层的强度和密度低于背层。建立了基于能量方法的密闭分析模型,用于双层板在均匀冲击载荷作用下的变形。此外,基于新的无量纲数得出经验设计公式,以预测后层和前层的最大永久挠度。在分析和经验模型中都考虑了材料的应变速率敏感性的影响。实验,分析和经验结果在归一化挠度方面达成了令人鼓舞的协议。

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