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M型皱褶芯材夹层板隔声性能研究

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作为先进复合材料夹层结构,皱褶芯材构型多样,先前研究大多围绕V型皱褶芯材展开,鲜有对其他构型的隔声性能研究.建立垂直入射声压激励下的四边简支M型皱褶芯材夹层板数值模型,基于有限元软件对其隔声性能进行数值仿真,并将理论预测的蜂窝夹层板隔声曲线与仿真结果进行对比;基于仿真模型,研究M型皱褶芯材夹层板结构的隔声性能,讨论皱褶芯材胞元几何参数对隔声性能的定性影响规律;研究双层芯材的M型皱褶芯材夹层板上下两层芯材的相对铺设错位、铺设角度对隔声性能的影响.结果表明:上下两层芯材在胞元Z形线步长方向错位叠放时隔声效果提高,且优于同面密度的单层皱褶芯材夹层板;在上下两层芯材相对铺设角度变化时,上下层芯材轴线垂直铺设时计权隔声量最大.
Research on sound insulation performance of the M-type folded core sandwich panel
As an advanced composite sandwich structure,the configuration of folded core is diverse,and previous research has mostly focused on the V-shaped folded core,while there is still relatively little research on the sound insulation performance of other configurations.A numerical model of a four sided simply supported M-shaped fold-ed core sandwich panel under vertical incident sound pressure excitation is established,and the numerical simulation of its sound insulation performance based on finite element software is conducted.The theoretical predicted sound transmission loss curve of the honeycomb sandwich panel is compared with the simulation results.Based on simula-tion models,the sound insulation performance of M-type folded core sandwich panel structure is systematically studied,and the qualitative influence of geometric parameters of folded core cell on sound insulation performance is discussed.The influence of relative misalignment and laying angle of the upper and lower layers of M-type folded core sandwich panel with double-layer core on sound insulation performance is proposed and studied.The results show that the sound insulation performance is improved when the upper and lower layers of core are staggered and stacked in the Z-shaped line step direction of the cell,and it is better than single-layer folded core sandwich panel with the same surface density.When the relative laying angle of the upper and lower layers of core changes,the maximum weighted sound insulation reached the most value while the axis of the upper and lower layers of core is vertically laid.

sandwich panelM-type folded core sandwich panelcellular parameterssound insulation perfor-mancedouble-layer corelaying method

叶语睿、王志瑾

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南京航空航天大学 航空学院,南京 210016

夹层板 M型皱褶芯材 胞元参数 隔声性能 双层芯材 铺设方式

2024

航空工程进展
中国航空学会 西北工业大学

航空工程进展

CSTPCD
影响因子:0.207
ISSN:1674-8190
年,卷(期):2024.15(5)
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