芯型对铝蜂窝板静动力性能影响的实验与数值研究

IF 5 Q1 ENGINEERING, MULTIDISCIPLINARY
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引用次数: 0

摘要

夹芯板采用蜂窝芯,这是一种广泛使用的复合材料结构,被认为是复合材料的基本分类。由一个类似蜂窝的核心组成,具有厚度和柔软性,并且侧面由刚性面片夹夹各种形状和材料。本文对铝蜂窝夹层复合材料轻量化板进行了静动力分析研究。蜂窝夹芯板样品长300 mm,宽300 mm,高度(10、15、20、25)mm不等。铝蜂窝芯采用电阻点焊(RSW)技术制造,取代了工业缺陷检测中常用的粘结材料。基于响应面法(RSM)的数值优化和实验软件设计(DOE)对现有工作进行了验证。对不同设计参数下蜂窝夹芯板的耐撞性能(最大弯曲载荷、最大挠度)和振动属性(固有频率、阻尼比、瞬态时间响应)进行了理论研究。此外,利用基于有限元法的ANSYS软件对理论结论进行了验证。本工作的发现表明,固有频率,核心高度和细胞大小之间的关系是直接的。相反,固有频率与细胞壁厚度之间的关系是相反的。相反,阻尼比与核心高度和细胞大小成反比,而与细胞壁厚度成正比。研究表明,将岩心高度改变在10 ~ 25 mm范围内,固有频率显著提高82 %,阻尼比显著降低49 %。这些发现是基于特定的细胞尺寸值0.01 m和细胞壁厚度0.001 m。此外,结果表明,对于一组给定的细胞壁厚度和尺寸值,岩心高度从0.01 m增加到0.025 m,导致最大瞬态响应百分比降低约76 %。相反,当芯高为0.015 m时,细胞壁厚度从0.3到0.7 mm增加,最大瞬态响应降低了7.8 %。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental and numerical study of effecting core configurations on the static and dynamic behavior of honeycomb plate with aluminum material

The sandwich panel incorporated a honeycomb core, a widely utilized composite structure recognized as a fundamental classification of composite materials. Comprised a core resembling a honeycomb, possessing thickness and softness, and is flank by rigid face sheets that sandwich various shapes and materials. This paper presents an examination of the static and dynamic analysis of lightweight plates made of aluminum honeycomb sandwich composites. Honeycomb sandwich plate samples are 300 mm long, and 300 mm wide, the heights of the core have been varied at four values ranging from 10 to 25 mm. The honeycomb core is manufactured from Aluminum material by using a novel technique namely resistance spot welding (RSW) instead of using adhesive material, which is often used when an industrial flaw is detected. Numerical optimization based on response surface methodology (RSM) and design of experiment software (DOE) was used to verify the current work. A theoretical examination of the crashworthiness behavior (maximum bending load, maximum deflection) and vibration attributes (natural frequency, damping ratio, transient temporal response) of honeycomb sandwich panels with different design parameters was also carried out. In addition, the finite element method-based ANSYS software was used to confirm the theoretical conclusions. The findings of the present work showed that the relationship between the natural frequency, core height, and cell size is direct. In contrast, the relationship between the natural frequency and the thickness of the cell wall is inverse. Conversely, the damping ratio is inversely proportional to the core height and cell size but directly proportional to the thickness of the cell wall. The study indicates that altering the core height within 10–25 mm leads to a significant increase of 82 % in the natural frequency and a notable decrease of 49 % in the damping ratio. These findings are based on a specific cell size value of 0.01 m and a cell wall thickness of 0.001 m. Also, the results indicate that for a given set of cell wall thickness and size values, an increase in core height from (0.01–0.025) m, leads to a reduction of the percentage of maximum response approximately 76 %. Conversely, the increasing thickness of the wall of cell wall, ranging 0.3–0.7 mm with a constant core height equal to 0.015 m, resulted in a de crease of maximum transient response by 7.8 %.

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来源期刊
Defence Technology(防务技术)
Defence Technology(防务技术) Mechanical Engineering, Control and Systems Engineering, Industrial and Manufacturing Engineering
CiteScore
8.70
自引率
0.00%
发文量
728
审稿时长
25 days
期刊介绍: Defence Technology, a peer reviewed journal, is published monthly and aims to become the best international academic exchange platform for the research related to defence technology. It publishes original research papers having direct bearing on defence, with a balanced coverage on analytical, experimental, numerical simulation and applied investigations. It covers various disciplines of science, technology and engineering.
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