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Study on the influence of design parameter variation on the dynamic behaviour of thermoplastic honeycomb panels

机译:设计参数变化对热塑性蜂窝板动力性能的影响研究

摘要

Sandwich panels are layered structures that consist of at least five layers : two thin face sheets that are bonded with bonding layers to the thick core. The core has a very low density whereas the face sheets are stiff and strong. The entire panel combines high mechanical properties with a very low areal mass. Most of the structural characteristics of the panel (material selection and thickness of each layer) can be selected independently of other parameters, and the overall characteristics of the panel depend on the particular selection of parameters. Because of the wide range of panel parameters, numerical modelling is useful to provide insight into the structural characteristics of a particular panel.This paper studies the effect of design parameter variations on the dynamic behaviour of honeycomb sandwich panels. The dynamic behaviour includes natural frequencies, mode shapes and damping of such panels with free boundary conditions.In the first section the structure of honeycomb sandwich panels is illustrated, in particular those with a ThermHex core. For a typical honeycomb panel the different design parameters are outlined.Natural frequencies and mode shapes can be predicted approximately using analytical models. Some of the methods are outlined in this article.The second section of the paper presents the numerical modelling of a sandwich panel using commercial finite element codes. Different core modelling strategies are compared, e.g. geometrically correct or as a homogenised equivalent material. Advantages and drawbacks of the different methods are outlined. Different ways of modelling damping in the panels are also presented.The third section discusses the experimental validation. To validate the finite element models, measurements are carried out on some test panels. Free-free boundary conditions are provided by elastically suspending the panels. To make measurements totally contactless, the test panels are excited acoustically and the vibration measurement is performed with a laser vibrometer. The way the data are captured and processed is also outlined.Measured natural frequencies and mode shapes are compared with the calculated results from the different FE models and the analytical models. The techniques that are used for this comparison are briefly discussed.The different FE models are updated using results from a sensitivity analysis. This analysis is performed theoretically for every design parameter and is discussed in detail. Results from the updated models are again compared with those obtained from measurements.The uncertainty on different design parameters is studied and discussed. The influence of these various uncertainties on the natural frequencies and mode shapes is investigated using Monte Carlo simulations.
机译:夹心板是至少由五层组成的分层结构:两块薄面板,通过粘结层粘结到厚芯上。芯的密度很低,而面板却又硬又结实。整个面板兼具高机械性能和极低的面积质量。面板的大多数结构特征(材料选择和每一层的厚度)可以独立于其他参数进行选择,面板的总体特征取决于特定的参数选择。由于面板参数的范围很广,因此数值建模有助于深入了解特定面板的结构特性。本文研究了设计参数变化对蜂窝夹心面板动力行为的影响。动态行为包括具有自由边界条件的此类面板的固有频率,振型和阻尼。在第一部分中,说明了蜂窝夹芯板的结构,特别是具有ThermHex芯的蜂窝夹心板的结构。对于典型的蜂窝板,其设计参数概述如下:可以使用分析模型大致预测固有频率和振型。本文概述了一些方法。本文的第二部分介绍了使用商业有限元代码对夹心板进行数值建模的方法。比较了不同的核心建模策略,例如几何上正确或均质的等效材料。概述了不同方法的优缺点。还介绍了面板中阻尼建模的不同方法。第三部分讨论了实验验证。为了验证有限元模型,在一些测试面板上进行了测量。通过弹性悬挂面板来提供自由边界条件。为了使测量完全无接触,可对测试面板进行声学激励,并使用激光振动计进行振动测量。还概述了数据的捕获和处理方式。将测得的固有频率和振型与来自不同有限元模型和分析模型的计算结果进行比较。简要讨论了用于此比较的技术。使用灵敏度分析的结果更新不同的有限元模型。理论上对每个设计参数都进行了此分析,并进行了详细讨论。再次将更新后的模型的结果与测量结果进行比较。研究并讨论了不同设计参数的不确定性。使用蒙特卡洛模拟研究了这些各种不确定性对固有频率和振型的影响。

著录项

  • 作者

    Debruyne Stijn;

  • 作者单位
  • 年度 2009
  • 总页数
  • 原文格式 PDF
  • 正文语种 en
  • 中图分类

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