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Damage modeling and damage detection for structures using a perturbation method.

机译:使用微扰方法进行结构的损伤建模和损伤检测。

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摘要

This thesis is about using structural-dynamics based methods to address the existing challenges in the field of Structural Health Monitoring (SHM). Particularly, new structural-dynamics based methods are presented, to model areas of damage, to do damage diagnosis and to estimate and predict the sensitivity of structural vibration properties like natural frequencies to the presence of damage.;Towards these objectives, a general analytical procedure, which yields nth-order expressions governing mode shapes and natural frequencies and for damaged elastic structures such as rods, beams, plates and shells of any shape is presented. Features of the procedure include the following:;1. Rather than modeling the damage as a fictitious elastic element or localized or global change in constitutive properties, it is modeled in a mathematically rigorous manner as a geometric discontinuity.;2. The inertia effect (kinetic energy), which, unlike the stiffness effect (strain energy), of the damage has been neglected by researchers, is included in it.;3. The framework is generic and is applicable to wide variety of engineering structures of different shapes with arbitrary boundary conditions which constitute self adjoint systems and also to a wide variety of damage profiles and even multiple areas of damage.;To illustrate the ability of the procedure to effectively model the damage, it is applied to beams using Euler-Bernoulli and Timoshenko theories and to plates using Kirchhoff's theory, supported on different types of boundary conditions. Analytical results are compared with experiments using piezoelectric actuators and non-contact Laser-Doppler Vibrometer sensors.;To illustrate the ability of the procedure to effectively model the damage, it is applied to beams using Euler-Bernoulli and Timoshenko theories and to plates using Kirchhoff's theory, supported on different types of boundary conditions. Analytical results are compared with experiments using piezoelectric actuators and non-contact Laser-Doppler Vibrometer sensors.;Assuming the damaged structure to be a linear system, the response is expressed as the summation of the responses of the corresponding undamaged structure and the response (negative response) of the damage alone. If the second part of the response is isolated, it forms what can be regarded as the damage signature. The damage signature gives a clear indication of the damage. In this thesis, the existence of the damage signature is investigated when the damaged structure is excited at one of its natural frequencies and therefore it is called "partial mode contribution". The second damage detection method is based on this new physical parameter as determined using the partial mode contribution. The physical reasoning is verified analytically, thereupon it is verified using finite element models and experiments. The limits of damage size that can be determined using the method are also investigated. There is no requirement of having a baseline data with this damage detection method. Since the partial mode contribution is a local parameter, it is thus very sensitive to the presence of damage. The parameter is also shown to be not affected by noise in the detection ambience.
机译:本文是关于使用基于结构动力学的方法来解决结构健康监测(SHM)领域中的现有挑战。特别是,提出了基于结构动力学的新方法,以对损伤区域进行建模,进行损伤诊断并估算和预测结构振动特性(如固有频率)对损伤存在的敏感性。给出了控制模式形状和固有频率的n阶表达式,并给出了损坏的弹性结构(例如任何形状的杆,梁,板和壳)的n阶表达式。该程序的功能包括以下内容:1。与其将损坏建模为虚拟的弹性元件或本构特性的局部或全局变化,不如将其以数学上严格的方式建模为几何不连续性; 2。与损伤的刚度效应(应变能)不同,惯性效应(动能)已被研究人员所忽略; 3。该框架是通用的,适用于构成自伴系统的具有任意边界条件的各种形状各异的工程结构,也适用于各种损坏情况甚至损坏的多个区域。有效地对损伤进行建模,使用Euler-Bernoulli和Timoshenko理论将其应用于梁,并使用Kirchhoff的理论将其应用于板,并在不同类型的边界条件下进行支持。将分析结果与使用压电致动器和非接触式激光多普勒振动计传感器的实验进行了比较。为了说明该程序有效建模损伤的能力,使用欧拉-伯努利和蒂莫申科理论将其应用于梁,并使用基尔霍夫定律将其应用于板理论,支持不同类型的边界条件。将分析结果与使用压电致动器和非接触式激光多普勒振动计传感器的实验进行比较。假设损坏的结构为线性系统,则响应表示为相应未损坏结构的响应与响应(负)之和。响应)。如果响应的第二部分是孤立的,则它将形成可视为损坏特征的部分。损坏签名清楚地表明了损坏。在本文中,研究了当损伤结构以其固有频率之一激发时损伤特征的存在,因此将其称为“部分模式贡献”。第二种损坏检测方法基于使用部分模式贡献确定的新物理参数。通过分析验证了物理推理,随后使用有限元模型和实验对其进行了验证。还研究了可以使用该方法确定的损坏大小的限制。这种损伤检测方法不需要基线数据。由于部分模式贡献是局部参数,因此它对损坏的存在非常敏感。还显示该参数不受检测环境中的噪声影响。

著录项

  • 作者

    Dixit, Akash.;

  • 作者单位

    Georgia Institute of Technology.;

  • 授予单位 Georgia Institute of Technology.;
  • 学科 Engineering Aerospace.;Engineering Civil.;Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2012
  • 页码 134 p.
  • 总页数 134
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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