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Flexible multibody analysis of thin structures with actuated components.

机译:带有致动部件的薄结构的灵活多体分析。

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摘要

A multibody system consisting of rigid bodies, flexible bodies and various joints is called a flexible multibody system. When constructing a numerical model of a flexible multibody system, the simulation tool needs to be able to adequately represent the physical characteristics of the system. In particular, structural flexibility plays a fundamental role in the behavior of many modern mechanical systems. Space structures often comprise thin structures that are in relative motion with respect to one another, resulting in variable geometry systems that are truly multibody in nature. Low cost, accurate simulation tools are essential for the comprehensive analysis of these multibody systems. The overall goal of the present work is to develop a general, finite-element-based nonlinear multibody analysis tools for the simulation of static and dynamic responses of flexible multibody systems containing membrane or shell elements. To achieve this goal, a geometrically exact, nonlinear shallow shell model is developed. It features the following characteristics: anisotropic linear or possibly nonlinear elastic material, large displacements and rotations but small strains, actuation by hygrothermal effects or piezoelectric materials. A pre/post-processor to recover the three dimensional stress fields of a plate using the variational asymptotic method is implemented. A membrane model for flexible multibody analysis is developed. It features the following characteristics: anisotropic linear or possibly nonlinear elastic material, large displacements but small strains, actuation by hygrothermal effects or piezoelectric materials. Robust and rigorous time integrators, the Energy Preserving and Energy Decaying schemes, are developed for the shell and membrane model. Application of the proposed multibody dynamic analysis tool to a realistic inflatable space structure is demonstrated.
机译:由刚体,柔性体和各种关节组成的多体系统称为柔性多体系统。在构建柔性多体系统的数值模型时,仿真工具需要能够充分表示系统的物理特性。特别是,结构柔韧性在许多现代机械系统的行为中起着根本性的作用。空间结构通常包括彼此相对运动的薄结构,从而导致可变几何系统实际上是真正的多体系统。低成本,精确的仿真工具对于全面分析这些多体系统至关重要。本工作的总体目标是开发一种通用的基于有限元的非线性多体分析工具,用于仿真包含膜或壳单元的柔性多体系统的静态和动态响应。为了实现这个目标,开发了几何精确的非线性浅壳模型。它具有以下特征:各向异性的线性或可能为非线性的弹性材料,位移和旋转较大,但应变较小,受潮热效应或压电材料驱动。实现了使用变分渐近方法恢复板的三维应力场的前/后处理器。开发了一种用于柔性多体分析的膜模型。它具有以下特征:各向异性的线性或可能为非线性的弹性材料,大位移但较小的应变,由湿热效应致动或压电材料。针对壳和膜模型开发了功能强大且严格的时间积分器,即“能量保存和能量衰减”方案。演示了所提出的多体动力学分析工具在现实的充气空间结构中的应用。

著录项

  • 作者

    Choi, Jou-Young.;

  • 作者单位

    Georgia Institute of Technology.;

  • 授予单位 Georgia Institute of Technology.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2002
  • 页码 152 p.
  • 总页数 152
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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