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Free Vibration Analysis of a Rotating Thin Pretwisted and Delaminated Composite Strip

机译:旋转薄预缠绕和分层复合带材的自由振动分析

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摘要

Free vibration analysis of rotating composite strip with delamination is presented. The analysis is based on the framework developed using variational asymptotic method, which is used to reduce the three-dimensional (3D) composite strip with delamination problem into a two-dimensional (2D) cross-sectional analysis and a one-dimensional (1D) problem. This approach, in combination with the sublaminate method, delivers homogenized nonlinear cross-sectional stiffness of the delaminated strip with explicit delamination representation. For the purpose of free vibration study, only the linear cross-sectional stiffness obtained from zeroth-order analysis is used in the 1D problem. The 1D problem is set up by using the Hamilton's principle to derive the dynamic equilibrium equations of motion of a rotating composite strip used in the determination of its natural frequencies. The approach presented is applied to composite strips of different layup configurations and delamination size to investigate their effect on the modal behavior of the strips. The efficacy of the results obtained from the model is validated in comparison with experimental data, other theories, and 3D finite element analysis. Apart from being computationally efficient, due to the closed-form analytical determination of the strip cross-sectional stiffness constants, the approach is capable of providing insight into the strip modal behavior by directly relating structural response with appropriate cross-sectional stiffness constants.
机译:给出了旋转复合材料带分层的自由振动分析。该分析基于使用变分渐近方法开发的框架,该框架用于将具有分层问题的三维(​​3D)复合带材简化为二维(2D)横截面分析和一维(1D)问题。这种方法与分层方法相结合,以明确的分层表示形式提供了分层条带的均化非线性横截面刚度。出于自由振动研究的目的,在一维问题中仅使用了从零阶分析获得的线性横截面刚度。一维问题是通过使用汉密尔顿原理来推导的,用于确定其固有频率的旋转复合材料条带的运动动态平衡方程。提出的方法应用于具有不同铺层构型和分层尺寸的复合带材,以研究其对带材模态行为的影响。与实验数据,其他理论和3D有限元分析相比,从该模型获得的结果的有效性得到了验证。除了计算效率高之外,由于对带钢横截面刚度常数进行了封闭形式的分析确定,该方法还能够通过将结构响应与适当的横截面刚度常数直接相关来提供对带钢模态行为的洞察力。

著录项

  • 来源
    《AIAA Journal》 |2019年第10期|4141-4154|共14页
  • 作者单位

    Indian Inst Technol Dept Aerosp Engn Mumbai 400076 Maharashtra India;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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