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Nonlinear vibration analysis of fiber reinforced composite cylindrical shells with partial constrained layer damping treatment

机译:纤维增强复合圆柱壳的非线性振动分析,具有部分约束层阻尼处理

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摘要

This research proposes a novel analytical model capable of accurately predicting the strain-dependent characteristics of fiber reinforced composite shells (FRCSs) with partial constrained layer damping (CLD) treatment by considering the nonlinearities of fiber reinforced composite and viscoelastic materials simultaneously. The nonlinear material properties are represented based on Jones-Nelson nonlinear theory, energy-based strain energy method, and complex modulus method. Then, the governing equations of motion for FRCSs are developed via Ritz method, and the identification procedure of nonlinear fitting parameters is also presented. By taking a T300 carbon fiber/epoxy resin cylindrical shell with partial CLD patches as an example, a series of experiments are carried out to validate the proposed modeling approach. Finally, the effects of material properties on nonlinear vibration behaviors of FRCSs covered with partial CLD patches are evaluated. Comparisons show that the proposed nonlinear model is more accuracy than that without considering strain dependence, where the maximum errors between the proposed model and measured data for natural frequencies, damping ratios and resonant response are 6.9%, 11.3%, and 11.2%, respectively.
机译:该研究提出了一种新的分析模型,其能够准确地预测纤维增强复合壳(FRCS)的应变依赖性特性,通过考虑纤维增强复合材料和粘弹性材料的非线性来处理偏重的层阻尼(CLD)处理。非线性材料特性基于琼斯 - 尼尔森非线性理论,能量基应变能量方法和复杂模量法。然后,通过RITZ方法开发FRCS的动作的控制方程,并且还呈现了非线性拟合参数的识别过程。通过采用具有部分CLD贴剂的T300碳纤维/环氧树脂圆柱形壳体作为示例,进行了一系列实验以验证提出的建模方法。最后,评估了材料特性对覆盖部分CLD贴片覆盖的FRCS的非线性振动行为的影响。比较表明,所提出的非线性模型比在不考虑应变依赖性的情况下更准确,其中所提出的模型与用于固有频率的测量数据,阻尼比和共振反应的最大误差分别为6.9%,11.3%和11.2%。

著录项

  • 来源
    《Thin-Walled Structures》 |2020年第1期|107000.1-107000.12|共12页
  • 作者单位

    Northeastern Univ Sch Mech Engn & Automat Shenyang 110819 Peoples R China|Northeastern Univ Key Lab Vibrat & Control Aeroprop Syst Minist Educ Shenyang 110819 Peoples R China|Chinese Acad Sci Shenyang Inst Automat State Key Lab Robot Shenyang 110016 Peoples R China;

    Northeastern Univ Sch Mech Engn & Automat Shenyang 110819 Peoples R China|Northeastern Univ Key Lab Vibrat & Control Aeroprop Syst Minist Educ Shenyang 110819 Peoples R China;

    Northeastern Univ Sch Mech Engn & Automat Shenyang 110819 Peoples R China|Northeastern Univ Key Lab Vibrat & Control Aeroprop Syst Minist Educ Shenyang 110819 Peoples R China;

    Northeastern Univ Sch Mech Engn & Automat Shenyang 110819 Peoples R China|Northeastern Univ Key Lab Vibrat & Control Aeroprop Syst Minist Educ Shenyang 110819 Peoples R China;

    Northeastern Univ Sch Mech Engn & Automat Shenyang 110819 Peoples R China|Northeastern Univ Key Lab Vibrat & Control Aeroprop Syst Minist Educ Shenyang 110819 Peoples R China;

    Chinese Acad Sci Shenyang Inst Automat State Key Lab Robot Shenyang 110016 Peoples R China;

    Northeastern Univ Key Lab Vibrat & Control Aeroprop Syst Minist Educ Shenyang 110819 Peoples R China|Chinese Acad Sci Shenyang Inst Automat State Key Lab Robot Shenyang 110016 Peoples R China|Tsinghua Univ Dept Mech Engn State Key Lab Tribol Beijing Peoples R China;

  • 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

    Fiber-reinforced composite shell; Constrained layer damping; Nonlinear material modeling; Strain dependence; Nonlinear vibration;

    机译:纤维增强复合壳;约束层阻尼;非线性材料建模;应变依赖性;非线性振动;

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