Volume 34 Issue 4
Jul 2020
Turn off MathJax
Article Contents
JIA Lin, LI Congfu, ZOU Xuetao, YAO Xiaohu. Deformation and Destruction of TC4 Titanium Alloy Plate under the Bird Impact[J]. Chinese Journal of High Pressure Physics, 2020, 34(4): 044102. doi: 10.11858/gywlxb.20200515
Citation: JIA Lin, LI Congfu, ZOU Xuetao, YAO Xiaohu. Deformation and Destruction of TC4 Titanium Alloy Plate under the Bird Impact[J]. Chinese Journal of High Pressure Physics, 2020, 34(4): 044102. doi: 10.11858/gywlxb.20200515

Deformation and Destruction of TC4 Titanium Alloy Plate under the Bird Impact

doi: 10.11858/gywlxb.20200515
  • Received Date: 24 Feb 2020
  • Rev Recd Date: 17 Mar 2020
  • In order to analyze the dynamic behavior of aerospace TC4 titanium alloy plane under the bird impact, the deformation field of TC4 titanium alloy plate subjected to the bird impact was studied by 3D-DIC dynamic deformation field test technology. Meanwhile, a numerical simulation model was established based on explicit finite element analysis software ABAQUS. In this model the Johnson-Cook dynamic constitutive relations was used to describe the property of TC4 titanium alloy, and the bird model was established with smooth particle method (SPH). Comparing the numerical and experimental results, it is concluded that the calculated strain can match the experimental results well. The rationality and reliability of numerical analysis of the bird impact on the TC4 titanium alloy model are verified.

     

  • loading
  • [1]
    黄旭, 朱知寿, 王红红. 先进航空钛合金材料与应用 [M]. 北京: 国防工业出版社, 2012.

    HUANG X, ZHU Z S, WANG H H. Advanced aeronautical titanium alloys and applications [M]. Beijing: National Defense Industry Press, 2012.
    [2]
    GUIDA M, MARULO F, MEO M, et al. SPH-Lagrangian study of bird impact on leading edge wing [J]. Composite Structures, 2011, 93(3): 1060–1071. doi: 10.1016/j.compstruct.2010.10.001
    [3]
    DE VUYST T, VIGNJEVIC R, CAMPBELL J C. Coupling between meshless and finite element methods [J]. International Journal of Impact Engineering, 2005, 31(8): 1054–1064. doi: 10.1016/j.ijimpeng.2004.04.017
    [4]
    张鼎逆, 上官倩芡, 刘富. 基于SPH方法的LY12-CZ铝合金平板鸟撞模型 [J]. 江苏大学学报: 自然科学版, 2016, 37(4): 418–422. doi: 10.3969/j.issn.1671-7775.2016.04.008

    ZHANG D N, SHANGGUAN Q Q, LIU F. Model of bird impact on LY12-CZ aluminum alloy plate based on SPH [J]. Journal of Jiangsu University (Natural Science Edition), 2016, 37(4): 418–422. doi: 10.3969/j.issn.1671-7775.2016.04.008
    [5]
    刘军, 李玉龙, 刘元镛. 基于SPH方法的叶片鸟撞数值模拟研究 [J]. 振动与冲击, 2008, 27(9): 90–93. doi: 10.3969/j.issn.1000-3835.2008.09.022

    LIU J, LI Y L, LIU Y Y. Numerical simulation study of bird-impact on a blade using SPH method [J]. Journal of Vibration and Shock, 2008, 27(9): 90–93. doi: 10.3969/j.issn.1000-3835.2008.09.022
    [6]
    刘富, 张嘉振, 童明波, 等. 2024-T3铝合金动力学实验及其平板鸟撞动态响应分析 [J]. 振动与冲击, 2014, 33(4): 113–118. doi: 10.3969/j.issn.1000-3835.2014.04.021

    LIU F, ZHANG J Z, TONG M B, et al. Dynamic tests and bird impact dynamic response analysis for a 2024-T3 aluminum alloy plate [J]. Journal of Vibration and Shock, 2014, 33(4): 113–118. doi: 10.3969/j.issn.1000-3835.2014.04.021
    [7]
    LIU J, LI Y L, GAO X S. Bird strike on a flat plate: experiments and numerical simulations [J]. International Journal of Impact Engineering, 2014, 70: 21–37. doi: 10.1016/j.ijimpeng.2014.03.006
    [8]
    姚小虎, 韩强, 赵隆茂, 等. 飞机圆弧风挡的抗鸟撞击问题研究 [J]. 华南理工大学学报(自然科学版), 2007, 35(2): 6–12. doi: 10.3321/j.issn:1000-565X.2007.02.002

    YAO X H, HAN Q, ZHAO L M, et al. Investigation into arc windshield of aircraft subjected to bird impact [J]. Journal of South China University of Technology (Natural Science Edition), 2007, 35(2): 6–12. doi: 10.3321/j.issn:1000-565X.2007.02.002
    [9]
    邹学韬, 张晓晴, 姚小虎. 压剪载荷作用下TB6钛合金的动态力学性能 [J]. 高压物理学报, 2019, 33(2): 024206. doi: 10.11858/gywlxb.20190713

    ZOU X T, ZHANG X Q, YAO X H. Dynamic behavior of TB6 titanium alloy under shear-compression loading [J]. Chinese Journal of High Pressure Physics, 2019, 33(2): 024206. doi: 10.11858/gywlxb.20190713
    [10]
    惠旭龙, 牟让科, 白春玉, 等. TC4钛合金动态力学性能及本构模型研究 [J]. 振动与冲击, 2016, 35(22): 161–168. doi: 10.13465/j.cnki.jvs.2016.22.024

    HUI X L, MU R K, BAI C Y, et al. Dynamic mechanical property and constitutive model for TC4 titanium alloy [J]. Journal of Vibration and Shock, 2016, 35(22): 161–168. doi: 10.13465/j.cnki.jvs.2016.22.024
    [11]
    KAY G. Failure modeling of titanium 6Al-4V and aluminum 2024-T3 with the Johnson-Cook material model: DOT/FAA/AR-03/57 [R]. Washington: U.S. Department of Transportation, Federal Aviation Administration, 2003: 1–11.
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Figures(13)  / Tables(3)

    Article Metrics

    Article views(8440) PDF downloads(46) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return