knowledge of professional and technical personnel Notice on the organization of advanced research class on high-pressure science and new materials of engineering
Volume 33 Issue 4
Jul 2019
Turn off MathJax
Article Contents
Chinese Journal of High Pressure Physics  > 2019  >  33(4): 044202.
LIAO Binbin, ZHOU Jianwu, LIN Yuan, JIA Liyong, WANG Dongliang, HUA Zhengli, ZHENG Jinyang, GU Chaohua. Low-Velocity Impact Behavior and Damage Characteristics of CFRP Laminates[J]. Chinese Journal of High Pressure Physics, 2019, 33(4): 044202. doi: 10.11858/gywlxb.20180699
Citation: LIAO Binbin, ZHOU Jianwu, LIN Yuan, JIA Liyong, WANG Dongliang, HUA Zhengli, ZHENG Jinyang, GU Chaohua. Low-Velocity Impact Behavior and Damage Characteristics of CFRP Laminates[J]. Chinese Journal of High Pressure Physics, 2019, 33(4): 044202. doi: 10.11858/gywlxb.20180699
shu

Low-Velocity Impact Behavior and Damage Characteristics of CFRP Laminates

doi: 10.11858/gywlxb.20180699
  • 1.

    Institute of Process Equipment, Zhejiang University, Hangzhou 310027, China

  • 2.

    School of Mechanical Engineering, Northwestern Polytechnical University, Xi’an 710072, China

  • 3.

    College of Field Engineering, PLA Army Engineering University, Nanjing 210042, China

  • 4.

    First Aircraft Institute of Aviation Industry Corporation, Xi’an 710089, China

  • 5.

    State Key Laboratory of Fluid Power and Mechanical Systems, Hangzhou 310027, China

  • Received Date: 12 Dec 2018
  • Rev Recd Date: 25 Dec 2018
    Abstract
  • Low-velocity impact tests were performed for the [454/–454]4T carbon fiber reinforced plastics (CFRP) laminates for exploring the low-velocity impact behaviors. The effects of impact angle of strip impactor and impactor diameter of hemispherical impactor on the impact responses of laminates are studied. Besides, the damage characteristics are evaluated by dent depth and delamination damage area simultaneously. The experimental results show that larger maximum center displacement and more energy dissipation can be caused when the impact direction of the strip impactor is parallel to the fibers in the surface plies and the impactor diameter is smaller. The dent depth and delamination damage area are also larger at the two situations above. In addition, the dent depth is positive correlated with the delamination damage area under single factor variables of impact angle and impactor diameter. There has significant fiber break around the impact area under the impact of 10 mm hemispherical impactor, but no obvious fiber break appears around the impact area for 14 mm and 16 mm impactors.

     

    • FullText(HTML)
  • loading
    • References(20)
  • [1]
    LIU P F, LIAO B B, JIA L Y, et al. Finite element analysis of dynamic progressive failure of carbon fiber composite laminates under low velocity impact [J]. Composite Structures, 2016, 149: 408–422. doi: 10.1016/j.compstruct.2016.04.012
    [2]
    LIAO B B, LIU P F. Finite element analysis of dynamic progressive failure properties of GLARE hybrid laminates under low-velocity impact [J]. Journal of Composite Materials, 2018, 52(10): 1317–1330. doi: 10.1177/0021998317724216
    [3]
    SCHOEPPNER G A, ABRATE S. Delamination threshold loads for low velocity impact on composite laminates [J]. Composites Part A: Applied Science and Manufacturing, 2000, 31(9): 903–915. doi: 10.1016/S1359-835X(00)00061-0
    [4]
    YANG B, WANG Z, ZHOU L, et al. Experimental and numerical investigation of interply hybrid composites based on woven fabrics and PCBT resin subjected to low-velocity impact [J]. Composite Structures, 2015, 132: 464–476. doi: 10.1016/j.compstruct.2015.05.069
    [5]
    WAN Y, DIAO C, YANG B, et al. GF/epoxy laminates embedded with wire nets: a way to improve the low-velocity impact resistance and energy absorption ability [J]. Composite Structures, 2018, 202: 818–835. doi: 10.1016/j.compstruct.2018.04.041
    [6]
    钭李昕, 王秋成, 陈光耀. 碳纤维复合材料低速冲击特性及损伤分析研究 [J]. 机电工程, 2016, 33(7): 815–821.

    TOU L X, WANG Q C, CHEN G Y. Analysis on low velocity impact performance and damage behavior of carbon fiber composite beam [J]. Journal of Mechanical & Electrical Engineering, 2016, 33(7): 815–821.
    [7]
    竺铝涛, 张发. 碳纤维复合材料层压板低速冲击试验研究 [J]. 航空发动机, 2015, 41(1): 85–88.

    ZHU L T, ZHANG F. Experimental investigation of low-speed impact for carbon fiber composite laminate [J]. Aeroengine, 2015, 41(1): 85–88.
    [8]
    TAN W, FALZON B G, CHIU L N S, et al. Predicting low velocity impact damage and compression-after-impact (CAI) behaviour of composite laminates [J]. Composites Part A: Applied Science and Manufacturing, 2015, 71: 212–226. doi: 10.1016/j.compositesa.2015.01.025
    [9]
    DUBARY N, BOUVET C, RIVALLANT S, et al. Damage tolerance of an impacted composite laminate [J]. Composite Structures, 2018, 206: 261–271. doi: 10.1016/j.compstruct.2018.08.045
    [10]
    姚振华, 李亚智, 刘向东, 等. 复合材料层合板低速冲击后剩余压缩强度研究 [J]. 西北工业大学学报, 2012, 30(4): 518–523. doi: 10.3969/j.issn.1000-2758.2012.04.008

    YAO Z H, LI Y Z, LIU X D, et al. Effectively calculating residual compressive strength of composite laminate after impact(CAI) [J]. Journal of Northwestern Polytechnical University, 2012, 30(4): 518–523. doi: 10.3969/j.issn.1000-2758.2012.04.008
    [11]
    MITREVSKI T, MARSHALL I H, THOMSON R, et al. The effect of impactor shape on the impact response of composite laminates [J]. Composite Structures, 2005, 67(2): 139–148. doi: 10.1016/j.compstruct.2004.09.007
    [12]
    AMARO A M, REIS P N B, MAGALHÃES A G, et al. The effect of the impactor diameter and boundary conditions on low velocity impact composites behavior [J]. Applied Mechanics and Materials, 2007, 7/8: 217–222. doi: 10.4028/www.scientific.net/AMM.7-8
    [13]
    ICTEN B M, KIRAL B G, DENIZ M E. Impactor diameter effect on low velocity impact response of woven glass epoxy composite plates [J]. Composites Part B: Engineering, 2013, 50: 325–332. doi: 10.1016/j.compositesb.2013.02.024
    [14]
    ANSARI M M, CHAKRABARTI A. Effect of boundary condition and impactor nose angle on impact behaviour of FRP composite: experimental and FE analyses [J]. Materials Today: Proceedings, 2017, 4(9): 9645–9649. doi: 10.1016/j.matpr.2017.06.241
    [15]
    XIE W B, ZHANG W, KUANG N H, et al. Experimental investigation of normal and oblique impacts on CFRPs by high velocity steel sphere [J]. Composites Part B: Engineering, 2016, 99: 483–493. doi: 10.1016/j.compositesb.2016.06.020
    [16]
    SEBAEY T A, GONZÁLEZ E V, LOPES C S, et al. Damage resistance and damage tolerance of dispersed CFRP laminates: effect of ply clustering [J]. Composite Structures, 2013, 106: 96–103. doi: 10.1016/j.compstruct.2013.05.052
    [17]
    WANG H R, LONG S C, ZHANG X Q, et al. Study on the delamination behavior of thick composite laminates under low-energy impact [J]. Composite Structures, 2018, 184: 461–473. doi: 10.1016/j.compstruct.2017.09.083
    [18]
    SHI Y, SWAIT T, SOUTIS C. Modelling damage evolution in composite laminates subjected to low velocity impact [J]. Composite Structures, 2012, 94(9): 2902–2913. doi: 10.1016/j.compstruct.2012.03.039
    [19]
    XU Z, YANG F, GUAN Z W, et al. An experimental and numerical study on scaling effects in the low velocity impact response of CFRP laminates [J]. Composite Structures, 2016, 154: 69–78. doi: 10.1016/j.compstruct.2016.07.029
    [20]
    ASTM International. Standard test method for measuring the damage resistance of a fiber-reinforced polymer matrix composite to a drop-weight impact event: ASTM D7136/D7136M-15 [S]. West Conshohocken, PA: ASTM International, 2015.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 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(10)  / Tables(2)

    Get Citation
    PDF
    XML

    Article Metrics

    Article views(6520) PDF downloads(26) Cited by()
    Proportional views
    Related

    Copyright©《高压物理学报》编辑部

    Tel:0816-2490042 E-mail:gaoya@caep.cn

    Shu ICP, 11011126 -2

    Supported by: Beijing Renhe Information Technology Co. Ltd support: info@rhhz.net  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return