THE RESPONSE OF FIBROUS COMPOSITES TO IMPACT LOADING

被引:70
|
作者
JANG, BZ
CHEN, LC
HWANG, LR
HAWKES, JE
ZEE, RH
机构
[1] Auburn University, Alabama
关键词
D O I
10.1002/pc.750110303
中图分类号
TB33 [复合材料];
学科分类号
摘要
The response of advanced composites to low‐velocity projectile loading was investigated. The impact failure mechanisms of composites containing various fibers with different strength and ductility were studied by a combination of static indentation testing, instrumented falling dart impact testing, acoustic emission monitoring, and scanning electron microscopy (SEM). The composites containing fibers with both high strength and high ductility (eg., polyethylene (PE) fibers) demonstrate a superior impact resistance as compared to those containing fibers with high strength (eg., graphite fibers) or high ductility (eg., nylon fibers) but not both. Upon impact loading, the composites containing PE fibers usually exhibited a great degree of plastic deformation and some level of delamination. These mechanisms acted to dissipate a significant amount of strain energy prior to the penetration phase of the impact process. No through penetration was observed in all the samples containing more than three layers of PE fabric except when loaded at relatively high rates and low temperatures. Although certain levels of delamination also took place in other composite systems, very little plastic deformation occurred, allowing ready penetration of the projectile. The stacking sequences in the hybrid laminates studied were found to play a critical role in triggering or inhibiting the processes of plastic deformation and delamination and, therefore, controlling their energy absorption capability. The penetration resistance of composites appeared to be dictated by the fiber toughness. The later property must be measured in a simulated high‐rate condition. Copyright © 1990 Society of Plastics Engineers
引用
收藏
页码:144 / 157
页数:14
相关论文
共 50 条
  • [1] Progressive damage modeling and optimization of fibrous composites under ballistic impact loading
    Dhari, Rahul Singh
    Patel, Nirav P.
    Wang, Hongxu
    Hazell, Paul J.
    MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2021, 28 (12) : 1227 - 1244
  • [2] Processing of nanoclay filled sandwich composites and their response to impact loading
    Hosur, M. V.
    Mohammed, A. A.
    Jeelani, S.
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2008, 27 (08) : 797 - 818
  • [3] Response of laminated FRP composites under multiple impact loading
    Chakraborty, D
    Kumar, M
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2005, 24 (14) : 1457 - 1477
  • [4] Modeling of nonlinear response in loading-unloading tests for fibrous composites under tension and compression
    Wang, Jie
    Xiao, Yi
    Inoue, Keisuke
    Kawai, Mashamichi
    Xue, Yuande
    COMPOSITE STRUCTURES, 2019, 207 : 894 - 908
  • [5] GEOMETRY AND LOADING EFFECTS ON THE COMPRESSIVE STRENGTH OF FIBROUS COMPOSITES
    LAGOUDAS, DC
    SALEH, AM
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 1993, 12 (09) : 1016 - 1023
  • [6] Influence of porosity on the response of fibrous composites
    Baxter, SC
    Herakovich, CT
    Roerden, AM
    IUTAM SYMPOSIUM ON THEORETICAL AND NUMERICAL METHODS IN CONTINUUM MECHANICS OF POROUS MATERIALS, 2001, 87 : 131 - 136
  • [7] EFFECT OF LOADING RATE ON TENSILE-STRENGTH OF FIBROUS COMPOSITES
    LHYMN, C
    LHYMN, Y
    PECKENS, R
    YOUNG, J
    COMPOSITES, 1988, 19 (04): : 295 - 299
  • [8] IMPACT-RESISTANT COATINGS FOR FIBROUS COMPOSITES
    WHEELER, WH
    IZU, YD
    CREEDON, JF
    AMERICAN CERAMIC SOCIETY BULLETIN, 1983, 62 (08): : 870 - 870
  • [9] Shock loading and drop weight impact response of glass reinforced polymer composites
    Hebert, Michael
    Rousseau, Carl-Ernst
    Shukla, Arun
    COMPOSITE STRUCTURES, 2008, 84 (03) : 199 - 208
  • [10] FRACTURE CRITERIA OF FIBROUS LAMINATED COMPOSITES UNDER INPLANE MULTIDIRECTIONAL LOADING
    TIROSH, J
    MAST, P
    BEAUBIEN, L
    MULVILLE, D
    SUTTON, S
    WOLOCK, I
    JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1980, 47 (03): : 563 - 569