The Influence of Carbon Fiber Composite Specimen Design Parameters on Artificial Lightning Strike Current Dissipation and Material Thermal Damage

被引:7
作者
Millen, Scott [1 ]
Kumar, Vipin [2 ]
Murphy, Adrian [1 ]
机构
[1] Queens Univ Belfast, Sch Mech & Aerosp Engn, Belfast, North Ireland
[2] Oak Ridge Natl Lab, Mfg Sci Div, Oak Ridge, TN USA
来源
SAE INTERNATIONAL JOURNAL OF AEROSPACE | 2023年 / 16卷 / 02期
关键词
Lightning strike; Carbon fiber; Finite element analysis (FEA); Computational modelling; Aerospace materials; Composite damage; Current dissipation; FIBER/EPOXY COMPOSITES; MECHANICAL DAMAGE; PROTECTION; SIMULATION; PREDICTION; THICKNESS; IMPACT; FOILS;
D O I
10.4271/01-16-02-0017
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Previous artificial lightning strike direct effect research has examined a broad range of specimen design parameters. No works have studied how such specimen design parameters and electrical boundary conditions impact the dissipation of electric current flow through individual plies. This article assesses the influence of carbon fiber composite specimen design parameters (design parameters = specimen size, shape, and stacking sequence) and electrical boundary conditions on the dissipation of current and the spread of damage resulting from Joule heating. Thermal-electric finite element (FE) modelling is used and laboratory scale (<1 m long) and aircraft scale (>1 m long) models are generated in which laminated ply current dissipation is predicted, considering a fixed artificial lightning current waveform. The simulation results establish a positive correlation between the current exiting the specimen from a given ply and the amount of thermal damage in that ply. The results also establish that the distance to ground, from the strike location to the zero potential boundary conditions (ground), is the controlling factor which dictates the electric current dissipation in each ply. Significantly, this distance to ground is dependent on each of the specimen shape, dimensions, stacking sequence, and location of ground boundary conditions. Therefore, it is not possible to decouple current dissipation and damage from specimen design and boundary condition setup. However, it is possible to define a specimen size for a given specimen shape, stacking sequence, and waveform which limit the influence of specimen dimensions on the resulting current distribution and damage. For a rectangular specimen design which appears in literature multiple times, as 100 x 150 mm and with a stacking sequence of [45/0/-45/90](4s), a specimen design of greater than 300 x 200 mm is required to limit the influence of specimen dimensions on current distribution and damage.
引用
收藏
页码:231 / 246
页数:16
相关论文
共 53 条
  • [1] ABAQUS, 2017, ABAQUS THEORY MANUAL
  • [2] Nonlinear numerical modelling of lightning strike effect on composite panels with temperature dependent material properties
    Abdelal, G.
    Murphy, A.
    [J]. COMPOSITE STRUCTURES, 2014, 109 : 268 - 278
  • [3] A Multiphysics Simulation Approach for Efficient Modeling of Lightning Strike Tests on Aircraft Structures
    Abdelal, Gasser F.
    Murphy, Adrian
    [J]. IEEE TRANSACTIONS ON PLASMA SCIENCE, 2017, 45 (04) : 725 - 735
  • [4] Lightning arc channel effects on surface damage development on a PRSEUS composite panel: An experimental study
    Boushab, Dounia
    Gharghabi, Pedram
    Lee, Juhyeong
    Lacy, Thomas E.
    Pittman, Charles U.
    Mazzola, Michael S.
    Velicki, Alexander
    [J]. COMPOSITES PART B-ENGINEERING, 2021, 224
  • [5] The coupling mechanism and damage prediction of carbon fiber/epoxy composites exposed to lightning current
    Chen, H.
    Wang, F. S.
    Ma, X. T.
    Yue, Z. F.
    [J]. COMPOSITE STRUCTURES, 2018, 203 : 436 - 445
  • [6] Damage analysis of carbon fiber composites exposed to combined lightning current components D and C
    Dong, Qi
    Wan, Guoshun
    Guo, Yunli
    Zhang, Leian
    Wei, Xiuting
    Yi, Xiaosu
    Jia, Yuxi
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2019, 179 : 1 - 9
  • [7] Coupled thermal-mechanical damage model of laminated carbon fiber/resin composite subjected to lightning strike
    Dong, Qi
    Wan, Guoshun
    Ping, Lu
    Guo, Yunli
    Yi, Xiaosu
    Jia, Yuxi
    [J]. COMPOSITE STRUCTURES, 2018, 206 : 185 - 193
  • [8] Damage of Carbon/Epoxy Composite Plates Subjected to Mechanical Impact and Simulated Lightning
    Feraboli, Paolo
    Kawakami, Hirohide
    [J]. JOURNAL OF AIRCRAFT, 2010, 47 (03): : 999 - 1012
  • [9] Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lightning strike
    Feraboli, Paolo
    Miller, Mark
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2009, 40 (6-7) : 954 - 967
  • [10] Quantifying the Influence of Lightning Strike Pressure Loading on Composite Specimen Damage
    Foster, P.
    Abdelal, G.
    Murphy, A.
    [J]. APPLIED COMPOSITE MATERIALS, 2019, 26 (01) : 115 - 137