Damage of Carbon/Epoxy Composite Plates Subjected to Mechanical Impact and Simulated Lightning

被引:81
|
作者
Feraboli, Paolo [1 ]
Kawakami, Hirohide [1 ]
机构
[1] Univ Washington, Dept Aeronaut & Astronaut, Automobili Lamborghini Adv Composite Struct Lab, Seattle, WA 98195 USA
来源
JOURNAL OF AIRCRAFT | 2010年 / 47卷 / 03期
关键词
D O I
10.2514/1.46486
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Damage is inflicted on carbon-fiber/epoxy composite plates using both simulated lightning strike and mechanical impact in the effort to understand the relative effect of the two damage mechanisms. A methodology is proposed to characterize the damage resistance and tolerance of unconfigured composite plates subjected to lightning strike in a fashion that is consistent with the extensive work previously done on low-velocity impact. Using current and voltage diagnostics, it is possible to extrapolate the amount of electromechanical energy absorbed by the plate during the strike and compare it to that absorbed during a mechanical impact. Damage resistance is characterized by means of ultrasonic C-scans and microscopy, whereas residual strength is measured by means of compression after impact testing. Results show that the energy dissipated in a specimen during the lightning strike is much greater than the strain energy introduced by mechanical impact, and hence a comparison based on energy is not recommended. However, based on the relative threat levels associated with the impact and the lightning strike events, the comparison yields insightful observations on both damage state and residual performance. In general, for the configurations tested, lightning strike damage seems to be less detrimental than the mechanical impact in terms of both damage area and residual strength.
引用
收藏
页码:999 / 1012
页数:14
相关论文
共 50 条
  • [1] Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lightning strike
    Feraboli, Paolo
    Miller, Mark
    COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2009, 40 (6-7) : 954 - 967
  • [2] Damage analysis for carbon fiber/epoxy composite exposed to simulated lightning current
    Li Shulin
    Yin Junjie
    Yao Xueling
    Chang Fei
    Shi Xiaopeng
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2016, 35 (15) : 1201 - 1213
  • [3] Development of an Experimental Setup to Study Carbon/Epoxy Composite Subjected to Simulated Lightning Current
    Gharghabi, Pedram
    Lee, Juhyeong
    Mazzola, Michael
    Lacy, Thomas
    Kluss, Joni
    2017 IEEE CONFERENCE ON ELECTRICAL INSULATION AND DIELECTRIC PHENOMENON (CEIDP), 2017, : 773 - 775
  • [4] DAMAGE SUSTAINED BY A CARBON EPOXY COMPOSITE-MATERIAL SUBJECTED TO REPEATED IMPACT
    WYRICK, DA
    ADAMS, DF
    COMPOSITES, 1988, 19 (01): : 19 - 27
  • [5] Damage properties of carbon fiber reinforced epoxy composite subjected to multiple continuous lightning current strikes
    Sun J.
    Yao X.
    Li Y.
    Tian X.
    Chen J.
    Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica, 2019, 36 (12): : 2764 - 2771
  • [6] Effect of hygrothermal aging on the damage characteristics of carbon woven fabric/epoxy laminates subjected to simulated lightning strike
    Li, Yichao
    Li, Renfu
    Huang, Lai
    Wang, Kun
    Huang, Xianrong
    MATERIALS & DESIGN, 2016, 99 : 477 - 489
  • [7] Resistance characteristics of unidirectional carbon fiber/epoxy prepreg subjected to simulated lightning currents
    Chen J.
    Fu Z.
    Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica, 2020, 37 (01): : 82 - 88
  • [8] Damage prediction in composite plates subjected to low velocity impact
    Tiberkak, R.
    Bachene, M.
    Rechak, S.
    Necib, B.
    COMPOSITE STRUCTURES, 2008, 83 (01) : 73 - 82
  • [9] Damage generated in carbon/epoxy composite plates with holes under different levels of impact energy
    Luo, RK
    Wu, WX
    Gahagan, PGP
    Mortel, WJ
    DAMAGE AND FRACTURE MECHANICS VI: COMPUTER AIDED ASSESSMENT AND CONTROL, 2000, 6 : 191 - 200
  • [10] Impact response and damage tolerance characteristics of glass-carbon/epoxy hybrid composite plates
    Naik, NK
    Ramasimha, R
    Arya, H
    Prabhu, SV
    ShamaRao, N
    COMPOSITES PART B-ENGINEERING, 2001, 32 (07) : 565 - 574