Effect of hygrothermal condition on compression after impact strength of CFRP laminates

被引:70
|
作者
Aoki, Yuichiro [1 ]
Yamada, Ken
Ishikawa, Takashi [2 ]
机构
[1] Japan Aerosp Explorat Agcy, Adv Composite Technol Ctr, Tokyo 1810015, Japan
[2] Japan Aerosp Explorat Agcy, Aviat Program Grp, Tokyo, Japan
关键词
hygrothermal effect; mechanical properties; strength; impact behavior;
D O I
10.1016/j.compscitech.2007.11.015
中图分类号
TB33 [复合材料];
学科分类号
摘要
This study investigated the combined effects of water absorption and thermal environment on compression after impact (CAI) characteristics of CFRP laminates. Specimens were immersed in 71 degrees C water for over 10,000 h to quantify the ratio of water absorption in the CFRP laminates. Numerical simulation based on Fick's law was conducted to predict moisture diffusion using the measured orthotropic diffusivities. Compression tests after drop-weight impact tests were carried out at various temperatures, i.e. -54 degrees C, 22 degrees C, 82 degrees C, 121 degrees C, 149 degrees C, 177 degrees C. Delamination area and the number of transverse cracks of the wet specimen were smaller than those of dry specimens. Smaller delamination area of the wet specimens provides higher CAI strength than the dry specimens at mid-high temperatures of 22 degrees C, 82 degrees C and 121 degrees C. The CAI strength of the wet CFRP decreased slightly at 149 'C and significantly at 177 degrees C because the glass transition temperature deteriorates seriously due to the water absorption. The failure mode changes at high temperature, i.e. impact induced delamination is not the trigger of the failure but buckling induced crippling causes final failure at 177 degrees C. (c) 2007 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1376 / 1383
页数:8
相关论文
共 50 条
  • [31] Effect of hygrothermal aging on moisture diffusion and tensile behavior of CFRP composite laminates
    Yong DU
    Yue MA
    Wenbo SUN
    Zhenhai WANG
    [J]. Chinese Journal of Aeronautics., 2023, 36 (03) - 392
  • [32] Hygrothermal effects on ballistic behavior of toughened CFRP laminates
    Xu, K.L.
    Liu, L.L.
    Zhi, J.
    Chen, W.
    Tay, T.E.
    [J]. International Journal of Mechanical Sciences, 2024, 280
  • [33] Impact of thick CFRP laminates: the effect of impact velocity
    Breen, C
    Guild, F
    Pavier, M
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2005, 36 (02) : 205 - 211
  • [34] Compression after impact strength of thin laminates with various percentage of 0° plies
    Nettles, Alan Tate
    Sabo, Stosch
    [J]. JOURNAL OF COMPOSITE MATERIALS, 2014, 48 (03) : 345 - 354
  • [35] Effect of hygrothermal aging on compression behavior of CFRP material with different layups
    Liu, Yuchi
    Wang, Han
    Ding, Huiming
    Wang, Haijin
    Bi, Yunbo
    [J]. COMPOSITES PART B-ENGINEERING, 2024, 270
  • [36] Experimental analysis of CFRP laminates subjected to compression after impact: The role of impact-induced cracks in failure
    Rivallant, Samuel
    Bouvet, Christophe
    Abdallah, Elias Abi
    Broil, Bernhard
    Barrau, Jean-Jacques
    [J]. COMPOSITE STRUCTURES, 2014, 111 : 147 - 157
  • [37] A Numerical Study on Failure Strength of CFRP Laminates with Impact Damage
    Ichiki, Makoto
    Suemasu, Hiroshi
    Aoki, Yuichiro
    [J]. DESIGN, MANUFACTURING AND APPLICATIONS OF COMPOSITES, 2013, : 83 - 90
  • [38] Compression after impact strength of repaired GFRP composite laminates under repeated impact loading
    Andrew, J. Jefferson
    Arumugam, V.
    Saravanakumar, K.
    Dhakal, H. N.
    Santulli, C.
    [J]. COMPOSITE STRUCTURES, 2015, 133 : 911 - 920
  • [39] Effect of resin and fibre properties on impact and compression after impact performance of CFRP
    Cartié, DDR
    Irving, PE
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2002, 33 (04) : 483 - 493
  • [40] RESIDUAL BENDING STRENGTHS OF CFRP LAMINATES AFTER IMPACT
    ADACHI, T
    OKAZAKI, M
    UJIHASHI, S
    MATSUMOTO, H
    [J]. JSME INTERNATIONAL JOURNAL SERIES A-MECHANICS AND MATERIAL ENGINEERING, 1995, 38 (03): : 370 - 377