Transverse crack growth behavior considering free-edge effect in quasi-isotropic CFRP laminates under high-cycle fatigue loading

    研究成果: Conference contribution

    1 引用 (Scopus)

    抄録

    The high-cycle fatigue characteristics focused on the behavior of the transverse crack growth up to 108 cycles were investigated using quasi-isotropic carbon fiber reinforced plastic (CFRP) laminates whose stacking sequence was [45/0/45/90]s. To assess the fatigue behavior in the high-cycle region, fatigue tests were conducted at a frequency of 100 Hz in addition to 5 Hz. In this study, to evaluate quantitative characteristics of the transverse crack growth in the high-cycle region, the energy release rate considering the free-edge effect was calculated. Transverse crack growth behavior was evaluated based on a modified Paris law approach. The results revealed that transverse crack growth was delayed under the test conditions of the applied stress level of rmax/rb = 0.2.

    元の言語English
    ホスト出版物のタイトルSpecial Issue on the 12th European Conference on Composite Materials, ECCM 2006
    ページ1388-1393
    ページ数6
    69
    エディション9
    DOI
    出版物ステータスPublished - 2008
    イベント12th European Conference on Composite Materials, ECCM 2006 - Biarritz
    継続期間: 2006 8 282006 9 1

    Other

    Other12th European Conference on Composite Materials, ECCM 2006
    Biarritz
    期間06/8/2806/9/1

    Fingerprint

    Plastic laminates
    Carbon fiber reinforced plastics
    Crack propagation
    Fatigue of materials
    Energy release rate
    carbon fiber reinforced plastic

    Keywords

      ASJC Scopus subject areas

      • Ceramics and Composites

      これを引用

      Hosoi, A., Arao, Y., & Kawada, H. (2008). Transverse crack growth behavior considering free-edge effect in quasi-isotropic CFRP laminates under high-cycle fatigue loading. : Special Issue on the 12th European Conference on Composite Materials, ECCM 2006 (9 版, 巻 69, pp. 1388-1393) https://doi.org/10.1016/j.compscitech.2008.09.003

      Transverse crack growth behavior considering free-edge effect in quasi-isotropic CFRP laminates under high-cycle fatigue loading. / Hosoi, Atsushi; Arao, Yoshihiko; Kawada, Hiroyuki.

      Special Issue on the 12th European Conference on Composite Materials, ECCM 2006. 巻 69 9. 編 2008. p. 1388-1393.

      研究成果: Conference contribution

      Hosoi, A, Arao, Y & Kawada, H 2008, Transverse crack growth behavior considering free-edge effect in quasi-isotropic CFRP laminates under high-cycle fatigue loading. : Special Issue on the 12th European Conference on Composite Materials, ECCM 2006. 9 Edn, 巻. 69, pp. 1388-1393, 12th European Conference on Composite Materials, ECCM 2006, Biarritz, 06/8/28. https://doi.org/10.1016/j.compscitech.2008.09.003
      Hosoi A, Arao Y, Kawada H. Transverse crack growth behavior considering free-edge effect in quasi-isotropic CFRP laminates under high-cycle fatigue loading. : Special Issue on the 12th European Conference on Composite Materials, ECCM 2006. 9 版 巻 69. 2008. p. 1388-1393 https://doi.org/10.1016/j.compscitech.2008.09.003
      Hosoi, Atsushi ; Arao, Yoshihiko ; Kawada, Hiroyuki. / Transverse crack growth behavior considering free-edge effect in quasi-isotropic CFRP laminates under high-cycle fatigue loading. Special Issue on the 12th European Conference on Composite Materials, ECCM 2006. 巻 69 9. 版 2008. pp. 1388-1393
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      title = "Transverse crack growth behavior considering free-edge effect in quasi-isotropic CFRP laminates under high-cycle fatigue loading",
      abstract = "The high-cycle fatigue characteristics focused on the behavior of the transverse crack growth up to 108 cycles were investigated using quasi-isotropic carbon fiber reinforced plastic (CFRP) laminates whose stacking sequence was [45/0/45/90]s. To assess the fatigue behavior in the high-cycle region, fatigue tests were conducted at a frequency of 100 Hz in addition to 5 Hz. In this study, to evaluate quantitative characteristics of the transverse crack growth in the high-cycle region, the energy release rate considering the free-edge effect was calculated. Transverse crack growth behavior was evaluated based on a modified Paris law approach. The results revealed that transverse crack growth was delayed under the test conditions of the applied stress level of rmax/rb = 0.2.",
      keywords = "Durability, Fatigue, Stress concentration, Transverse cracking",
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      T1 - Transverse crack growth behavior considering free-edge effect in quasi-isotropic CFRP laminates under high-cycle fatigue loading

      AU - Hosoi, Atsushi

      AU - Arao, Yoshihiko

      AU - Kawada, Hiroyuki

      PY - 2008

      Y1 - 2008

      N2 - The high-cycle fatigue characteristics focused on the behavior of the transverse crack growth up to 108 cycles were investigated using quasi-isotropic carbon fiber reinforced plastic (CFRP) laminates whose stacking sequence was [45/0/45/90]s. To assess the fatigue behavior in the high-cycle region, fatigue tests were conducted at a frequency of 100 Hz in addition to 5 Hz. In this study, to evaluate quantitative characteristics of the transverse crack growth in the high-cycle region, the energy release rate considering the free-edge effect was calculated. Transverse crack growth behavior was evaluated based on a modified Paris law approach. The results revealed that transverse crack growth was delayed under the test conditions of the applied stress level of rmax/rb = 0.2.

      AB - The high-cycle fatigue characteristics focused on the behavior of the transverse crack growth up to 108 cycles were investigated using quasi-isotropic carbon fiber reinforced plastic (CFRP) laminates whose stacking sequence was [45/0/45/90]s. To assess the fatigue behavior in the high-cycle region, fatigue tests were conducted at a frequency of 100 Hz in addition to 5 Hz. In this study, to evaluate quantitative characteristics of the transverse crack growth in the high-cycle region, the energy release rate considering the free-edge effect was calculated. Transverse crack growth behavior was evaluated based on a modified Paris law approach. The results revealed that transverse crack growth was delayed under the test conditions of the applied stress level of rmax/rb = 0.2.

      KW - Durability

      KW - Fatigue

      KW - Stress concentration

      KW - Transverse cracking

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