Chinese Journal of Ship Research, Volume. 19, Issue 5, 131(2024)

Analysis of damage behavior of new-type marine composite thick plate with reinforcing ribs and core material in middle

Hao TONG1,2, Yuchao YUAN1,2, and Wenyong TANG1,2
Author Affiliations
  • 1State Key Laboratory of Ocean Engineering, Shanghai Jiao Tong University, Shanghai 200240, China
  • 2School of Ocean and Civil Engineering, Shanghai Jiao Tong University, Shanghai 200240, China
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    Figures & Tables(20)
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    Evolution process of at point A,BA,B点的演化过程
    Evolution process of at point C,DC,D点的演化过程
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    • Table 1. Performance parameters of CFRP laminates

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      Table 1. Performance parameters of CFRP laminates

      参数数值参数数值
      $ {E_{11}}{\text{/MPa}} $165 000$ {X_{\rm{T}}}{\text{/MPa}} $2 714
      $ {E_{22}}{\text{/MPa}} $9 560$ {X_{\rm{C}}}/{\text{MPa}} $1 305
      $ {E_{33}}{\text{/MPa}} $9 560$ {Y_{\rm{T}}}{\text{/MPa}} $37.5
      $ {G_{12}}{\text{/MPa}} $5 400$ {Y_{\rm{C}}}{\text{/MPa}} $188
      $ {G_{23}}{\text{/MPa}} $5 400$ {Z_{\rm{T}}}{\text{/MPa}} $40
      $ {G_{31}}{\text{/MPa}} $4 800$ {Z_{\rm{C}}}{\text{/MPa}} $140
    • Table 2. Performance parameters of adhesive

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      Table 2. Performance parameters of adhesive

      材料参数普通胶高强胶
      $ E{\text{/MPa}} $3.43.4
      $ G{\text{/MPa}} $3.43.4
      $ \sigma /{\text{MPa}} $31.563
      $\tau /{\text{MPa}}$36.573
      ${\text{G}}_{\rm{n}}^{\rm{C}}/({\rm{N}} \cdot{{\rm{mm}}^{ - 1}})$0.95.4
      $ ({\text{G}}_{\rm{s}}^{\rm{C}},{\text{G}}_{\rm{t}}^{\rm{C}})/({\rm{N}}\cdot {\rm{mm}}^{-1}) $1.06.0
    • Table 3. 2D Hashin criterion

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      Table 3. 2D Hashin criterion

      破坏模式失效准则
      纤维拉伸($ \widehat {{\sigma _{11}}} \geqslant 0 $$ F_{\rm{f}}^{\rm{t}} = {\left( {\dfrac{{\widehat {{\sigma _{11}}}}}{{{X_{\rm{T}}}}}} \right)^2} + {\left( {\dfrac{{\widehat {{\tau _{12}}}}}{{{S_{\rm{L}}}}}} \right)^2} $
      纤维压缩($ \widehat {{\sigma _{11}}} < 0 $$ F_{\rm{f}}^{\text{c}} = {\left( {\dfrac{{\widehat {{\sigma _{11}}}}}{{{X_{\rm{C}}}}}} \right)^2} $
      基体拉伸($ \widehat {{\sigma _{22}}} \geqslant 0 $$ F_{\rm{m}}^{\rm{t}} = {\left( {\dfrac{{\widehat {{\sigma _{22}}}}}{{{Y_{\rm{T}}}}}} \right)^2} + {\left( {\dfrac{{\widehat {{\tau _{12}}}}}{{{S_{\rm{L}}}}}} \right)^2} $
      基体压缩($ \widehat {{\sigma _{22}}} < 0 $$ F_{\rm{m}}^{\rm{c}} = {\left( {\dfrac{{\widehat {{\sigma _{22}}}}}{{2{S_{\rm{T}}}}}} \right)^2} + \left[ {\left( {\dfrac{{{Y_{\rm{C}}}}}{{2{S_{\rm{T}}}}}} \right) - 1} \right]\dfrac{{\widehat {{\sigma _{22}}}}}{{{Y_{\rm{C}}}}} + {\left( {\dfrac{{\widehat {{\tau _{12}}}}}{{{S_{\rm{L}}}}}} \right)^2} $
    • Table 4. Comparison of \begin{document}${\sigma _{33}}$\end{document}\begin{document}${\tau _{13}}$\end{document}\begin{document}${\tau _{23}}$\end{document} peak stress of adhesive layer at points A,B,C,D

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      Table 4. Comparison of \begin{document}${\sigma _{33}}$\end{document}\begin{document}${\tau _{13}}$\end{document}\begin{document}${\tau _{23}}$\end{document} peak stress of adhesive layer at points A,B,C,D

      参考点载荷峰值/MPa
      $ {\sigma _{33}} $${\tau _{13}}$${\tau _{23}}$
      A−8.279.8335.06
      B−2.641.0035.00
      C−7.9234.814.08
      D−5.7733.179.14
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    Hao TONG, Yuchao YUAN, Wenyong TANG. Analysis of damage behavior of new-type marine composite thick plate with reinforcing ribs and core material in middle[J]. Chinese Journal of Ship Research, 2024, 19(5): 131

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    Paper Information

    Category: Ship Structure and Fittings

    Received: Jun. 29, 2023

    Accepted: --

    Published Online: Mar. 14, 2025

    The Author Email:

    DOI:10.19693/j.issn.1673-3185.03434

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