强冲击载荷下单向加筋板拉伸撕裂的临界条件

姚熊亮 周晏霈 王治 魏庆媛

姚熊亮, 周晏霈, 王治, 魏庆媛. 强冲击载荷下单向加筋板拉伸撕裂的临界条件[J]. 爆炸与冲击, 2024, 44(2): 023104. doi: 10.11883/bzycj-2023-0182
引用本文: 姚熊亮, 周晏霈, 王治, 魏庆媛. 强冲击载荷下单向加筋板拉伸撕裂的临界条件[J]. 爆炸与冲击, 2024, 44(2): 023104. doi: 10.11883/bzycj-2023-0182
YAO Xiongliang, ZHOU Yanpei, WANG Zhi, WEI Qingyuan. Critical condition for tensile tearing failure of unidirectional stiffened plate under strong impact load[J]. Explosion And Shock Waves, 2024, 44(2): 023104. doi: 10.11883/bzycj-2023-0182
Citation: YAO Xiongliang, ZHOU Yanpei, WANG Zhi, WEI Qingyuan. Critical condition for tensile tearing failure of unidirectional stiffened plate under strong impact load[J]. Explosion And Shock Waves, 2024, 44(2): 023104. doi: 10.11883/bzycj-2023-0182

强冲击载荷下单向加筋板拉伸撕裂的临界条件

doi: 10.11883/bzycj-2023-0182
基金项目: 国家自然科学基金( 52001091),中央高校基本科研业务费专项资金(3072022TS2608),黑龙江省自然科学基金联合引导项目(LH2020E075)
详细信息
    作者简介:

    姚熊亮(1963- ),男,博士,教授,xiongliangyao@hrbeu.edu.cn

    通讯作者:

    王 治(1985- ),男,博士,副教授,wang_z@hrbeu.edu.cn

  • 中图分类号: O383; O347.3

Critical condition for tensile tearing failure of unidirectional stiffened plate under strong impact load

  • 摘要: 针对固支单向加筋板在冲击载荷下的拉伸撕裂临界条件开展研究,首先将均布冲击载荷下的固支单向加筋板简化为带板梁模型,基于固支梁冲击变形理论解给出了加筋板最大永久变形理论解,之后基于复合运动场模型,修正了固支梁端点拉伸应变与最大永久变形关系式,并以等效应变达到失效应变作为拉伸撕裂条件,建立了加筋板在冲击载荷下的拉伸撕裂临界条件。经过数值模拟验证,该最大永久变形理论解和拉伸撕裂临界条件具有适用性,理论与数值误差小于15%。
  • 图  1  带板梁示意图

    Figure  1.  Schematic diagram of beam structure model attached with band plate

    图  2  等效载荷示意图

    Figure  2.  Schematic diagram of equivalent load

    图  3  板的最终运动场示意图

    Figure  3.  Schematic diagram of the final motion mode of the plate

    图  4  简化的单一运动场示意图[20]

    Figure  4.  Schematic diagram of simplified single motion mode[20]

    图  5  小变形阶段塑性铰长度示意[22]

    Figure  5.  Schematic of plastic hinge length in small deformation stage[22]

    图  6  第1阶段变形

    Figure  6.  Deformation diagram of the first stage

    图  7  第2阶段变形

    Figure  7.  Deformation diagram of the second stage

    图  8  第3阶段变形

    Figure  8.  Deformation diagram of the third stage

    图  9  第4阶段变形

    Figure  9.  Deformation diagram of the fourth stage

    图  10  单向加筋板结构示意

    Figure  10.  Schematic of unidirectional stiffened plates

    图  11  单向加筋板结构模型

    Figure  11.  Unidirectional stiffened plate structure model

    图  12  实验舱室与数值模拟模型舱室

    Figure  12.  Experimental cabin and numerical simulation model cabin

    图  13  S1舱壁实验与模拟毁伤效果

    Figure  13.  Experimental and simulation damage of S1 bulkhead

    图  14  单向加筋板在8 MPa矩形冲击载荷下的位移云图

    Figure  14.  Displacement contour of unidirectional stiffened plate under 8 MPa rectangular impact load

    图  15  不同加筋板的变形量计算误差

    Figure  15.  Calculation error of deformation of different stiffened plates

    表  1  T型钢结构参数

    Table  1.   Structural parameters of stiffeners

    加强筋 尺寸/mm
    1 $ \bot \dfrac{{5 \times 80}}{{8 \times 80}}$
    2 $ \bot \dfrac{{5 \times 80}}{{8 \times 100}}$
    3 $ \bot \dfrac{{5 \times 100}}{{8 \times 100}}$
    下载: 导出CSV

    表  2  Q345钢参数

    Table  2.   Parameters of Q345 steel

    $\rho $/(kg·m−3)$E$/GPa$\nu$${\sigma _{\text{0}}}$/MPa${E_{\text{t}}}$/MPa$C$$q$$ {\varepsilon _{\text{f}}} $
    78702120.3134512914050.348
     注:ρ为密度,ν为泊松比。
    下载: 导出CSV

    表  3  实验舱壁结构参数

    Table  3.   Experimental bulkhead structural parameters

    舱壁编号 板厚/mm 加强筋尺寸/mm 加强筋间距/mm 加强筋方向
    S1 8 $ \bot \dfrac{{8 \times 60}}{{8 \times 18}}$ 600 背爆
    S2 600 迎爆
    S3 300 背爆
    S4 300 迎爆
    下载: 导出CSV

    表  4  实验与模拟结果对比

    Table  4.   Comparison of experimental and numerical simulation results

    舱壁最大永久变形量/mm误差/%
    实验模拟
    S139.041.76.92
    S237.039.25.95
    S331.533.46.03
    S427.527.21.09
    下载: 导出CSV

    表  5  单向加筋板变形量对比

    Table  5.   Comparison of deformation of unidirectional stiffened plates

    加强筋 矩形载荷/
    MPa
    最大永久变形/mm 误差/
    %
    加强筋 矩形载荷/
    MPa
    最大永久变形/mm 误差/
    %
    加强筋 矩形载荷/
    MPa
    最大永久变形/mm 误差/
    %
    理论 数值模拟 理论 数值模拟 理论 数值模拟
    1 8 366 326 12.27 2 8 327 320 2.19 3 8 306 307 0.33
    9 413 372 11.02 9 370 364 1.65 9 346 350 1.14
    10 459 416 10.34 10 412 405 1.73 10 387 390 0.77
    11 505 459 10.02 11 453 445 1.80 11 426 432 1.39
    12 550 502 9.56 12 494 485 1.86 12 466 471 1.06
    下载: 导出CSV

    表  6  临界撕裂载荷验证

    Table  6.   Verification of critical tearing failure load

    型材类型 临界载荷/MPa 与模拟结果的误差/%
    文献[20] 本文修正 模拟结果 文献[20] 本文修正
    型材1 26.9 16.8 17.1 57.31 1.75
    型材2 30.0 18.5 17.5 71.42 5.71
    型材3 31.2 20.0 17.8 75.28 12.36
    下载: 导出CSV
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出版历程
  • 收稿日期:  2023-05-17
  • 修回日期:  2023-10-17
  • 网络出版日期:  2023-12-21
  • 刊出日期:  2024-02-06

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