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断裂过程区视角下的I型弹塑性断裂理论

鲁龙坤

鲁龙坤. 断裂过程区视角下的I型弹塑性断裂理论. 力学进展, 待出版 doi: 10.6052/1000-0992-25-041
引用本文: 鲁龙坤. 断裂过程区视角下的I型弹塑性断裂理论. 力学进展, 待出版 doi: 10.6052/1000-0992-25-041
Lu L K. Mode I elastic-plastic fracture theory from the perspective of fracture process zone. Advances in Mechanics, in press doi: 10.6052/1000-0992-25-041
Citation: Lu L K. Mode I elastic-plastic fracture theory from the perspective of fracture process zone. Advances in Mechanics, in press doi: 10.6052/1000-0992-25-041

断裂过程区视角下的I型弹塑性断裂理论

doi: 10.6052/1000-0992-25-041 cstr: 32046.14.1000-0992-25-041
基金项目: 本文所涉及的系列研究工作, 得到了国家自然科学基金项目 (批准号: 12372083, 12002182)、中央高校基本科研业务费项目 (批准号: G2023KY05104) 以及清华大学“水木学者”计划 (项目号: 2019SM077) 的资助与支持, 特此致谢.
详细信息
    作者简介:

    鲁龙坤, 西北工业大学航空学院副教授, 主要从事飞机金属薄壁结构的断裂理论研究. 2009年—2019年, 在西北工业大学航空学院先后获得学士、硕士和博士学位. 2019年—2022年, 在清华大学航天航空学院从事博士后研究, 并荣获“清华大学水木学者”称号. 2022年至今就职于西北工业大学航空学院. 主持国家自然科学基金青年项目 (C类)、面上项目各一项, 以第一完成人获陕西高等学校科学技术研究优秀成果奖二等奖一项. 其学术成果以第一作者身份在JMPS、IJSS、EFM等力学领域国际重要期刊发表论文10余篇

    通讯作者:

    lulongkun@nwpu.edu.cn

  • 中图分类号: O34, O39

Mode I elastic-plastic fracture theory from the perspective of fracture process zone

More Information
  • 摘要: 以飞机金属薄壁结构失效为典型代表的等温或常温环境下弹塑性裂纹扩展问题, 因涉及大范围屈服与稳态扩展特征, 对线弹性断裂力学及J积分理论的适用性构成了严峻挑战. 尽管学术界相继提出了断裂应变、裂纹尖端张开角/位移、断裂本征功及增量裂纹尖端积分等多种参量, 但因其物理内涵差异显著、内在关联模糊且“可迁移性”存疑, 严重阻碍了统一理论的构建与工程应用. 针对上述困境, 本文作者以断裂过程区 (FPZ) 为核心视角, 在忽略热源效应及体积力的简化假设下, 构建了一套统一的弹塑性断裂理论框架. 该框架不仅对Rice悖论等历史难题提供了统一且自洽的解释, 更系统论证了增量积分、裂纹尖端张开角/位移、断裂应变与断裂本征功等主流参数在本质上均等价于“定常FPZ”的驱动力, 从而揭示了现有弹塑性断裂参数的内在统一性. 在此基础上, 通过阐释含扩展裂纹体功率平衡定律的热力学意义, 该框架证明了FPZ可视为具有“自治性”的独立热力学系统, 为断裂参数的“可迁移性”提供了坚实的理论支撑. 本文系统阐述了该理论框架的构建过程、核心论点及其学术价值.

     

  • 图  1  弹塑性材料与非线性弹性材料

    图  2  断裂参数选取与验证的两阶段框架

    图  3  常规固体的参考构型与当前构型

    图  4  二维I型边裂纹体的参考构型

    图  5  小应变条件下围绕裂纹尖端的两个圆形围线

    图  6  典型的弹塑性扩展裂纹尖端场

    图  7  参考构型中移动的有限大小围线

    图  8  小应变条件下的弹塑性含裂纹体

    图  9  裂纹面固定部分有作用力

    图  10  裂纹面上作用力边界的移动特征

    图  11  二维含“线FPZ”裂纹体的参考构型

    图  12  弹塑性裂纹扩展过程中不同围线的能量耗散率(Brust et al. 1985; Okada et al. 1999)

    图  13  “点FPZ”弹塑性扩展裂纹的示意图

    图  14  “非定常FPZ”上的速度矢量分布

    图  15  一个具体的离散裂纹扩展步: (a) 裂纹扩展前的状态; (b) 裂纹扩展后的状态

    图  16  CTOA的工程定义与裂纹面的三角形等效 (右图为A710高强度低合金钢韧性裂纹扩展的光学显微照片, 引自McMeeking & Parks 1979)

    图  17  考虑“有限尺寸FPZ”的CTOA定义

    图  18  “终端拉伸准则”的定义

    图  19  裂纹尖端前方$ \Delta $处一物质点的状态

    图  20  常见弹塑性断裂参数的等价性

    图  21  “直裂纹面”的裂纹扩展过程

    图  22  DENT试样的几何构型及断裂时的韧带区模型

    图  23  固结于移动裂纹尖端的有限围线

    图  24  独立系统假设

    图  25  任意形状FPZ的边界演化描述

    图  26  FPZ的“自相似膨胀”过程与“等体积扭曲”过程

    图  27  “启裂前”与“启裂后”的FPZ演化过程

    表  1  基于DENT试样的“临界CTOA与EWF关系式”验证

    文献 材料 B/mm $ {w}_{\mathrm{e}} $/(N/mm) $ {\sigma }_{\mathrm{u}} $/MPa $ {l}_{\text{FPZ}} $/mm $ {\psi }_{\mathrm{c}} $ $ \psi _{\mathrm{c}}^{\text{es}} $
    Chandra et al. 2018 IF 1 210.1 324 2 0.316 0.282
    Sarkara et al. 2019 DP780 1 233 840 2 0.132 0.121
    Mohammed 2017 AL-C* 1.55 51.5 93.2 2 0.254 0.24
    Marchal & Delanny 1996 Zn* 0.6 78.2 140 3 0.142 0.161
    Marchal & Delanny 1996 Zn* 1 102.8 140 4 0.160 0.160
    Marchal & Delanny 1996 Zn* 1.3 128.7 140 4 0.213 0.200
    Knockaert et al. 1996 LC* 0.7 206 360 3 0.22 0.169
    Knockaert et al. 1996 LC* 1 247 360 3 0.216 0.203
    Knockaert et al. 1996 LC* 1.5 400.5 360 4 0.222 0.247
    Knockaert et al. 1996 LC* 2 442 360 4 0.237 0.272
    Cotterell & Reddel 1977 LA* 1.6 234 510 3 0.1 0.125
    Chaitanya et al. 2018 PC* 1 28.5 56 2 0.215 0.221
    下载: 导出CSV
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  • 收稿日期:  2025-12-10
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