A computational framework for microstructural crack propagation

被引:4
作者
Brockman, Robert A. [1 ,2 ]
Hoffman, Rebecca M. [1 ,2 ]
Golden, Patrick J. [1 ]
Musinski, William D. [1 ]
Jha, Sushant K. [1 ,2 ]
John, Reji [1 ]
机构
[1] Air Force Res Lab, Mat & Mfg Directorate, AFRL RXCM, Wright Patterson AFB, OH 45433 USA
[2] Univ Dayton, Res Inst, Dayton, OH 45469 USA
关键词
Microstructural crack propagation; Material model; Crystal plasticity; Abaqus; User subroutines; FINITE-ELEMENT-METHOD; CYCLE FATIGUE; SUPERALLOY; INITIATION; MODEL; DEFORMATION; SENSITIVITY; GROWTH;
D O I
10.1016/j.ijfatigue.2021.106397
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper describes a computational framework for solving, in the context of large-scale commercial mechanics codes, complex problems in which specialized models are required for phenomena that are larger in scope than pointwise material models, or for loading and constraints that vary by position. Production analysis codes typically include interfaces for user-supplied submodels, but supply information only at a single point of interest, such as a model node or integration point. The particular example addressed herein is that of crack propagation on the microstructural scale, in which communications are required not only between the submodels and the analysis code, but between individual submodels to allow decision-making about nonlinear material response, crack propagation criteria, material interface behavior, time-dependent load variation, and convergence of nonlinear cyclic forced response. While the specific models discussed are of interest in metal plasticity and fatigue analysis, the methodology described is applicable to numerous other complex problems in computational mechanics where communication between user-written submodels and the analysis code require more than pointwise response information.
引用
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页数:12
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