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ANISOTROPIC CONSTITUTIVE MODEL FOR NICKEL BASE SINGLE CRYSTAL ALLOYS: DEVELOPMENT AND FINITE ELEMENT IMPLEMENTATION.

机译:镍基单晶合金的各向异性本构模型:发展和有限元实现。

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摘要

The purpose of this research is to develop a tool for the mechanical analysis of nickel base single crystal superalloys, specifically Rene N4, used in gas turbine engine components. This objective is achieved by developing a rate dependent anisotropic constitutive model and implementing it in a nonlinear three dimensional finite element code.; The constitutive model is developed from metallurgical concepts utilizing a crystallographic approach. A non Schmid's law formulation is used to model the tension/compression asymmetry and orientation dependence in octahedral slip. Schmid's law is a good approximation to the inelastic response of the material in cube slip. The constitutive equations model the tensile behavior, creep response and strain rate sensitivity of these alloys. Methods for deriving the material constants from standard tests are presented.; The finite element implementation utilizes an initial strain method and twenty noded isoparametric solid elements. The ability to model piecewise linear load histories is included in the finite element code. The constitutive equations are accurately and economically integrated using a second order Adams-Moulton predictor-corrector method with a dynamic time incrementing procedure.; Computed results from the finite element code are compared with experimental data for tensile, creep and cyclic tests at 760(DEGREES)C. The strain rate sensitivity and stress relaxation capabilities of the model are evaluated. Limitations and future development needs are discussed.
机译:这项研究的目的是开发一种用于分析燃气涡轮发动机部件中使用的镍基单晶高温合金(特别是Rene N4)的工具。通过开发速率相关的各向异性本构模型并将其以非线性三维有限元代码实现,可以实现该目标。本构模型是利用结晶学方法从冶金学概念发展而来的。非Schmid定律公式用于模拟八面体滑移中的拉伸/压缩不对称性和方向依赖性。施密德定律很好地近似了材料在立方滑移中的无弹性响应。本构方程对这些合金的拉伸行为,蠕变响应和应变速率敏感性进行建模。提出了从标准试验中得出材料常数的方法。有限元实现利用初始应变方法和二十个节点等参实体单元。对分段线性载荷历史进行建模的功能包含在有限元代码中。本构方程是使用具有动态时间增量程序的二阶Adams-Moulton预测器-校正器方法精确且经济地集成的。将有限元代码的计算结果与在760(DEGREES)C下进行拉伸,蠕变和循环测试的实验数据进行比较。评估模型的应变率敏感性和应力松弛能力。讨论了局限性和未来的发展需求。

著录项

  • 作者

    DAME, L. THOMAS.;

  • 作者单位

    University of Cincinnati.;

  • 授予单位 University of Cincinnati.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 1985
  • 页码 136 p.
  • 总页数 136
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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