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VISCOPLASTIC AND CREEP CRACK GROWTH ANALYSIS BY THE FINITE-ELEMENT METHOD.

机译:粘塑性和蠕变裂纹扩展的有限元分析。

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摘要

Creep crack growth in a nickel base alloy at elevated temperatures was analyzed through a hybrid experimental-numerical (HEN) procedure. This HEN procedure consisted of simultaneous use of creep crack growth test displacement data from center cracked plate specimens of IN-100 at 1350(DEGREES)F and a theoretical finite element model of the test specimen.A method for getting creep crack growth behavior solely from high resolution displacement measurements, in conjunction with a cracked specimen model which utilizes realistic constitutive relationships, has been developed. The constitutive law, in the form of the Bodner-Partom material model, was especially tailored to the nickel-base alloy studied which displays time dependent nonlinear inelastic behavior at elevated temperatures. It has been demonstrated that the technique can be applied where crack extension is very small and could not otherwise be resolved by conventional experimental crack measuring techniques. This method provides realistic monotonically increasing crack growth values. The predictions agreed to within 10% of post-test measurements.Crack growth rate and crack growth criteria were studied. Cracktip strain and crack opening displacement were studied in the HEN results for a unique parameter controlling crack growth. Because the parameters were not independent of time due to apparent environmental degradation, it became necessary to establish an empirical criterion for crack growth based on the best fit of HEN results. A damage accumulation criterion based on creep rupture formulations was also developed and applied with promising results.Several crack growth rate criteria were investigated, one of which is the stress intensity factor. The K criterion matched fairly well with an extrapolation of published results. But two other criteria, based on the C* integral and load point displacement rate which are closely related theoretically, were found to be ineffective as crack growth rate criteria.A two-dimensional (constant strain triangular) finite element program was developed which accounts for both nonlinear viscoplastic material behavior and changing boundary conditions due to crack growth. Three viscoplastic material models--(1) Malvern Flow Law, (2) Norton's Creep Law, and (3) Bodner-Partom Flow Law--were incorporated into the program. These time dependent material models were numerically integrated through time by a linear Euler extrapolation technique. A variable time step algorithm was included that maximized time step during the analysis while maintaining good accuracy. This program was used as the plane stress theoretical model for the HEN procedure to analyze sustained load creep crack growth.
机译:通过混合实验数字(HEN)程序分析了镍基合金在高温下的蠕变裂纹扩展。该HEN程序包括同时使用IN-100中心裂纹板样品在1350(DEGREES)F处的蠕变裂纹扩展测试位移数据和测试样品的理论有限元模型。已经开发了高分辨率位移测量,并结合了利用实际本构关系的破裂样本模型。本构律以Bodner-Partom材料模型的形式特别针对研究的镍基合金量身定制,该镍基合金在高温下表现出随时间变化的非线性非弹性行为。已经证明该技术可以应用在裂纹扩展非常小并且不能通过常规实验裂纹测量技术解决的情况下。该方法提供了逼真的单调增加的裂纹扩展值。预测值在测试后测量值的10%之内是一致的。研究了裂纹扩展速率和裂纹扩展标准。在HEN结果中研究了裂纹尖端应变和裂纹开口位移,以控制裂纹扩展的唯一参数。由于参数由于明显的环境退化而与时间无关,因此有必要根据HEN结果的最佳拟合来建立裂纹扩展的经验标准。还建立了基于蠕变断裂公式的损伤累积判据,并应用到了有希望的结果。研究了几种裂纹扩展速率判据,其中之一是应力强度因子。 K准则与已发布结果的推断相当吻合。但基于理论上密切相关的C *积分和载荷点位移率,另两个判据作为裂纹扩展率判据无效。开发了二维(恒应变三角形)有限元程序非线性粘塑性材料行为和由于裂纹扩展而改变的边界条件。三种粘塑性材料模型-(1)马尔文流动定律,(2)诺顿蠕变定律和(3)Bodner-Partom流动定律-已合并到程序中。这些时间相关的材料模型通过线性Euler外推技术随时间进行数值积分。包括可变时间步长算法,该算法在分析过程中最大化了时间步长,同时保持了良好的准确性。该程序用作HEN程序的平面应力理论模型,用于分析持续载荷蠕变裂纹扩展。

著录项

  • 作者

    HINNERICHS, TERRY DEAN.;

  • 作者单位

    Air Force Institute of Technology.;

  • 授予单位 Air Force Institute of Technology.;
  • 学科 Applied Mechanics.
  • 学位 Ph.D.
  • 年度 1980
  • 页码 198 p.
  • 总页数 198
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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