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An investigation of fatigue crack propagation under mode I and mixed mode I/II loadings.

机译:在I型和I / II型混合载荷下疲劳裂纹扩展的研究。

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摘要

An investigation on fatigue crack propagation under mode I and mixed mode (I and II) loadings has been performed. Fatigue crack growth data in the case of plane strain mode I have been obtained by performing experiments on compact tension specimens of 4340 steel for increasing {dollar}Delta{dollar}K{dollar}sb{lcub}rm I{rcub}{dollar}, decreasing {dollar}Delta{dollar}K{dollar}sb{lcub}rm I{rcub}{dollar} and constant {dollar}Delta{dollar}K{dollar}sb{lcub}rm I{rcub}{dollar} loading conditions.; Under mixed mode plane stress condition, the fatigue crack growth trajectory has been determined by performing experiments on the center cracked thin disk specimen of aluminum 2024. With two mixed mode loading ratios, the subsequent propagation of the main crack has been performed by producing a series of kinks and forks. For practical applications such as the case of a flaw or a crack in aircraft or ship structure in which the loading axis (with respect to the crack) frequently changes, a zig-zag or complicated crack trajectory is very important in both experimental and theoretical studies. In order to apply any specific crack growth criterion for the analysis of the experimental results, a detailed analysis for the stresses near the crack front and the extent of yielding is necessary.; A full field solution, based on small deformation, three-dimensional elastic-plastic finite element analysis of the centrally cracked thin disk under mode I loading has been performed. The solution for the stresses under small-scale yielding and locally fully plastic state has been compared with the HRR plane stress solution. At the outside of the 3D zone, within a distance of {dollar}rsigmasb{lcub}it 0/{rcub}{dollar}/{dollar}J{dollar} = 18, HRR dominance is maintained in the presence of a significant amount of compressive stress along the crack flanks. Ahead of this region, the HRR field overestimate the stresses. These results demonstrate a completely reversed state of stress in the near crack front compared to that in the plane strain case. The combined effect of geometry and finite thickness of the specimen on elastic-plastic crack tip stress field has been explored.; Under mixed mode loading, the dominance of the elastic K-field outside the elastic-plastic region has been demonstrated at the load level at which the crack extension experiment has been performed in the thin disk.; The complex crack trajectory has been analyzed on the basis of the strain energy density criterion for the prediction of propagated crack path under subsequent changes in orientation of the crack to the loading axis or equivalently saying the changes in loading direction with respect to the crack. (Abstract shortened by UMI.)
机译:已经进行了在模式I和混合模式(I和II)载荷下疲劳裂纹扩展的研究。通过在4340钢的致密拉伸试样上进行实验,获得了增加的{dollar} Delta {dollar} K {dollar} sb {lcub} rm I {rcub} {dollar}的实验结果,获得了平面应变模式I下的疲劳裂纹扩展数据。 ,降低{dollar} Delta {dollar} K {dollar} sb {lcub} rm I {rcub} {dollar}和常数{dollar} Delta {dollar} K {dollar} sb {lcub} rm I {rcub} {dollar}加载条件。在混合模式平面应力条件下,通过对2024铝中心裂纹薄盘试样进行实验确定了疲劳裂纹扩展的轨迹。在两种混合模式载荷比下,通过产生一系列裂纹来进行主裂纹的后续扩展扭结和叉子。对于实际应用,例如飞机或船舶结构中的缺陷或裂纹,其中加载轴(相对于裂纹)频繁变化的情况,在实验和理论研究中,之字形或复杂的裂纹轨迹都非常重要。 。为了将任何特定的裂纹扩展标准应用于实验结果分析,需要对裂纹前沿附近的应力和屈服程度进行详细分析。基于小变形,在模式I载荷下对中心裂纹薄盘进行了三维弹塑性有限元分析,从而进行了全场求解。将小规模屈服和局部完全塑性状态下的应力解与HRR平面应力解进行了比较。在3D区域的外部,在{dollar} / {rcub} {dollar} / {dollar} J {dollar} = 18的距离内,在大量存在的情况下,HRR的主导地位得以维持。沿裂纹侧面的压缩应力。在该区域之前,HRR字段高估了应力。这些结果表明,与平面应变情况相比,裂纹近端的应力状态完全相反。研究了试样的几何形状和有限厚度对弹塑性裂纹尖端应力场的综合影响。在混合模式载荷下,已在薄盘上进行裂纹扩展实验的载荷水平下证明了弹塑性区域外弹性K场的优势。已经基于应变能密度标准对复杂的裂纹轨迹进行了分析,以预测在随后裂纹相对于加载轴的方向变化或等效地说出相对于裂纹的加载方向变化的情况下扩展的裂纹路径。 (摘要由UMI缩短。)

著录项

  • 作者

    Paul, Tapan Kumar.;

  • 作者单位

    The University of Oklahoma.;

  • 授予单位 The University of Oklahoma.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1993
  • 页码 174 p.
  • 总页数 174
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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