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Detailed Observation of Change in the Strain near Fatigue Crack Tip

Detailed Observation of Change in the Strain near Fatigue Crack Tip
疲劳裂纹尖端附近应变变化的详细观察
批准号:
08455469
负责人:
YOSHINARI Hitoshi
金额:
$4.74万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (B)
财政年份:
1996
资助国家:
日本
项目状态:
已结题
起止时间:
1996 至 1997

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中文摘要
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英文摘要
In this study, for the purpose of proper understanding of the fatigue crack propagation mechanism, detaild observations of change in strain near the fatigue crack tip were carrind out. And successful measurement of the hysteresis curve of load (P) vs. strain (epsilon') with high accuracy was made.First, from introducing the curve of compliance (depsilon'/dp) and the change rate compliance (d^2epsilon'/dp^2) during one cycle, the following observations have been obtained concernig the fatigue crack opening/closure phenomenon.1) Unloading part of the hysteresis curve is found to be "S" shape, and the point of inflection of the unloading part is considered to be the crak closure point. So if the accuracy of measurement is high enough to be able to obtain a smooth curve of compliance, the crack closure point can be measured automatically as the maximum point of the unloading part of this curve.2) Loading part of the curve of compliance is found to be "S" shape, and the point of inflection … More of the loading part is considered to be RPG (Re-tensile Plastic zone' Generated) point. So if the accuracy of measurement is high enough to be able to obtain a amooth curve of the change rate of compliance, the RPG point can be measured automatically as the minimum point of the loading part of this curve.Secondly, from dividing the loading and unloading processes into several characteristic areas on the basis of the tendency which the compliance and the change rate of compliance show, the following observations have been obtained concerning the fatigue crack propagation parameters.3) In unloading process, it seems to be impossible to isolate the area corresponding to the creation of the re-compressive plastic zone and there is also doubt about using the stress intensity factor because of the influence of the crack closing. So it seems to be rational to adopt the area in loading process, corresponding to the creation of the re-tensile plastic zone, for the fatigue crack propagation parameter.4) According to the experimental results, it is found to be clear that the re-tensile plastic zone's generated point disagrees with the crack opening point.5) From the facts described above 3) & 4), it may be concluded that DELTAK_<RP>, , not DELTAK_<OP> nor DELTAK_<C1>, is considered the most suitable parameter which controls the fatigue crack propagation. Less
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町田 進: "過大過重下におけるき裂進展(1)" 日本造船協会第219研究部会 平成6年度報告書. 44-57 (1995)
Susumu Machida:“过负荷下的裂纹扩展(1)”日本造船研究所第 219 次研究小组委员会 1994 年报告 44-57(1995 年)。
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19
    A Study on mechanisms of cleavage crack propagation of polycrystal metallic materials in crystal grain size level
    • 批准号:
      13450407
    • 项目类别:
      Grant-in-Aid for Scientific Research (B)
    • 资助金额:
      $7.1万
    • 财政年份:
      2001
    • 负责人:
      YOSHINARI Hitoshi
    • 依托单位:
    A Study on Applicability of Microscopic Approach to clear the Fracture Behavior of Materials
    • 批准号:
      10450383
    • 项目类别:
      Grant-in-Aid for Scientific Research (B).
    • 资助金额:
      $8.77万
    • 财政年份:
      1998
    • 负责人:
      YOSHINARI Hitoshi
    • 依托单位:
    海外基金