节点文献

2024T3铝板试件疲劳裂纹张开应力测量

FATIGUE CRACK CLOSURE MEASUREMENTS ON 2024T3SHEET SPECIMENS

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 伍义生

【Author】 Wu Yisheng(Institute of Mechanics,Chinese Academy of Sciences,Beijing,100080)J.Schijve(Delft University of Technology,Faculty of Aerospace Enginecring,The Netherlands)

【机构】 中国科学院力学研究所

【摘要】 建立了一种用裂纹张开位移引伸计对2024T3铝板试件的疲劳裂纹张开应力进行自动测量的方法。比较了斜率法、切线相交法和切点法所得结果的差别及测点位置的影响。并给出了超载作用下的疲劳裂纹张开应力的测量结果。

【Abstract】 A computer controlled procedure is developed for automatic measurements of the crack opening stress Sop during fatigue tests A crack opening displacement gauge(CODmeter)is used to obtain digital data on load COD curves. Three methods for deriving Sop from the da- ta sets are compared:(1) slope method,(2)tangent lines intersection method,and(3)tangent point method. The effect of the position of the COD meter with respect to the crack tip is studied in tests on 2024T3 specimens. Results on crack growth and Sop are presented for CA loading with an overload and with an overload followed bv an underload.

【关键词】 疲劳裂纹闭合超载
【Key words】 fatiguecrack closureoverload
  • 【文献出处】 航空学报 ,ACTA AERONAUTICA ET ASTRONAUTICA SINICA , 编辑部邮箱 ,1994年03期
  • 【分类号】V214.35
  • 【被引频次】3
  • 【下载频次】130
节点文献中: 

本文链接的文献网络图示:

本文的引文网络