摘要
对含有预制裂纹的中心穿透裂纹板和三点弯曲试样在动态载荷作用下进行了有限元模拟。前者裂纹面与载荷作用方向的夹角取15°～90°之间的6种情况，后者按纯Ⅰ型和纯Ⅱ型两种方式进行加载。得到了Ⅰ型和Ⅱ型动态应力强度因子的时间历程，并研究不同裂纹角对动态复合比的影响。结果表明：中心穿透裂纹板试样在15°和90°两种情况下KⅡ（t）和KⅠ（t）分剐占主导成分；45°时KⅠ（t）和KⅡ（t）基本相同；随着裂纹面与载荷夹角的增加KⅠ（t）呈增加趋势而KⅡ（t）呈先增加后减小趋势。三点弯曲试样按纯Ⅰ型加载时KⅡ（t）基本为零，按纯Ⅱ型加栽时KⅠ（t）幅值随时间而增加。
In this paper, finite element simulation of central-cracked plates with different angles between the load and the crack surface and of three-point bend specimens under impact loading are performed. The central-cracked plates are analyzed with six crack angles ranging from 15° to 90°, while the threepoint bend specimens are analyzed under two load modes Modes Ⅰ and Ⅱ Dynamic stress intensity factors （DSIF） of Modes Ⅰ and Ⅱare calculated and the effect of different crack angles on the ratio of KⅡ/KⅠ is studied. The results show that for the central-cracked plate specimen, KⅡ （t） is much lager than KⅠ （t） when the crack angle is 15° and that it is just opposite when the crack angle is 90°. KⅠ （t） and KⅡ （t） are nearly the same when the crack angle is 45°. With the increase of the crack angle, KⅠ （t） increases, while KⅠ （t） increases first and then decreases. The results of the three-point bend specimens show that under Mode Ⅱ load, KIⅠ（t） increases as time goes on, but under KⅠ load KⅡ（t） is almost zero.
出处
《机械科学与技术》
CSCD
北大核心
2006年第1期123-126,共4页
Mechanical Science and Technology for Aerospace Engineering
基金
国家自然科学基金委员会/中国工程物理研究院"NSAF"联合基金项目(10276033)资助
