偏置三维内裂纹单轴拉伸裂纹扩展数值模拟
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TV223.1

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Numerical simulation of one-axis tensile crack propagation of bias three-dimensional internal crack
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    摘要:

    为研究偏置三维内裂纹在单轴应力下的裂纹扩展过程,利用三维裂纹计算软件Franc3d软件进行了数值模拟,得到了裂纹扩展过程及裂纹前缘的应力强度因子变化,计算结果表明:(1)单轴拉力作用下,预制裂纹尖端首先出现翼型裂纹,随后裂纹逐渐向四周扩展,裂纹先贯穿试件左右两面,而后贯穿试件的前后面形成贯穿型裂纹.(2)三维预制内裂纹倾角α=0°、30°时,预制裂纹尖端翼裂纹扩展后期两个翼裂纹呈现相互吸引的规律,而当三维预制内裂纹倾角α=45°、60°时,翼裂纹之间则不存在相互吸引靠近的趋势,预制裂纹内侧尖端的翼裂纹扩展要小于预制裂纹外侧尖端.(3)相对Ⅰ型应力强度因子随着预制裂纹尖端距离的变化(从相对距离0变化到相对距离1)呈现先增大后减小再增大再减小的规律,相对Ⅱ型应力强度因子随着预制裂纹尖端距离的变化呈现先减小后增大再减小再增大的趋势.

    Abstract:

    In order to study the process of crack propagation under uniaxial stress,the crack propagation process and the stress intensity factor of the front edge of the crack are obtained by the numerical simulation of the threedimensional crack calculation software Franc 3d.The results show that:(1)under uniaxial tension,the wing crack first appears at the tip of the precast crack,and then the crack propagates around the specimen.The crack first runs through both sides of the specimen and then through the front and back of the specimen.(2)in the case of three dimensional precast internal crack inclination α=0 degree and 30 degree,the two wing cracks at the tip of the precast crack tip exhibit mutual attraction during the later stage of crack growth.When the angle of internal crack is 45°and 60°,there is no tendency to attract and approach each other between wing cracks,and the propagation of wing crack at the inner tip of precast crack is smaller than that on the outer tip of precast crack.(3)the relative mode Istress intensity factor changes with the distance of prefabricated crack tip(from relative distance 0 to relative distance 1).Compared with the modeⅡ stress intensity factor,the stress intensity factor decreases first and then decreases and then increases with the change of the distance between the prefabricated crack tip and the crack tip.

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刘丹珠,王义兴,肖 望.偏置三维内裂纹单轴拉伸裂纹扩展数值模拟[J].江西水利科技,2019,(1):

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  • 在线发布日期: 2019-04-11
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