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On fatigue crack growth in plastically compressible hardening and hardening-softening-hardening solids using crack-tip blunting

机译:用裂纹尖端钻孔疲劳可压缩硬化和硬化软化硬化固体疲劳裂纹增长

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In the present study, mode I crack subjected to cyclic loading has been investigated for plastically compressible hardening and hardeningsoftening- hardening solids using the crack tip blunting model where we assume that the crack tip blunts during the maximum load and re- sharpening of the crack tip takes place under minimum load. Plane strain and small scale yielding conditions have been assumed for analysis. The influence of cyclic stress intensity factor range ( K), load ratio ( R), number of cycles ( N), plastic compressibility ( a) and material softening on near tip deformation, stress- strain fields were studied. The present numerical calculations show that the crack tip opening displacement ( CTOD), convergence of the cyclic trajectories of CTOD to stable self- similar loops, plastic crack growth, plastic zone shape and size, contours of accumulated plastic strain and hydrostatic stress distribution near the crack tip depend significantly on K, R, N, a and material softening. For both hardening and hardening- softening- hardening materials, yielding occurs during both loading and unloading phases, and resharpening of the crack tip during the unloading phase of the loading cycle is very significant. The similarities are revealed between computed near tip stress- strain variables and the experimental trends of the fatigue crack growth rate. There was no crack closure during unloading for any of the load cycles considered in the present study.
机译:在本研究中,已经研究了对循环负载进行循环加载的模式I裂纹,用于使用裂缝尖端钻孔模型进行塑性可压缩的硬化和硬化固化固体,其中我们假设在最大负载和裂纹尖端的最大载荷和重新锐化期间裂缝尖端钝化在最小负载下发生。已经假设平面应变和小规模的条件进行分析。研究了循环应力强度因子范围(k),负荷比(R),循环次数,塑料压缩性(A)和近尖端变形的材料,应力 - 应变场的影响。目前的数值计算表明,裂纹尖端开口位移(CTOD),CTOD环状轨迹的收敛性稳定的自相似环,塑料裂纹生长,塑料区形状和尺寸,累积塑性应变的轮廓和静压应力分布附近裂纹尖端显着取决于K,R,N,A和材料软化。对于硬化和硬化 - 软化 - 硬化材料,在装载和卸载期间发生屈服,并且在装载循环的卸载阶段中的裂纹尖端重新抛弃裂纹尖端是非常显着的。在疲劳裂纹生长速率的计算近尖应力变量和实验趋势之间揭示了相似性。在本研究中考虑的任何载荷周期卸载期间没有裂缝关闭。

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