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Prediction of Low Cycle Fatigue Crack Growth under Mixed-Mode Loading Conditions using Cohesive Zone Models

机译:利用粘性区模型预测混合模式负载条件下的低循环疲劳裂纹生长

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Damage tolerant design is based on reliable fatigue crack growth methods for both high cycle and low cycle fatigue problems. While the Paris' law can be applied for estimate crack growth life in quasi-elastic materials, elastic-plastic fatigue crack growth needs more accurate computational models. In the past decade numerous cohesive zone models were proposed and investigated for predicting elastic-plastic fatigue crack growth. However, most cohesive zone models were used to reproduce fatigue crack growth with vanishingly small scale yielding and failed to predict low cycle fatigue crack growth with the finite plastic zone. In the present work a new CCZM is introduced for the high fatigue crack growth rate and attempting to give a uniform description from cyclic fatigue crack growth to elastoplastic rupture in ductile materials. The damage accumulation equation in the cohesive model contains both monotonic damage as well as cyclic damage mechanism. Experimental verification was carried out in an austenitic stainless steel AISI 304 through fracture tests and fatigue crack growth tests of compact tension (CT) specimens under mode I and compact-tension shear (CTS) specimens under mixed mode loading conditions. Detailed finite element computations confirmed that the present cohesive zone model provides a uniform description for the whole fatigue crack growth regimes. The model parameters can be determined in the conventional CT specimens. The cohesive zone model has the potential to be applied for more complex structural failure analysis.
机译:损伤容限的设计是基于对两个高周期和低循环疲劳的问题可靠疲劳裂纹生长的方法。虽然可以在准弹性材料,弹性 - 塑性疲劳裂纹增长的需要更精确的计算模型被应用于估计裂纹扩展寿命巴黎的法律。在过去十年中无数内聚力模型,提出并研究了预测弹塑性疲劳裂纹扩展。然而,大多数内聚带模型来再现疲劳裂纹增长与微乎其微规模屈服和未能预测低周疲劳裂纹增长与有限塑性区。在本工作的新CCZM被引入用于高疲劳裂纹扩展速率和试图给从循环疲劳裂纹扩展到弹塑性破裂一个统一的描述韧性材料。在粘结模型中的损伤累积方程包含两个单调损伤以及环损坏机制。 (CT)下试样模式实验验证在奥氏体不锈钢AISI 304通过断裂试验和紧凑拉伸的疲劳裂纹增长进行的测试I和紧凑张力剪切(CTS)混合模式加载条件下的样品。详细的有限元计算证实本内聚力模型提供了用于整个疲劳裂纹扩展制度一个统一的描述。该模型的参数可以在常规的CT试样来确定。的内聚力模型必须施加用于更复杂的结构失效分析的潜力。

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