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Crack Growth in Stainless Steel 304 Under Creep-Fatigue Loading

机译:蠕变疲劳载荷下不锈钢304的裂纹扩展

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摘要

Crack growth in compact specimens of type 304 stainless steel is studied at 538℃. Loading conditions include pure fatigue loading, static loading and fatigue loading with hold time. Crack growth rates are correlated with the stress intensity factor. A finite element analysis is performed to understand the crack tip field under creep-fatigue loading. It is found that fatigue loading interrupts stress relaxation around the crack tip and cause stress reinstatement, thereby accelerating crack growth compared with pure static loading. An effort is made to model crack growth rates under combined influence of creep and fatigue loading. The correlation with the stress intensity factor is found better when da/dt is used instead of da/dN. Both the linear summation rule and the dominant damage rule overestimate crack growth rates under creep-fatigue loading. A model is proposed to better correlate crack growth rates under creep-fatigue loading: da/dt =(da/dt)_c~Ψ(da/dt)_f~(1-Ψ) , where Ψ is an exponent determined from damage under pure fatigue loading and pure creep loading. This model correlates crack growth rates for relatively small loads and low stress intensity factors. However, correlation becomes poor as the crack growth rate becomes large under a high level of load.
机译:研究了在538℃下304型紧凑型试样的裂纹扩展。载荷条件包括纯疲劳载荷,静态载荷和具有保持时间的疲劳载荷。裂纹扩展速率与应力强度因子相关。进行有限元分析以了解蠕变疲劳载荷下的裂纹尖端场。发现疲劳载荷会中断裂纹尖端周围的应力松弛并导致应力恢复,从而与纯静态载荷相比,会加速裂纹的扩展。在蠕变和疲劳载荷的综合影响下,努力对裂纹扩展速率进行建模。当使用da / dt代替da / dN时,发现与应力强度因子的相关性更好。线性求和规则和主要破坏规则都高估了蠕变疲劳载荷下的裂纹扩展速率。提出了一个模型来更好地关联蠕变疲劳载荷下的裂纹扩展速率:da / dt =(da / dt)_c〜Ψ(da / dt)_f〜(1-Ψ),其中Ψ是由在以下条件下的损伤确定的指数纯疲劳载荷和纯蠕变载荷。该模型将裂纹扩展速率与相对较小的载荷和较低的应力强度因子相关联。但是,在高载荷下,裂纹扩展率越大,相关性越差。

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