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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的裂纹增长

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Crack growth in compact specimens of type 304 stainless steel is studied at 538 deg C. 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~(psi)}{[(da)/(dt)]_f~(1-psi)}, where psi 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:538℃不锈钢型紧凑型试样的裂纹生长在538℃下进行。装载条件包括纯疲劳负载,静载荷和疲劳负载,保持时间。裂纹增长率与应力强度因子相关。进行有限元分析以了解蠕变疲劳负载下的裂缝尖端。发现疲劳负载在裂纹尖端周围中断应力松弛并引起应力恢复,从而与纯静载荷相比加速裂纹生长。在蠕变和疲劳载荷的综合影响下,努力模拟裂纹增长率。当使用DA / DT而不是DA / DN时,与应力强度因子的相关性更好地发现。线性求和规则和主导损伤规则在蠕变 - 疲劳负荷下高估裂纹增长率。提出了一种模型以在蠕变 - 疲劳负载下更好地相关裂纹生长速率:(da)/(dt)= {[(da)/(dt)] _c〜(psi)} {[(da)/(dt)] _F〜(1-PSI)},其中PSI是从纯疲劳负荷和纯蠕变加载下的损伤确定的指数。该模型与相对较小的负载和低应力强度因子相关联的裂纹增长率。然而,随着裂缝的生长速率在高载荷级别变大,相关性变差。

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