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71.
复合材料疲劳Ⅱ型层间裂纹扩展门槛值试验方法研究 总被引:1,自引:0,他引:1
疲劳裂纹扩展门槛值在结构损伤安全设计中具有重要作用,该文提出了复合材料Ⅱ型疲劳裂纹扩展门槛值的试验方法,并实测了两种复合材料的疲劳裂纹扩展门槛值。 相似文献
72.
A. P. Shabanov 《Journal of Applied Mechanics and Technical Physics》2005,46(6):861-866
A specimen with a crack shaped like a thin long defect with parallel edges and a rounded tip of finite radius is considered.
When the specimen is subjected to compressive cyclic loads, the stresses in zones adjacent to the crack tip vary according
to a sign-variable cycle because of plastic strains occurring at the crack tip. This can cause fatigue-crack growth. Results
of numerical simulations and experimental data support the possibility of fatigue-crack growth in the field of compressive
external stresses.
__________
Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 46, No. 6, pp. 108–115, November–December, 2005. 相似文献
73.
本文提供了一种可以进行自增强处理的圆筒试样,通过实验用柔度法确定了该试样的表面裂纹的应力强度因子,介绍了含表面裂纹试样的柔度测试技术,导出了柔度与表面裂纹尖端前缘各点的应力强度因子的关系式,该式可作为各种含表面裂纹试样柔度法测表面裂纹 K_1因子的参考,本文还测定了不同自增强程度下,自增强圆筒的表面裂纹疲劳扩展规律。 相似文献
74.
回火温度对40Cr钢疲劳裂纹萌生寿命的影响 总被引:2,自引:0,他引:2
用系统分析的方法,通过三点弯曲疲劳试验,以数值描述的方式,在线跟踪了40Cr钢及其在三种回火温度下疲劳裂纹萌生过程的疲劳损伤,实验结果表明:随着回火处理温度的提高,40Cr钢的疲劳裂纹萌生寿命都有不同程度的提高.但裂纹萌生寿命在低于450℃的温度范围里,随着回火温度的提高,裂纹萌生寿命有明显的提高,在450℃至580℃范围内,随回火温度的上升,裂纹萌生寿命则没有明显的增加. 相似文献
75.
A crystal plasticity model for hcp materials is presented which is based on dislocation glide and pinning. Slip is assumed to occur on basal and prismatic systems, and dislocation pinning through the generation of geometrically necessary dislocations (GNDs). Elastic anisotropy and, through the coupling of GNDs with slip rate, physically-based lengthscale effects are included. 相似文献
76.
Jiang Mingxiao Zhu Weiqiu Zhejiang University Hangzhou P. R. China 《Acta Mechanica Solida Sinica》1996,9(2):169-178
Two stochastic models of fatigue crack growth under constant amplitude cyclic loadingare proposed and studied by using the stochastic averaging method and total probability theorem to ac-count for high frequency component and low frequency component, respectively, of the irregular na-ture of fatigue crack growth observed in Virkler's experiment. Particular attention is paid to the predic-tion performance of the models under a change in the initial crack length. It is shown that the modelsproposed in the present paper yields better agreement with experimental data than other models avail-able in literature. 相似文献
77.
78.
A new photoelastic model for studying fatigue crack closure 总被引:1,自引:0,他引:1
The photoelastic analysis of crack tip stress intensity factors has been historically developed for use on sharp notches in
brittle materials that idealize the cracked structure. This approach, while useful, is not applicable to cases where residual
effects of fatigue crack development (e.g., plasticity, surface roughness) affect the applied stress intensity range. A photoelastic
model of these fatigue processes has been developed using polycarbonate, which is sufficiently ductile to allow the growth
of a fatigue crack. The resultant stress field has been modeled mathematically using the stress potential function approach
of Muskhelishvili to predict the stresses near a loaded but closed crack in an elastic body. The model was fitted to full-field
photoelastic data using a combination of a generic algorithm and the downhill simplex method. The technique offers a significant
advance in the ability to characterize the behavior of fatigue cracks with plasticity-induced closure, and hence to gain new
insights into the associated mechanisms. 相似文献
79.
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