共查询到15条相似文献,搜索用时 46 毫秒
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将动态焦散线法与高速摄影技术相结合,本文记录了高分子材料悬臂梁内裂纹扩展加速、减速过程。一方面,利用动态焦散线可确定扩展裂尖的瞬态应力强度因子;另一方面,利用最小二乘法将裂纹扩展的水平、垂直位移分量拟合成时间(t)的四次多项式,描述了裂纹扩展方向、裂纹扩展加速度以及裂纹扩展加速度与动态应力强度因子的关系。结果表明:裂纹扩展加速度与动态应力强度因子之间存在一定的依赖关系;利用最小二乘法将裂纹扩展的水平、垂直分量拟合成时间(t)的四次多项式,可以对裂纹的扩展方向、加速度进行定量分析。 相似文献
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本文利用弹性力学及复变函数理论,对异弹簧V型切口附近应力场进行了分析,给出了该切口附近应力分量的显式表达式,对该情况下的应力强度因子应如何定义进行了。 相似文献
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利用爆炸加载数字激光动态焦散线试验系统,同时借助ABAQUS有限元分析中内聚力模型数值计算方法,研究了爆炸应力波作用下缺陷介质裂纹扩展规律,并将试验结果与数值计算结果进行了对比。研究表明:在爆炸应力波作用下预制缺陷两端产生了两条翼裂纹A、B,扩展长度基本相同,方向垂直于预制缺陷。两条翼裂纹的扩展基本是对称的,只是在尾端发生轻微翘曲;翼裂纹扩展速度先增大至峰值又振荡减小,之后又增大至第二个较小的峰值,然后又减小,这种变化趋势和裂纹尖端应力强度因子KⅠ保持一致;扩展角β为85°时,计算结果较为接近试验,内聚力模型为动态裂纹扩展的研究提供了一种有效的方法。 相似文献
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利用高速摄影技术与光学焦散线技术相结合,对冲击下正交复合材料Ⅰ型裂纹尖端的动态应力集中问题进行了光测力学实验研究。记录了两种层状碳纤维/环氧树脂复合材料在冲击作用下Ⅰ型裂纹尖端的动态焦散斑图,提取反映材料局部应力集中问题的力学参数:焦散斑特征尺寸,进而比较两种复合材料的抗冲击性能。这些研究工作对于复合材料冲击性能评估具有工程应用价值和科学研究意义。 相似文献
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为探究邻近巷道裂纹缺陷受爆炸荷载作用的扩展机理,采用透射式动态焦散线实验系统进行模拟实验。结果表明,对迎爆侧隐性裂纹,当裂纹与巷道左壁相对距离10 mm时,裂纹右尖端扩展因巷道的存在使预制裂纹导向作用更显著,引导爆生主裂纹与预制裂纹左尖端贯穿,衍射后作用于右尖端反射拉伸引起;对背爆侧隐性裂纹,当裂纹与巷道右壁相对距离4 mm时,裂纹扩展源于薄弱的巷道临空面将绕射的应力波能传递并导向裂纹缺陷,裂纹受拉扩展贯穿。巷道存在会增加其围岩裂纹缺陷处动应力集中,在爆炸应力波作用下会诱发裂纹扩展。 相似文献
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The practical applications of studies related to constant amplitude mode I loading are somewhat limited in situations where more than one mode exists. So, criteria, rules and laws for these situations have to be validated with experiments. This paper extends previous results by the authors for mixed-mode I and II fatigue loading. An effective stress intensity factor range which considers crack closure and crack surface interference is described for the analysis of a crack under mixed-mode I and II fatigue loadings, and this factor is assessed from experimental results. 相似文献
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I. Ohkawa H. Takahashi M. Moriwaki M. Misumi 《Fatigue & Fracture of Engineering Materials & Structures》1997,20(6):929-940
Abstract— Fatigue tests were performed on thin-walled tubular specimens of S45C steel under tension-compression, pure torsion, in-phase and out-of-phase axial-torsional loadings. The relationship between cracking behaviour and stress components on the crack plane was investigated. Measurement of microcrack density showed that microcracking was governed predominantly by the shear stress amplitude acting on the crack plane for all loading conditions. The failure crack was formed by coalescence of many cracks initiated near the maximum shear planes. The cracks grew turning their orientation to the direction perpendicular to the maximum normal stress. The transition of crack orientation occurred at relatively longer crack lengths at a higher stress ratio. The crack growth behaviour for all loading modes can be correlated using an equivalent strain intensity parameter based on shear and normal strains on the crack plane. 相似文献
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Y. N. Lenets 《Fatigue & Fracture of Engineering Materials & Structures》1997,20(2):249-256
Abstract— The behaviour of fatigue cracks in an Al-alloy under cyclic compression, either with or without overloads, was studied. For constant-amplitude compressive cycling, a non-catastrophic (saturation) character of the fatigue crack behaviour was confirmed, with the final depth of a crack depending on the applied load level. Single (tensile or compressive) intermittent overloads were shown to re-activate a previously arrested crack while reversed (tensile—compressive or compressive—tensile) ones were also shown to maintain continual fatigue crack extension under otherwise fully compressive cycling. 相似文献