排序方式: 共有52条查询结果,搜索用时 250 毫秒
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粘塑性材料结构的有限元分析方法 总被引:6,自引:3,他引:3
本文针对Walker粘塑性本构方程,通过发展一自适应变步长积分算法,用户子程序的方法把该本构方程结合进了国际著名的非线性有限元软件ABAQUS,并进行了算例验证。它包括了四种单元类型,可考虑材料变形的率相关,加载的循环、非等温、变温等情况。适用于发动机热端部件非线性结构分析。 相似文献
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Because of its chemical and radiative properties, atmospheric ozone constitutes a key element of the Earth’s climate system.
Absorption of sunlight by ozone in the ultraviolet wavelength range is responsible for stratospheric heating, and determines
the temperature structure of the middle atmosphere. Changes in middle atmospheric ozone concentrations result in an altered
radiative input to the troposphere and to the Earth’s surface, with implications on the energy balance and the chemical composition
of the lower atmosphere. Although a wide range of ground- and satellite-based measurements of its integrated content and of
its vertical distribution have been performed since several decades, a number of uncertainties still remain as to the response
of middle atmospheric ozone to changes in solar irradiance over decadal time scales. This paper presents an overview of achieved
findings, including a discussion of commonly applied data analysis methods and of their implication for the obtained results.
We suggest that because it does not imply least-squares fitting of prescribed periodic or proxy data functions into the considered
times series, time-domain analysis provides a more reliable method than multiple regression analysis for extracting decadal-scale
signals from observational ozone datasets. Applied to decadal ground-based observations, time-domain analysis indicates an
average middle atmospheric ozone increase of the order of 2% from solar minimum to solar maximum, which is in reasonable agreement
with model results. 相似文献
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《中国航空学报》2020,33(4):1338-1348
The microstructural evolution mechanism and constitutive behavior of 2297 Al-Li alloy were studied via thermal compression test with the constant strain rates of 0.001–1 s−1 and the deformation temperatures ranging from 623 to 773 K. To verify the predictable ability of diverse constitutive models under different stress states, the hot compression experiments with stress triaxiality varying from −0.33 to 0.46 were conducted. The microstructures of the deformed specimens under diverse deformation conditions are probed to reveal the mechanism of hot deformation behavior. The experimental results indicate that the work-hardening and dynamic softening are competitive during the hot compression process, and the dynamic softening is more obvious under low deformation temperature and high strain rate. The microstructural analysis manifests that the dynamic recovery gets predominant at high deformation temperature to produce fine grains. Meanwhile, the dynamic recrystallization becomes more dominant as the strain rate decreases, which is sensitive to the stress triaxiality. In addition, both the modified Johnson-Cook model and strain-compensated Arrhenius-type function are suitable for describing the flow behavior of 2297 alloy, while the latter reveals a more accurate prediction. However, the predictability of the two kinds of models is worsened with the transformation of stress triaxiality, and the validity of the Arrhenius-type model is restricted by high stress triaxiality. 相似文献
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用于单晶叶片应力分析的滑移本构模型 总被引:1,自引:1,他引:0
为了建立适用于镍基单晶涡轮叶片的有限元分析平台,基于有限变形晶体滑移理论和有限元软件AN-SYS接口参数要求,导出了增量型本构方程公式。采用变刚度法,以切线系数法为初值,采用局部牛顿拉弗森迭代解法,编制了晶体弹塑性滑移本构模型程序,并以子程序Usermat的形式植入ANSYS软件。计算模拟了DD3试棒不同取向的单向拉伸和循环应力应变过程,讨论了〈011〉方向上的应变软化行为和该本构模型对DD3镍基单晶涡轮叶片的良好应用性。数值仿真结果与实验数据对比吻合良好,验证了程序的正确性。 相似文献
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分析了TiC颗粒增强钛基复合材料的微损伤演化规律,建立了含损伤演化的动态本构模型。TiC颗粒增强钛基复合材料在拉伸载荷作用下,微裂纹以翼型裂纹形式扩展,基于平面翼型裂纹扩展模型,建立了二维动态损伤本构关系,并退化到一维拉伸状态,假设微裂纹成核规律满足Weibull分布,得到了一维拉伸应力状态下能够反映TiC颗粒增强钛基复合材料的损伤演化规律的宏细观相结合的动态本构关系。模型计算结果与试验结果吻合较好。 相似文献
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