C51嵌套汇编子程序在阻抗测试仪研制中的应用

C51嵌套汇编子程序，充分发挥了两种语言自的优势，介绍了C51调用汇编子程序的接品规则，并通过阻抗测试仪程序开发的例子予以详细说明。     

巨型机转子机制的改进策略

本文分析了通用寄存器型计算机和通用堆栈型计算机处理转子指令的不同方法,研究了类Cray-1转子机制的实现原理,提出了在类Cray-1通用寄存器型模型机上采用堆栈来处理转子指令的实现方法。     

基于最小二乘支持向量机的岩土本构关系曲线拟合

最小二乘支持向量机（Least Square Support Vector Machine,简称LSSVM）是对支持向量机（SVM）的一种改进,是继人工神经网络（ANN）之后又一新的机器学习方法。利用LSSVM拟合了利用Duncan-Chang本构模型的E-V模式数值模拟岩土的三轴实验得到的应力-应变函数曲线。通过对比分析,验证了LSSVM用于岩土本构关系曲线拟合的可行性和精确性。     

拉压异性纤维增强树脂基复合材料弹塑性问题的有限元分析

为了对复杂的非线性问题进行便捷求解,首先提出了考虑拉压异性的纤维增强树脂基复合材料统一非线性本构模型;然后,在此基础上进一步导出了本构模型的三维表现形式,以适用于非线性有限元分析工具的开发;随后,利用有限元软件ABAQUS提供的用户自定义子程序UMAT,自编了在二维和三维情况下的弹塑性应力分析程序;最后,应用程序对复合材料单向板和复合材料斜交板在偏轴拉伸/压缩下应力-应变曲线的预测与测试结果进行了比较,探讨了复合材料悬臂梁的弹塑性问题,并分析和比较了有无考虑拉压异性情况下应力分布和挠度响应的差异。结果表明:运用所提出的本构模型对考虑拉压不对称问题的弹塑性变形分析十分有效,这一本构模型有望成为实用数值分析工具,进而指导工程实践。     

Application of Gurson Model for Evaluation of Density‐Dependent Mechanical Behavior of Polyurethane Foam: Comparative Study on Explicit and Implicit Method

Recently, liquefied natural gas (LNG) is a focus of interest around the world for several reasons, and LNG cargo containment systems (CCS) increase in quality to prevent loss of LNG during shipping. For insulation of CCS, polyurethane foam (PUF), an outstanding insulation material, is commonly used. However, until now, although its mechanical properties are relatively good, the material is not considered as a structural member under compressive loading, principal load direction in CCS. Moreover, as PUF is a porous material by mixing and foaming, its mechanical properties depend on voids, which is a dominant parameter for density. Therefore, in the present study, nonlinear behavior of PUF is described using Gurson model with a novel technique, i.e., an acceleration factor. The model expresses the behavior through the volume fraction of voids with consideration of the density effect to evaluate structural performance using user‐defined material subroutine with explicit and implicit methods.

     

三角平衡轮廓轮胎滚动阻力的仿真研究

三角平衡轮廓轮胎是一种新型的轮胎结构,以低扁平率的传统轮廓轮胎255/30R22为基础,在其胎肩处和胎侧处增加高强度的支撑块来提高轮胎的性能。支撑块起到支撑胎面的作用,提高了胎侧的刚度。本文以滚动阻力计算公式和材料内耗机理为基础,用ABAQUS软件分别模拟2种轮胎的滚动阻力来验证三角平衡轮廓轮胎是否具有较低的滚动阻力。首先建立三角平衡轮廓轮胎和255/30R22轮胎的三维模型,施加相同载荷,对其进行以60km/h滚动工况的力学分析,算出单元积分点的生热率,提取每个单元的体积,最后计算每一种胶料的滚动阻力及轮胎总滚动阻力。通过两者的对比,三角平衡轮廓轮胎的滚动阻力仅18.7N,低于255/30R22轮胎滚动阻力的二分之一。     

板料成形过程有限元模拟中的接触处理

对板料成形过程进行有限元模拟时，为了取得可靠的计算结果，需要准确地描述模具与板料之间的动态接触状态．在全面分析成形中板料与模具接触边界动态变化的基础上，结合ABAQUS有限元分析软件给出了模型的几何描述、接触算法选择及应用VFRIC用户子程序进行接触摩擦模型的建立等具体方法．通过具体实例，证明了这些方法应用于板料成形过程的接触分析的可行性．     

Modeling strategies for unsteady turbulent flows in the lower plenum of the VHTR

Validation simulations are presented for turbulent flow in a staggered tube bank, geometry similar to the lower plenum of a gas-cooled high temperature reactor. Steady 2D RANS results are compared to unsteady 2D RANS results and experiment. The unsteady calculations account for the fact that nonturbulent fluctuations (due to vortex-shedding) are present in the flow. The unsteady computations are shown to predict the mean variables and the total shear stress quite well. Previous workers’ results indicate that 3D simulations are needed to obtain reasonable agreement; present results indicate 2D is sufficient. Best practices are based on requirements for the ASME Journal of Fluids Engineering.     

三维应力空间下改进状态变量的上下负荷面模型及其数值实现

为准确描述结构性土、超固结土的复杂弹塑性力学行为,对上下负荷面模型中的超固结状态变量R与结构性状态变量R*的演化规律进行改进,运用Sheng建议的破坏准则把模型的应用范围拓宽到三维应力空间,建立了三维应力空间下改进状态变量的上下负荷面模型。详细介绍了该模型隐式应力更新算法的数值实现过程,编制了对应的接口子程序,实现了对有限元软件的二次开发,并通过一系列数值模拟验证了模型的合理性、程序的精度与稳定性。最后应用本文模型模拟Boom黏土和Fujinomori黏土并与试验数据对比,结果表明,模型能够准确描述结构性土、超固结土的力学特征。     

Three‐dimensional Structural Analysis Approach for Aging Composite Solid Propellant Grains

The viscoelastic aging behavior of composite solid propellant grains is studied by a three‐dimensional thermoviscoelastic constitutive model with aging evolution, in which the crosslinking degree is taken as an aging variable. The resulting viscoelastic constitutive equations are numerically discretized into incremental form by integration algorithms, and the stress‐updating method is presented according to incremental law. Subsequently, the Abaqus‐based user material subroutine and its structural analysis module are constructed and validated through typical examples. Studies show that the results of structural analysis have high accuracy and are in well agreement with each other. The designed analysis module presents an effective aging‐mechanical analysis platform for further lifespan estimation of solid rocket motors.