浅析边坡稳定性分析的数值解

推导了坡面为两直线段斜坡的均质边坡稳定性安全系数函数式,利用遗传算法求出最危险滑弧位置、滑弧半径及相应的最小稳定性安全系数值,利用有限元法和接触摩擦弹簧元进行了边坡的渐进破坏分析,讨论了材料特性对边坡稳定性的影响。计算表明,渐进破坏分析所求出的稳定性安全系数比理论上求出的最小稳定性安全系数要小。     

膨胀薄壁圆管吸能特性研究

薄壁圆管的变形模式包括膨胀、撕裂、渐进压溃、欧拉屈曲等多种形式，文章通过ls-dyna软件对膨胀薄壁圆管的吸能特性进行了数值模拟。以建立的膨胀薄壁圆管有限元模型为研究对象，得到了在压模角度为30°、下压速度为5 m/s时，压模直径与膨胀薄壁圆管吸能特性之间的关系，得出当吸能特性最好时压模直径与膨胀薄壁圆管直径之间的比值D_d/D₀。通过相同尺寸的薄壁圆管在渐进压溃与膨胀2种变形模式下的吸能量对比，得到当D_d/D₀=1.22时，2种变形模式下圆管的吸能量基本相同；当1.22d/D₀<1.3时，膨胀圆管的吸能效果优于渐进压溃圆管；当D_d/D₀>1.3时，膨胀圆管出现压溃、撕裂等不稳定变形模式，吸能量开始下降。     

Ultimate strength analysis of composite stiffened panels based on multi-scale approach北大核心CSCD

［Objectives］As composite materials have varied internal structures, an in-depth analysis of the damage mechanisms of their component materials can provide a research foundation for the ultimate strength analysis of composite stiffened panels. ［Methods］The microscopic, mesoscopic and macroscopic mechanical analyses of marine glass fiber reinforced plastic (GFRP) composite stiffened panels are carried out using a multi-scale approach. Microscopic and mesoscopic representative volume element (RVE) models of chopped strand mat (CSM) and woven roving (WR) materials are established, and the macroscopic equivalent stiffness is obtained by homogenizing the RVE models. The ABAQUS VUMAT subroutine is used to code the progressive damage evolution model of the composite materials to derive the damage evolution mechanism of the microscopic and mesoscopic models respectively. The equivalent strength of macroscopic laminates is also obtained. ［Results］The multi-scale approach can be used to accurately evaluate the macroscopic mechanical properties of composite materials, and the ultimate strength of composite stiffened panels is mainly determined by fiber bundle failure. ［Conclusions］The obtained macroscopic material parameters can be used to calculate the ultimate strength of composite stiffened panels, while the parametric study of the mesomechanics of composite materials can provide an analysis tool for investigating the influence of material processing technology. © 2023 Chinese Journal of Ship Research. All rights reserved.     

基于渐进失效理论的碳纤维/泡沫夹芯设备舱底板强度仿真

设备舱底板在列车行驶过程中会受到气动载荷与石子冲击的影响，其强度直接影响到设备舱内的设备安全。文章基于渐进失效分析理论和刚度退化模型，在验证仿真建模的准确性后，建立了碳纤维/泡沫夹芯设备舱底板的静强度与低速冲击工况下的有限元模型。基于有限元模型分析了设备舱底板在5种静强度工况下的失效因子、应变和失效载荷，讨论了200 J、300 J、400 J、500 J的冲击能量以及100 mm、200 mm、300 mm的冲头直径对设备舱底板抗冲击性能的影响。结果表明，设备舱底板满足静强度要求，其失效载荷为63.0 kPa,最大失效因子及最大应变位置位于螺栓孔周围；冲击接触力峰值、上面板凹陷深度及各铺层的基体失效面积随冲击能量的增加而增大，而冲头直径的变化对设备舱底板的低速冲击性能影响较小。