以结构力学为理论依据,以有限单元法为基础,借助和参考有关有限元程序设计方法,按照结构系统可靠性失效模式分析的要求,采用编程语言研制成功基于有限元的可靠性分析软件RAPS(Reliability Analysis Program of Structure based on FEM)...以结构力学为理论依据,以有限单元法为基础,借助和参考有关有限元程序设计方法,按照结构系统可靠性失效模式分析的要求,采用编程语言研制成功基于有限元的可靠性分析软件RAPS(Reliability Analysis Program of Structure based on FEM),运用该软件对立体车库钢结构的可靠性进行具体的分析;对判定结构系统失效与否的失效准则进行讨论和分析,并针对立体车库钢结构,得出合理的失效准则和系统可靠度的计算方法;通过实例说明约界参数CAP、失效路径长度和系统复杂程度对失效准则和系统可靠度结果的影响。展开更多
A two-dimensioual stress analysis was developed to evaluate the failure of composite joints using characteristic length method. In this study, the accuracy of characteristic length method on the prediction of failure ...A two-dimensioual stress analysis was developed to evaluate the failure of composite joints using characteristic length method. In this study, the accuracy of characteristic length method on the prediction of failure strength and failure mode using different failure criteria was investigated. The stresses required for evaluating the joints were computed from stress functions obtained from displacement expressions that satisfy boundary conditions of the hole. The available experimental data for joint strength in literature were compared with the predicted failure loads and modes of failure for different composite pinned joints. No single failure criterion utilized to evaluate the failure gave a universally best fit across the three joints evaluated. However, the accuracy of characterizing the joints failure varies with joint laminate and choice of failure criterions.展开更多
文摘以结构力学为理论依据,以有限单元法为基础,借助和参考有关有限元程序设计方法,按照结构系统可靠性失效模式分析的要求,采用编程语言研制成功基于有限元的可靠性分析软件RAPS(Reliability Analysis Program of Structure based on FEM),运用该软件对立体车库钢结构的可靠性进行具体的分析;对判定结构系统失效与否的失效准则进行讨论和分析,并针对立体车库钢结构,得出合理的失效准则和系统可靠度的计算方法;通过实例说明约界参数CAP、失效路径长度和系统复杂程度对失效准则和系统可靠度结果的影响。
文摘A two-dimensioual stress analysis was developed to evaluate the failure of composite joints using characteristic length method. In this study, the accuracy of characteristic length method on the prediction of failure strength and failure mode using different failure criteria was investigated. The stresses required for evaluating the joints were computed from stress functions obtained from displacement expressions that satisfy boundary conditions of the hole. The available experimental data for joint strength in literature were compared with the predicted failure loads and modes of failure for different composite pinned joints. No single failure criterion utilized to evaluate the failure gave a universally best fit across the three joints evaluated. However, the accuracy of characterizing the joints failure varies with joint laminate and choice of failure criterions.
