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ANALYSIS OF FATIGUE CRACK GROWTH IN SHIP STRUCTURAL DETAILS

机译:船舶结构细节疲劳裂纹扩展分析

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Fatigue failure avoidance is a goal that can be achieved only if the fatigue design is an integral part of the original design program. The purpose of fatigue design is to ensure that the structure has adequate fatigue life. Calculated fatigue life can form the basis for meaningful and efficient inspection programs during fabrication and throughout the life of the ship. The main objective of this paper is to develop an add-on program for the analysis of fatigue crack growth in ship structural details. The developed program will be an add-on script in a pre-existing package. A crack propagation in a tanker side connection is analyzed by using the developed program based on linear elastic fracture mechanics (LEFM) and finite element method (FEM). The basic idea of the developed application is that a finite element model of this side connection will be first analyzed by using ABAQUS and from the results of this analysis the location of the highest stresses will be revealed. At this location, an initial crack will be introduced to the finite element model and from the results of the new crack model the direction of the crack propagation and the values of the stress intensity factors, will be known. By using the calculated direction of propagation a new segment will be added to the crack and then the model is analyzed again. The last step will be repeated until the calculated stress intensity factors reach the critical value.
机译:避免疲劳失效是只有在疲劳设计是原始设计程序的组成部分的情况下才能实现的目标。疲劳设计的目的是确保结构具有足够的疲劳寿命。计算得出的疲劳寿命可以构成在制造过程中以及整个船舶寿命中有意义且有效的检查程序的基础。本文的主要目的是开发一个附加程序,用于分析船舶结构细节中的疲劳裂纹扩展。开发的程序将是预先存在的软件包中的附加脚本。使用基于线性弹性断裂力学(LEFM)和有限元方法(FEM)的已开发程序,分析了油轮侧连接处的裂纹扩展。开发的应用程序的基本思想是,首先使用ABAQUS对这种侧连接的有限元模型进行分析,并从分析结果中揭示出最高应力的位置。在该位置,将初始裂纹引入到有限元模型中,并根据新裂纹模型的结果,知道裂纹扩展的方向和应力强度因子的值。通过使用计算出的传播方向,新的段将添加到裂缝中,然后再次分析模型。重复最后一步,直到计算出的应力强度因子达到临界值为止。

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