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A METHOD FOR DIRECTLY ASSESSING ELASTIC FOLLOW UP IN 3D FINITE ELEMENT CALCULATIONS

机译:在3D有限元计算中直接评估弹性跟随的方法

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Elastic follow up significantly influences the creep and creep-fatigue life of structural components in elevated temperature service. As such, assessing the amount of follow up a component sees under a given loading history is critical in properly designing a component for high temperature use. Current methods for quantifying elastic follow up based on an elastic follow up factor use simple constitutive models and are available only for simple component geometries. This work describes a method for assessing the follow up factor, as a function of position and time, from a finite element simulation. The method recovers the simple, analytic solutions for simple geometries and material models but can also provide follow up factors for complicated components, loading histories, and material models. We use this new method to assess the range of follow up factors in a variety of prototypical high temperature structural components. This information can be used to improve design methods by better understanding the magnitude of follow up present in typical high temperature components. The method can also be used to support new design methods that require time-dependent point values of the follow up factor across a component.
机译:在高温条件下,弹性跟进会显着影响结构部件的蠕变和蠕变疲劳寿命。因此,评估组件在给定的加载历史下所能看到的跟进量对于正确设计用于高温的组件至关重要。当前基于弹性跟进因子来量化弹性跟进的方法使用简单的本构模型,并且仅适用于简单的零件几何形状。这项工作描述了一种方法,用于从有限元模拟中评估随位置和时间而变的随动因子。该方法可以为简单的几何形状和材料模型恢复简单的解析解,但也可以为复杂的零件,加载历史和材料模型提供后续因素。我们使用这种新方法来评估各种原型高温​​结构组件中的后续因素的范围。通过更好地了解典型高温组件中存在的跟进幅度,可以将这些信息用于改进设计方法。该方法还可以用于支持新的设计方法,这些方法需要跨组件的随时间变化的跟进因子的点值。

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