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ADJOINT METHOD TO CALCULATE THE SHAPE GRADIENTS OF FAILURE PROBABILITIES FOR TURBOMACHINERY COMPONENTS

机译:涡轮机部件失效概率的形状梯度计算的辅助方法

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In the optimization of turbomachinery components, shape sensitivities for fluid dynamical objective functions have been used for a long time. As peak stress is not a differential functional of the shape, such highly efficient procedures so far have been missing for objective functionals that stem from mechanical integrity. This changes, if deterministic lifing criteria are replaced by probabilistic criteria, which have been introduced recently to the field of low cycle fatigue (LCF). Here we present a finite element (FEA) based first discretize, then adjoin approach to the calculation of shape gradients (sensitivities) for the failure probability with regard to probabilistic LCF and apply it to simple and complex geometries, as e.g. a blisk geometry. We review the computation of failure probabilities with a FEA postprocessor and sketch the computation of the relevant quantities for the adjoint method. We demonstrate high accuracy and computational efficiency of the adjoint method compared to finite difference schemes. We discuss implementation details for rotating components with cyclic boundary conditions. Finally, we shortly comment on future development steps and on potential applications in multi criteria optimization.
机译:在优化涡轮机械部件时,对流体动力学目标函数的形状敏感度已使用了很长时间。由于峰值应力不是形状的微分函数,因此到目前为止,对于源自机械完整性的目标函数,还缺少这种高效的过程。如果确定性的生活标准被概率标准所取代,则这种情况将发生变化,而概率标准最近已引入低周疲劳(LCF)领域。在这里,我们提出基于有限元(FEA)的先离散化,然后采用伴随方法来计算概率LCF的失效概率的形状梯度(灵敏度),并将其应用于简单和复杂的几何形状,例如叶状几何。我们使用有限元分析后处理程序回顾了故障概率的计算,并为伴随方法绘制了相关量的计算草图。与有限差分方案相比,我们证明了伴随方法的高精度和计算效率。我们讨论具有循环边界条件的旋转组件的实现细节。最后,我们不久将评论未来的开发步骤以及在多标准优化中的潜在应用。

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