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An adaptive mesh refinement approach based on optimal sparse sensing

机译:一种基于最优稀疏感测的自适应网格细化方法

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摘要

We introduce a new approach for adaptive mesh refinement in which adaptivity is driven by low rank decomposition and optimal sensing of the dynamically evolving flow field. This method seeks an ordered set of locations for mesh adaptation from the instantaneous data-driven basis of an online proper orthogonal decomposition of the velocity, which organizes features into sparse optimal orthogonal modes based on an energy norm. The sensing is achieved via a computationally expedient discrete empirical interpolation method using rank-revealing QR factorization (Drmac and Gugercin SIAM J Sci Comput 38(2):A631-A648, 2016). The methodology is applicable to a wide range of numerical discretizations, and is tested on a spatiotemporally evolving incompressible turbulent jet, a complex wind turbine wake, and supersonic flow over a forward-facing step. The proposed approach is demonstrated to predict accurate velocity statistics and yield significantly smaller grids in comparison to gradient-based methods. The algorithm is seen to focus refinement in the vicinity of dynamically significant regions such as those characterized by high turbulence kinetic energy, coherent structures and shock interactions. Moreover, the approach does not require parameters or thresholds, which may be difficult to obtain for complex flows, to be known a priori to facilitate mesh adaptation.
机译:我们介绍了一种新的自适应网格精制方法,其中适应性由低秩分解驱动和动态演化流场的最佳感测。该方法寻求一种有序的位置集,用于从速度的在线适当的正交分解的瞬时数据驱动的基础上的网格自适应,这基于能量规范组织成稀疏最佳正交模式的特征。通过计算QR分解(DRMAC和GUGERCIN SIAM J SCI Comput 38(2):A631-A648,2016),通过计算有利的离散经验插值方法实现感测。该方法适用于各种数值离散化,并在正面的步骤中测试了在瞬发不可压缩的不可压缩的湍流射流,复杂的风力涡轮机唤醒和超音速流动。所提出的方法被证明是为了预测准确的速度统计,与基于梯度的方法相比,加强了显着较小的网格。该算法被视为聚焦在动态有效区域附近的细化,例如高湍流动能,相干结构和冲击相互作用的那些。此外,该方法不需要参数或阈值,这可能难以获得复杂的流量,以便于先验以便于网格自适应。

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