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Modification of Multiresolution Analysis for Efficient Implicit Temporal Integration

机译:高效隐式时间积分的多分辨率分析的修改

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摘要

A modified method has been suggested to improve the computational efficiency of a multiresolution analysis for implicit temporal integrations. The fundamental idea behind multiresolution analysis is that high cost computations such as flux evaluation are performed only at the cells where the salient flow features exist, thereby reducing the computational cost. The multiresolution analysis, however, suffers from numerical inefficiency in implicit time integration because the efficiency of the multiresolution analysis method arises mainly from a reduction in the expensive flux evaluation for spatial discretization. This paper demonstrates that the implicit temporal integration of multiresolution analysis can be substantially improved by reducing the implicit operator matrix to the size of the additional residual dataset. To suppress the numerical error from the reduced implicit operation, the operator matrix is derived based on the additional residual dataset constructed by the decomposition and thresholding of the residuals, and the thresholding criterion is modified to retain the numerical accuracy at a high Courant-Friedrichs-Lewy number. The accuracy and efficiency of the present modified multiresolution analysis are verified through various application flow problems, such as a stationary vortex, a steady airfoil, an airfoil vortex interaction, and a transonic wing, ranging from two-dimensional steady/unsteady to three-dimensional steady applications. The results show that the computing speed of the modified multiresolution analysis with lower-upper symmetric Gauss-Seidel is about twice as fast as that of a baseline computational fluid dynamics solver on steady and unsteady simulations, while maintaining the accuracy of the solver.
机译:已提出一种改进的方法来提高隐式时间积分的多分辨率分析的计算效率。多分辨率分析背后的基本思想是,仅在存在显着流量特征的单元中执行诸如通量评估之类的高成本计算,从而降低了计算成本。但是,多分辨率分析在隐式时间积分方面存在数值效率低下的问题,因为多分辨率分析方法的效率主要来自减少用于空间离散化的昂贵通量评估。本文证明,通过将隐式算子矩阵减小为其他残差数据集的大小,可以大大改善多分辨率分析的隐式时间集成。为了抑制来自简化隐式运算的数值误差,根据由残差的分解和阈值构造的附加残差数据集,导出了算子矩阵,并对阈值标准进行了修改,以在高Courant-Friedrichs-路易号。本修正的多分辨率分析的准确性和效率通过各种应用程序流动问题进行了验证,例如固定涡旋,稳定翼型,翼型涡旋相互作用和跨音速机翼,范围从二维稳态/非稳态到三维稳定的应用程序。结果表明,在稳定和不稳定模拟中,具有较低的上对称高斯-赛德尔分布的改进的多分辨率分析的计算速度约为基线计算流体动力学求解器的两倍,同时保持了求解器的精度。

著录项

  • 来源
    《AIAA Journal》 |2016年第11期|3546-3563|共18页
  • 作者单位

    Pusan Natl Univ, Dept Aerosp Engn, Busan 609735, South Korea;

    Dongyang Mirae Univ, Dept Mech Engn, Seoul 152714, South Korea;

    Pusan Natl Univ, Dept Aerosp Engn, Busan 609735, South Korea;

    Seoul Natl Univ, Dept Mech & Aerosp Engn, Seoul 151742, South Korea;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
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