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Improved Convergence and Robustness of USM3D Solutions on Mixed-Element Grids

机译:改进的USM3D解决方案在混合元素网格上的收敛性和鲁棒性

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摘要

Several improvements to the mixed-element USM3D discretization and defect-correction schemes have been made. A new methodology for nonlinear iterations, called the Hierarchical Adaptive Nonlinear Iteration Method, has been developed and implemented. The Hierarchical Adaptive Nonlinear Iteration Method provides two additional hierarchies around a simple and approximate preconditioner of USM3D. The hierarchies are a matrix-free linear solver for the exact linearization of Reynolds-averaged Navier-Stokes equations and a nonlinear control of the solution update. Two variants of the Hierarchical Adaptive Nonlinear Iteration Method are assessed on four benchmark cases, namely, a zero-pressure-gradient flat plate, a bump-in-channel configuration, the NACA 0012 airfoil, and a NASA Common Research Model configuration. The new methodology provides a convergence acceleration factor of 1.4 to 13 over the preconditioner-alone method representing the baseline solver technology.
机译:已经对混合元素USM3D离散化和缺陷校正方案进行了一些改进。已经开发并实现了一种新的非线性迭代方法,称为层次自适应非线性迭代方法。层次自适应非线性迭代方法围绕USM3D的简单近似预处理器提供了两个附加层次结构。该层次结构是无矩阵线性求解器,用于对雷诺平均Navier-Stokes方程进行精确的线性化,以及对解决方案更新进行非线性控制。在四个基准情况下评估了分层自适应非线性迭代方法的两个变体,分别是零压力梯度平板,通道凸点配置,NACA 0012机翼和NASA通用研究模型配置。与代表基线求解器技术的单独预处理器方法相比,新方法提供了1.4到13的收敛加速因子。

著录项

  • 来源
    《AIAA Journal》 |2016年第9期|2589-2610|共22页
  • 作者单位

    NASA Langley Res Ctr, Configurat Aerodynam Branch, Mail Stop 499, Hampton, VA 23681 USA;

    Natl Inst Aerosp, Hampton, VA 23666 USA|Univ Virginia, MAE Dept, Charlottesville, VA USA;

    NASA Langley Res Ctr, Computat Aerosci Branch, Mail Stop 499, Hampton, VA 23681 USA;

    NASA Langley Res Ctr, Computat Aerosci Branch, Mail Stop 499, Hampton, VA 23681 USA;

  • 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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