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Improved Convergence and Robustness of USM3D Solutions on Mixed Element Grids (Invited)

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(已邀请)

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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 Scheme (HAMS), has been developed and implemented. It 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 (RANS) equations and a nonlinear control of the solution update. Two variants of the new methodology 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 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,称为分层自适应非线性迭代方案(HAMS)。它围绕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的线性求解器,用于对雷诺平均Navier Stokes(RANS)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。新方法的两个变体在四个基准案例上进行了评估,即零压力梯度平板,通道凸出配置,NACA 0012机翼和NASA通用研究模型配置。与基线求解器技术相比,新方法提供了1.4到13的收敛加速因子。

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