首页> 外文期刊>Journal of Computational Physics >Development and convergence analysis of an effective and robust implicit Euler solver for 3D unstructured grids
【24h】

Development and convergence analysis of an effective and robust implicit Euler solver for 3D unstructured grids

机译:3D非结构化网格的有效和强大隐式欧拉求解器的开发和收敛性分析

获取原文
获取原文并翻译 | 示例
       

摘要

This paper reports the development and convergence analysis in steady-state of an effective and robust implicit finite-volume solver for compressible Euler equations on three-dimensional unstructured grids. A second-order upwind scheme (MUSCL) was employed based on Roe's approximate Flux-Difference Scheme (FDS) by using Venkatrakishnan flux limiters. The construction of the linear system for the implicit scheme was performed by applying the backward Euler on the left-hand side of the conservation equation and Newton-type linearization on the right-hand side. The Jacobian matrix that resulted from the linearization process was computed analytically using Roe flux terms. In this phase, the defect-correction technique was employed allowing effective time-dependent computations by an implicit time-integration scheme. In this approach, the flux integral on the right-hand side is computed based on a high-order of accuracy whilst the left-hand side the Jacobian is performed based on the low-order. The resulting sparse and large system of linear equations is solved by a sequential Gauss-Seidel iterative method. Simulations were performed and the developed implicit defect-correction solver was validated and verified. In addition, convergence analysis comparing the implicit solver and the explicit Runge-Kutta of 5-steps using Implicit Residual Smoothing (IRS) were performed showing the significant speed-up of the implicit solver over the explicit one. Simulations were performed for case studies to demonstrate the robustness of the developed implicit defect-correction solver in solving typical problems of aerodynamic involving transonic condition and shock wave captures for internal and external flows. Finally, the main particularities of the implicit scheme were investigated and discussed considering the simulation results, showing also its capacity to serve as an effective preconditioner (start-up method) to other implicit techniques. (C) 2018 Elsevier Inc. All rights reserv
机译:本文报告了在三维非结构化网格上的可压缩欧拉方程的有效和强大的隐式有限音量求解器的稳态开发和收敛性分析。通过使用Venkatrakishnan助焊剂限制器基于ROE的近似通量差分方案(FDS)使用二阶Upwind方案(Muscl)。通过在右侧右侧施加留下左侧的左侧侧面施加后侧侧面来执行用于隐式方案的线性系统的结构。由线性化过程引起的雅可比矩阵使用ROE通量术语分析计算。在该阶段,采用缺陷校正技术通过隐式的时间集成方案允许有效的时间依赖计算。在这种方法中,基于高阶精度计算右侧侧的磁通量,同时基于低阶执行Jacobian的左侧。通过顺序高斯-Seidel迭代方法解决了所得到的稀疏和大型线性方程系统。执行模拟,验证并验证了发达的隐式缺陷校正求解器。另外,使用隐式残差平滑(IRS)进行隐式求解器和5步骤的显式runge-kutta的收敛分析,示出了明确的求解器的显着加速。为案例研究进行了模拟,以展示发达的隐式缺陷校正求解器的鲁棒性,以解决涉及内部和外部流动的跨音状态和冲击波捕获的空气动力学的典型问题。最后,考虑到模拟结果,研究了隐性方案的主要特征,并讨论了其作为其他隐式技术的有效预处理器(启动方法)的能力。 (c)2018 Elsevier Inc.全权储备

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号