A full multigrid method for eigenvalue problems

2016 ◽  
Vol 322 ◽  
pp. 747-759 ◽  
Author(s):  
Hongtao Chen ◽  
Hehu Xie ◽  
Fei Xu
2016 ◽  
Vol 59 (10) ◽  
pp. 2037-2048 ◽  
Author(s):  
ShangHui Jia ◽  
HeHu Xie ◽  
ManTing Xie ◽  
Fei Xu

Author(s):  
Manting Xie ◽  
Fei Xu ◽  
Meiling Yue

In this paper, a type of full multigrid method is proposed to solve non-selfadjoint Steklov eigenvalue problems. Multigrid iterations for corresponding selfadjoint and positive definite boundary value problems generate proper iterate solutions that are subsequently added to the coarsest finite element space in order to improve approximate eigenpairs on the current mesh. Based on this full multigrid, we propose a new type of adaptive finite element method for non-selfadjoint Steklov eigenvalue problems. We prove that the computational work of these new schemes are almost optimal, the same as solving the corresponding positive definite selfadjoint boundary value problems. In this case, these type of iteration schemes certainly improve the overfull efficiency of solving the non-selfadjoint Steklov eigenvalue problem. Some numerical examples are provided to validate the theoretical results and the efficiency of this proposed scheme.


2006 ◽  
Vol 13 (2-3) ◽  
pp. 275-291 ◽  
Author(s):  
M. Mehl ◽  
T. Weinzierl ◽  
Chr. Zenger

1994 ◽  
Vol 116 (3) ◽  
pp. 435-445 ◽  
Author(s):  
A. Arnone

A three-dimensional code for rotating blade-row flow analysis has been developed. The space discretization uses a cell-centered scheme with eigenvalue scaling for the artificial dissipation. The computational efficiency of a four-stage Runge–Kutta scheme is enhanced by using variable coefficients, implicit residual smoothing, and a full-multigrid method. An application is presented for the NASA rotor 67 transonic fan. Due to the blade stagger and twist, a zonal, nonperiodic H-type grid is used to minimize the mesh skewness. The calculation is validated by comparing it with experiments in the range from the maximum flow rate to a near-stall condition. A detailed study of the flow structure near peak efficiency and near stall is presented by means of pressure distribution and particle traces inside boundary layers.


2015 ◽  
Vol 1 (1) ◽  
pp. 207-228 ◽  
Author(s):  
Hongtao Chen ◽  
Yunhui He ◽  
Yu Li ◽  
Hehu Xie

2017 ◽  
Vol 10 (3) ◽  
pp. 639-655 ◽  
Author(s):  
M. M. Butt ◽  
Y. Yuan

AbstractA full multigrid method with coarsening by a factor-of-three to distributed control problems constrained by Stokes equations is presented. An optimal control problem with cost functional of velocity and/or pressure tracking-type is considered with Dirichlet boundary conditions. The optimality system that results from a Lagrange multiplier framework, form a linear system connecting the state, adjoint, and control variables. We investigate multigrid methods with finite difference discretization on staggered grids. A coarsening by a factor-of-three is used on staggered grids that results nested hierarchy of staggered grids and simplified the inter-grid transfer operators. A distributive-Gauss-Seidel smoothing scheme is employed to update the state- and adjoint-variables and a gradient update step is used to update the control variables. Numerical experiments are presented to demonstrate the effectiveness and efficiency of the proposed multigrid framework to tracking-type optimal control problems.


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