EXPANDABLE PARALLEL FINITE ELEMENT METHODS FOR LINEAR ELLIPTIC PROBLEMS∗
2020-06-04
School of Mathematics and Statistics,Shandong Normal University,Jinan 250014,China
E-mail:guangzhidu@gmail.com
Abstract In this article,two kinds of expandable parallel finite element methods,based on two-grid discretizations,are given to solve the linear elliptic problems.Compared with the classical local and parallel finite element methods,there are two attractive features of the methods shown in this article:1)a partition of unity is used to generate a series of local and independent subproblems to guarantee the final approximation globally continuous;2)the computational domain of each local subproblem is contained in a ball with radius of O(H)(H is the coarse mesh parameter),which means methods in this article are more suitable for parallel computing in a large parallel computer system.Some a priori error estimation are obtained and optimal error bounds in both H1-normal and L2-normal are derived.Finally,numerical results are reported to test and verify the feasibility and validity of our methods.
Key words Two-grid method;expandable method;partition of unity;parallel algorithm;finite element method
1 Introduction
In recent years,the development of efficient parallel computing for PDEs with high resolution has been an hot research topic.On the basis of the understanding of the local and global properties of a finite element solution to PDEs with high resolution,a new local and parallel approach[20,21],was first proposed for a class of linear and nonlinear elliptic boundary value problems by Xu and Zhou.This local and parallel finite element algorithm was further applied for the Stokes and Navier-Stokes equations by He et al.[12–14,18]and for the mixed Stokes-Darcy problems by Du et al.[7–9].The algorithm has low communication complexity and allows existing sequential existing codes to run in a parallel environment with little investment in recoding.
However,one disadvantage of these local finite element algorithms is that the finite element solution is in general discontinuous.To overcome this defect,the author in[20]modified the above method to ensure that the final approximation is continuous.Furthermore,some local finite element methods based on a partition of unity are proposed in[6,15,22–25]to derive the globally continuous solution by assembling all the local solutions via the flexible and controllable partition of unity functions.The partition of unity method[3,17]introduces us to a flexible and controllable way to implement domain decomposition and construct a global solution.There are many interesting works about the partition of unity method.For example,Hou et al.[15]developed an expandable local and parallel two-grid finite element scheme by considering the case of the Poisson equation,while for the computational fluid dynamic problems,Zheng et al.[22–25]proposed some new partition of unity methods based on two-grid discretiaztions and Appelhans et al.[2]proposed a new,low-communication algorithm for solving PDEs on massively parallel computers based on range decomposition.Larson et al.[16]and Song et al.[19]utilized the partition of unity method as the localization technique in post-processing procedure,and Bank et al.[4]presented a new domain decomposition algorithm for the parallel finite element solution of elliptic partial differential equations.
Although the partition of unity method could derive the globally continuous solution,the error estimates heavily depend on the usage of the superapproximation property of finite element spaces.As we known,the usage of this property causes the embarrassed problem that the distance between the boundaries of a specific subdomain and its expansion should be of constant order.Therefore the expansion of the subdomain could not be arbitrary small even when the diameter of the subdomain tends to zero.This will lead to a vast waste of parallel computing resources.In[15],we proposed an expandable local and parallel two-grid finite element scheme to overcome the dependence on superapproximation.The scale of each subproblem can be arbitrary small as H tends to zero and every two adjacent subproblems only have a small overlapping.Superposition principle is used to generate a series of local and independent subproblems and to make the global approximation continuous.In order to obtain an approximation with same accuracy as the fine mesh standard Galerkin approximation,a few iterations(O(|lnH|2)in 2-D or O(|lnH|)in 3-D respectively)are essential.
Following the idea in[15],two expandable two-grid parallel finite element methods are given to solve the linear elliptic problems.The first algorithm is one iterative form while the second method is one non-iterative form.As in[15],in order to derive optimal estimates,a few iterations(O(|lnH|2)in 2-D or O(|lnH|)in 3-D)are essential for the iterative method.However,for the non-iterative form,patches of diameter O(|lnH|2)H or O(|lnH|)H in 2-D or 3-D respectively are sufficient to guarantee the same accuracy as the fine mesh standard Galerkin approximation because errors decay exponentially with respect to the number of layers of elements in patches(see[11]for detail).Both the two algorithms can reach the same accuracy as the fine mesh standard Galerkin approximation in theoretical analysis and numerical simulation.
From the visual point of view,the non-iterative form has a similar approach except patch is a m-layer.But in practice,the non-iterative form needs only one global communication to derive the globally continuous approximation,while for the iterative form,in each iteration,one global communication is essential to reach the global approximation.That is the non-iterative form needs less communication than the iterative form.
The outline of this article is organized as follows.In Section 2,some preliminary materials and assumptions on mixed finite element spaces are provided.In Section 3,two expandable twogrid parallel finite element methods are presented.In Section 4,some a priori error estimation and optimal error bounds in both H1and L2-normal for the two algorithms are derived.In Section 5,some numerical experiments are reported to show the validity of our algorithms.Finally,a short conclusion is given.
2 Preliminaries
In this article,we consider the following linear elliptic equations with Dirichlet boundary condition defined in convex bounded domain Ω⊂Rd,d=2,3:
For a nonnegative integer s,we denote by Hs(Ω)the Sobolev space[1]in usual sense and their associated normswhile denote bythe closed subspace of H1(Ω)consisting of functions with zero trace on∂Ω.For convenience,the symbolsandwill be used in this article.Thatandmean thatandfor some constants C1,c2,c3,and C3independent of mesh size.For sub-domains S1⊂ S2⊂ Ω,we write S1⊂⊂ S2to mean that.
In the following,we denote by(·,·)the L2-inner product on Ω.Thus,Let us define a(·,·)as a(u,v)=(∇u,∇v)+(b ·∇u,v), ∀u,where(·,·)is the standard inner-product of L2(Ω).Then,the weak formulation of(2.1)reads: findsuch that
A sufficient and necessary condition for the well-posedness of(2.2)is that
The variational problem(2.2)has a unique solution(see,for ample,[5]).Assume that a(u,v)is continuous,that is,
and coercive,that is,
For a given bounded domain Ω⊂Rd,we assume thatis a regular triangulation of Ω.Here,is the mesh parameter.Associated with the mesh TH(Ω),letbe a C0- finite element space on Ω andwhere r≥1 is a positive integer,andis the space of polynomials of degree not greater than r defined on
For these finite element spaces and problem(2.1),we make the following assumptions.
A1 Interpolation.There is a finite element interpolation IHdefined on SH(Ω)such that for any0≤m≤s≤r+1,
A2 Inverse Inequality.For any w ∈ SH(Ω),
A3 Regularity.For any f ∈ Hr−1(Ω),the solution of
and its associated formal adjoint problem
satis fiy
Then,the standard Galerkin equation for solving(2.2)reads: findsuch that
For the standard Galerkin approximation uH,we have the following assumption:
which can be easily verified as long as u∈ Hr+1(Ω).
3 Numerical Algorithms
For each vertex xiof the coarse grid,let=supp φi=Di.We callthe patch of layer 0 defined on the ith vertex.Then,we can define the patch of layer m(m≥1,an integer)based on vertex i recursively.That is
and the vertices on the boundary are included.For a proper chosen m,we denotesee Figure 1.For fine mesh parameter h,we introduce following fine mesh finite element spacesandwhich have the same definitions as SH(Ω)andgiven in the previous section.
Figure 1 Patch of layer m(m=0,1,2),from left to right
Algorithm 1Iterative Form
1.Find a global coarse grid solutionsuch that
2.Find local fine grid correctionssuch that
Set
3.Do a global correction on the coarse gird: findsuch that
And the final approximate solution is defined as
In the later numerical tests,it is easy to find that errors of the expandable two-grid parallel finite element method decay exponentially with respect to the number of layers of elements in patches.Therefore,for a proper chosen m,which is relevant to coarse mesh size H,it is sufficient to guarantee the same accuracy as the fine mesh standard Galerkin approximation.Let us denote,then we derive the following non-iterative form algorithm.
Algorithm 2Non-iterative Form
1*.Find a global coarse grid solutionsuch that
2*.Find local fine grid correctionssuch that
Set
3*.Do a global correction on the coarse gird: findsuch that
And the final approximate solution is defined as
RemarkIt is obvious that all the subproblems in Step 2 and 2*are independent,once the global coarse grid solution uHis known and the scale of each subproblem in Step 2 and 2*can be arbitrary small as H tends to zero and every two adjacent subproblems only have a small overlapping.The layer m in Step 2*is relevant to coarse mesh H(see Lemma 4.2*for detail).And the final finite element solutions in both forms are globally continuous.
4 Theoretical Results
In this section,we will give the theoretical results for Algorithm 1 and Algorithm 2.Firstly,we give the error estimates of Algorithm 1.
By the idea of fictitious domain method(see[10]),we extend the local sub-problem(3.2)to Ω.Let us denote Γ = ∂Ω and.Then,there existssuch that the zero extension ofsatisfies
Denote
then the residual equation is
For the previously defined fine mesh Th(Ω)and the associated finite element spacethe Galerkin approximation for(4.2)reads:Findsuch that
By the superposition principle,(4.3)can be rewritten as follows:Findi=1,2,···,N,such that
If we set the local error and the global error of uH,hby
respectively,it is easy to obtain the following equations
and
For all points x ∈ Ω,it is clear that there exists a positive integer κ,which has nothing to do with N and x,such that each x belongs to κ differentat most.The following lemma can be found in[15].
Lemma 4.1The multiplier ξiin(4.1)satisfies
and
Noting that
Thus,we obtain
By(4.5),we give the estimate ofwhich plays a crucial role in the following section.
Lemma 4.2Let us set
where c>0 is a positive constant that does not depend on H,h.Then,there holds
ProofLet us denote
and a series of disjoint annular zones
It is obvious that
Let us define
Noting that
Here,we introduce a smooth functionsuch thatfor k≥1 and
Because of the estimation ofin[15],there holds
where βd(H)=H−1when d=3 and βd(H)=|lnH|when d=2.
By Young’s inequality,we get
or
where c>0 is a constant that does not depend on H,h,i,and k.
By repeating the last inequality,we have
Therefore,
This,together with(4.5),concludes the proof of Lemma 4.2.
Following the result in Lemma 4.2,we have to give some estimates ofto estimate
Lemma 4.3Suppose that the assumptions A1–A3 are valid.Then,for i=1,2,···,N,we have
ProofUsing coercive property and takingin(2.5),we can obtain
Using the continuity property of the bilinear form a(·,·),we have
Assume that A1–A2 hold and notice that φiis a linear function on eachandthen we can obtain
Adding the above two equations leads to
Now,we give the error estimations of Algorithm 1 in the following theorem.
Theorem 4.4Assume that assumptions A1,A2,A3,and(2.7)hold and u ∈ Hr+1(Ω).Then,
where αd>0 is defined in Lemma 4.2.
ProofAt the beginning,we introduce an H1-orthogonal projection PHfromonto:for givenfindsuch that
It is classical that
Hence,
On the other hand,the coarse mesh correction can be rewritten as
Combination of the above estimates yields
Finally,we have
and
Using the above error equation ofand by Lemmas 4.1–4.3,we obtain
Because of the triangle inequality,we can easily derive the first result.
The Aubin-Nitsche duality argument is necessary for the L2-error estimate.Suppose that A3 is valid,then forthere existssuch that
and
Consequently,
By combining triangle inequality,we finish the L2-error estimate.
As our algorithms could be seen as varied two-grid methods,therefore,we expect our methods can reach the same convergence order with the two-grid method,which we called optimal error.
From the above results,it is easy to observe that we can improve the convergence order of both H1and L2errors of the coarse mesh standard Galerkin approximation uHfor αdorder by one two-grid iteration,and this phenomenon suggests us to do the following two-grid iteration with
• (Step 0)Let k=0 and solve(3.1)to obtainand we set;
•(Step 1)Solve the equations in(3.2)withto get,which are denoted byThen,we deriveby(3.3);
if k+1>K,stop the iteration and denotewhich is the final approximation with optimal error.Otherwise,let k:=k+1 and goto(Step 1).
CorollaryAssume,the final approximationof scheme(Step 0)–(Step 2)has the following error estimates
Next,we give the the error estimations of Algorithm 2 in the same way.
Without distinction,we still use the same notions Γ = ∂Ω and Γi= ∂ωiΓ,and
the local error and the global error of uH,h,respectively.
It is obvious that Lemma 4.1 and Lemma 4.3 remain the same forms,while for Lemma 4.2,we do a little modification and get the following lemma.
Lemma 4.2*For a proper chosen m,
where c>0 is a positive constant that does not depend on H,h,ωi.We have
ProofIn the same way,we have
This,together with(4.5),concludes the proof of the lemma.
Theorem 4.5Assume that assumptions A1,A2,A3,and(2.7)hold and u ∈ Hr+1(Ω).Then
5 Numerical Experiments
In this section,we will report some numerical examples(2D and 3D)to complement the analysis results.In the 2D experiments,the domain Ω is the unit square Ω =(0,1)× (0,1)with a uniform triangulationIn the 3D experiments,the domain Ω is the unit cube Ω=(0,1)3with a uniform triangulationP1element is employed for the finite element discretization.And all the following numerical results are obtained by using the public domain software FreeFem++.
5.1 2D-Example
For both Algorithm 1 and Algorithm 2,to reach the H1accuracy,we should choose H and h such that h∼H2.With such configuration,we have
On the other hand,to reach the L2accuracy,we should choose H and h such that h2∼H3.In this case,
In the first experiment,we take b=(1.0,1.0)Tand consider the problem with the following analytic solution
Then,we can get f(x,y)in(2.1).
In the following Table 1 and Table 2,we give some numerical results according to the above configurations of H and h.For numerical experiments that the true solution u is known,we define the convergence order”ORDER1” with respect to the coarse mesh size H as
The symbol uappstands for certain approximation of u defined in the algorithms. “Iteration”stands for the number of iterations that are used for deriving the final approximation in Algorithm 1,and“m”stands for the patch of layer m that is necessary to obtain optimal error in Algorithm 2.
As seen from Table 1 and Table 2,both Algorithm 1 and Algorithm 2 reach almost the same accuracy as the fine mesh standard Galerkin approximation in H1-norm and L2-normal.For H1-normal,2 iterations are sufficient for Algorithm 1 and 2 patches of layer for Algorithm 2.Compared with the fine mesh standard Galerkin method,our algorithms can get better accuracy in L2-normal.
Table 1 H1-Error(h=H2)
Table 2 L2-Error(h=H32)
In Figure 2,we show the evolution of error in H1-normal with “Iteration” (patch of layer)for Algorithm 1(Algorithm 2).It is clear that the error of Algorithm 1(Algorithm 2)decays rapidly with respect to “Iteration” (patch of layer).
Figure 2 Left:evolution of error in H1-normal with “Iteration” for Algorithm 1;right:evolution of error in H1-normal with patch of layer for Algorithm 2
In the second example,we take b=(2x−ey,3y cos(πx))T,and f=70log((x+0.1)(sin(πy)+1))in(2.1).As the exact solution u is unknown,the convergence order of the approximate solution is calculated as
Here,uhis the standard Galerkin approximation in the fine mesh finite element spaceand the symbol uappstands for certain approximation of u defined in the proposed algorithms.It is generally known that the H1error estimate of the fine mesh standard Galerkin approximation admits the following estimation when h=H2
the “ORDER2(uapp)”calculated by the above formula equals to 2 means
therefore
Similarity,
The Table 3 and Table 4 report the numerical results of this test problem.It is clear that the errors obtained by the two algorithm are almost identical with each other and confirm the theoretical results.
Table 3 H1-Error(h=H2)
Table 4 L2-Error(h=H32)
5.2 3D-example
In this section,we will give two 3D examples.In these two examples,the domain Ω is the unit cube(0,1)3and b=(1,1,1).In the first 3-D example,we consider the test problem with the the following analytic solution
The numerical results are given in Tables 5 and 6.
Table 6 L2-Error(h=H32)
Table 7 H1-Error(h=H2)
Table 8 L2-Error(h=H32)
The second example of 3-D case is a test problem driven by the following free term
whose numerical results are given in Tables 7 and 8.
6 Conclusions
In this article,we have shown and analyzed two expandable two-grid parallel finite element methods for solving the linear elliptic problems.For Algorithm 1,a few iterations,sayor O(|lnH|)in 2-D or 3-D respectively,are essential to obtain optimal error;while for Algorithm 2,patches of diameter O(|lnH|2)H or O(|lnH|)H in 2-D or 3-D respectively are sufficient to guarantee to preserve the optimal convergence order.The numerical results and theoretical results keep consistent.Therefore,both the two algorithms can be regarded as flexible methods.
杂志排行
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