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Superconvergence of the local discontinuous Galerkin method for linear fourth-order time-dependent problems in one space dimension

XIONGMENG

Department of Mathematics, Harbin Institute of Technology, Harbin, Heilongjiang 150001, People’s Republic of China

Corresponding author: [email protected] CHI-WANGSHU

Division of Applied Mathematics, Brown University, Providence, RI 02912, USA [email protected]

AND

BOYINGWU

Department of Mathematics, Harbin Institute of Technology, Harbin, Heilongjiang 150001, People’s Republic of China

[email protected]

[Received on 2 April 2011; revised on 13 September 2011]

In this paper we investigate the superconvergence of local discontinuous Galerkin (LDG) methods for solving one-dimensional linear time-dependent fourth-order problems. We prove that the error between the LDG solution and a particular projection of the exact solution,e¯u, achieves

k+32

th-order supercon- vergence when polynomials of degreek(k1) are used. Numerical experiments withPkpolynomials, with 1k3, are displayed to demonstrate the theoretical results, which show that the errore¯uactually achieves(k+2)th-order superconvergence, indicating that the error bound fore¯uobtained in this paper is suboptimal. Initial boundary value problems, nonlinear equations and solutions having singularities, are numerically investigated to verify that the conclusions hold true for very general cases.

Keywords: local discontinuous Galerkin method; superconvergence; fourth-order problems; error estimates.

1. Introduction

In this paper we are interested in the superconvergence of local discontinuous Galerkin (LDG) methods for a class of one-dimensional linear fourth-order problems formulated as

ut+αux +βux x+ux x x x =0, (1.1)

whereαandβ are arbitrary constants. Note that, forβ > 0, there is an antidiffusion termβux x in the equation, which is, however, dominated by the higher-order diffusion termux x x x. The general problem (1.1) includes the following linear time-dependent biharmonic equation

ut+ux x x x =0, (1.2)

cThe author 2012. Published by Oxford University Press on behalf of the Institute of Mathematics and its Applications. All rights reserved.

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and the linearized Cahn–Hilliard equation

ut+ux x +ux x x x =0, (1.3)

as its special cases.

The discontinuous Galerkin (DG) method is a class of finite element methods using discontinuous piecewise polynomials as the solution and the test spaces. It was first introduced by Reed & Hill (1973) for solving a first-order steady-state linear conservation law and later developed by Cockburn et al.

(Cockburn & Shu, 1989, 1998b; Cockburn et al., 1989, 1990) for solving time-dependent nonlinear equations. Motivated by the successful numerical experiments of Bassi & Rebay (1997) for the com- pressible Navier–Stokes equations, the LDG methods were developed for solving nonlinear convection–

diffusion equations (Cockburn & Shu, 1998a) containing second-order spatial derivatives in which L2 stability and a suboptimalL2error estimates were obtained for linear equations with smooth solutions.

Later, the LDG methods were generalized to solve various partial differential equations (PDEs) involv- ing higher-order derivatives. For Korteweg-de Vries-type equations containing third-order derivatives, an LDG method was developed in Yan & Shu (2002a), where a suboptimal error estimate was proved for the linear case, and more recently, an optimalL2error estimate was obtained in Xu & Shu (in press).

In Yan & Shu (2002b), Xu & Shu (2004); Xu & Shu (2006) and Xiaet al.(2007), LDG techniques were developed for solving other types of high-order PDEs including the time-dependent biharmonic equa- tions, the fully nonlinear K(n,n,n)equations, the Kuramoto–Sivashinsky-type equations, the Cahn–

Hilliard-type equations and so on. In Dong & Shu (2009), optimal error estimates for the LDG method applied to the linear biharmonic equation and linearized Cahn–Hilliard-type equations were obtained in one dimension and in multidimensions for Cartesian and triangular meshes. For more details of the DG and LDG methods we refer to the lecture notes, Cockburn (1999), and review papers, Cockburn & Shu (2001); Xu & Shu (2010).

Apart from the LDG methods mentioned above, there are also other finite element methods in the lit- erature for solving fourth-order time-dependent problems. For example, Elliott & Zheng (1986) applied a conforming finite element method to the Cahn–Hilliard equation and obtained optimal error estimates inL2andLnorms provided the approximate solution is bounded inLand the polynomial degree k3. Feng & Prohl (2004) applied a mixed finite element method for solving Cahn–Hillard equations on quasiuniform triangular meshes and obtained an optimal error estimate under minimum regularity assumptions on the initial data and the domain.

Adjerid & Issaev (2005) and Adjerid & Klauser (2005) showed that the LDG solution is super- convergent at Radau points for solving convection- or diffusion-dominant time-dependent equations.

Based on Fourier analysis, Cheng & Shu (2008, 2009) proved superconvergence of the DG and LDG solutions towards a particular projection of the exact solution in the case of piecewise linear polyno- mials on uniform meshes for the linear conservation law and heat equation, respectively. The results were later improved, using a different technique, in Cheng & Shu (2010) for arbitrary nonuniform reg- ular meshes and schemes of any order. In this paper we follow the approach in Cheng & Shu (2010) to obtain the superconvergence property of the LDG method for a class of fourth-order problems. An important motivation for studying such superconvergence is to set a firm theoretical foundation for the excellent behaviour of DG and LDG methods for long-time simulations, which have been repeatedly observed by practitioners. Indeed, if superconvergence for the error between the DG or LDG solution and a particular projection of the exact solution of the order

k+32

, with linear growth in time, can be shown for polynomials of degreek, then the error between the numerical solution and the exact solution does not grow for a long timet =O 1

h

, wherehis the mesh size (Cheng & Shu, 2010). The gen- eralization from first- and second-order equations in Cheng & Shu (2010) to the fourth-order equation

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in this paper involves several technical difficulties, including the estimate of different combinations of the LDG solution and auxiliary variables that approximate derivatives of different orders, and the design and analysis of a special operator to guarantee the superconvergence property of the initial condition.

This paper is organized as follows. In Section 2 we define the LDG scheme for fourth-order time- dependent problems, state the main results and present the details of the proof of the superconvergence property. In Section 3 various numerical experiments, including linear equations, nonlinear equations, initial boundary value problems and solutions having singularities, are shown to demonstrate that the conclusions hold true for very general cases. Concluding remarks and comments on future work are given in Section 4. The proofs for some of the technical lemmas are collected in Appendix.

2. LDG scheme for fourth-order problems

We consider the following linear fourth-order equation

ut+αux+βux x +ux x x x =0 (2.1a)

with initial condition

u(x,0)=u0(x) (2.1b)

and periodic boundary conditions

u(0,t)=u(2π,t). (2.1c)

We would like to remark that the assumption of periodic boundary conditions is for simplicity only and not essential: see Cheng & Shu (2010) for discussion related to initial boundary value problems for conservation laws.

2.1 The LDG scheme

We assume the following mesh to cover the computational domain I = [0,2π], consisting of cells Ij =

xj1 2,xj+1

2

, for 1 j N, where 0=x1

2 <x3

2 <· · ·<xN+1

2 =2π.

The cell centre is denoted byxj = xj1

2+xj+1 2

2. We also sethj =xj+1 2xj1

2 andh=maxjhj. We denote by(vh)j+1

2

and(vh)+j+1 2

the values ofvh at the discontinuity pointxj+1

2 from the left cell, Ij, and from the right cell, Ij+1, respectively. The following piecewise polynomial space is chosen as the finite element space:

Vhk= {v:v|IjPk(Ij),j =1, . . . ,N},

wherePk(Ij)denotes the set of polynomials of degree up tokdefined on the cellIj. Note that functions inVhk are allowed to have discontinuities across element interfaces.

In order to construct the LDG scheme, firstly, we introduce some auxiliary variables approximating various order derivatives of the solution and rewrite equation (2.1a) as a first-order system,

ut+(αu+βq+r)x =0, rpx =0, pqx =0, qux =0.

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Then, the semidiscrete LDG scheme is defined as follows: finduh,qh,ph,rhVhk, such that

Ij

(uh)tρdx−

Ij

αuhρxdx+αu˜hρ|j+1

2 −αu˜hρ+|j1

2

Ij

βqhρxdx

qˆhρ|j+1

2 −βqˆhρ+|j1

2

Ij

rhρxdx+ ˆrhρ|j+1

2 − ˆrhρ+|j1

2 =0, (2.2a)

Ij

rhηdx+

Ij

phηxdx− ˆphη|j+1

2 + ˆphη+|j1

2 =0, (2.2b)

Ij

phξdx+

Ij

qhξxdx− ˆqhξ|j+1

2 + ˆqhξ+|j1

2 =0, (2.2c)

Ij

qhψdx+

Ij

uhψxdx− ˆuhψ|j+1

2 + ˆuhψ+|j1

2 =0 (2.2d) hold for anyρ, ψ, ξ, η∈Vhk,whereu˜his the upwind flux depending on the sign ofα. Without loss of generality we assume thatα0 and takeu˜h=uh and then choose alternating fluxes for the diffusion terms as follows:

ˆ

uh=uh, qˆh=qh+, pˆh =ph, rˆh=rh+. (2.3) 2.2 Notation and auxiliary results

To prove superconvergence of the LDG method, we would like to introduce the following notation, definitions and useful lemmas.

2.2.1 Notation for the DG discretization. First, we use [ξ] = ξ+−ξto denote the jump in the functionξat each cell boundary point. For the linear problems discussed in this paper, we introduce the DG discretization operatorDas in Xu & Shu (in press): for each cellIj =

xj1 2,xj+1

2

,

DIj(ξ, η; ˆξ)= −

Ijξηxdx+ ˆξη|j+1

2 − ˆξη+|j1

2. We also use the notation

D(ξ, η; ˆξ)=

j

DIj(ξ, η; ˆξ).

Using the definition of this operator, we have the following lemmas, whose proof is straightforward (see Xu & Shu, in press and also Zhang & Shu, 2010).

LEMMA2.1 (Xu & Shu, in press) Choosing different numerical fluxes the DG discretization operator satisfies the equalities

D(ξ, η;ξ)+D(η, ξ;η+)=0, (2.4a)

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D(ξ, η;ξ+)+D(η, ξ;η)=0, (2.4b) D(ξ, η;ξ+)+D(η, ξ;η+)= −

j

[ξ]j+1

2[η]j+1

2, (2.4c)

D(ξ, η;ξ)+D(η, ξ;η)=

j

[ξ]j+1 2[η]j+1

2, (2.4d)

D(ξ, ξ;ξ)=1 2

j

[ξ]2j+1

2, (2.4e)

D(ξ, ξ;ξ+)= −1 2

j

[ξ]2

j+12. (2.4f)

LEMMA2.2 By integration by parts we also have DIj(ξ, η;ξ)=

Ij

ξxηdx+[ξ]η+|j1

2, (2.5)

DIj(ξ, η;ξ+)=

Ijξxηdx+[ξ]η|j+1

2. (2.6)

2.2.2 Projections and interpolation properties. In what follows we define two special projections, Ph± into Vhk, which are commonly used in the analysis of DG methods. For any given functionuH1(I)and arbitrary subinterval Ij =

xj1 2,xj+1

2

,the special projections ofu, denoted by Ph+uand Phu, are the unique functions in the finite element spaceVhksatisfying, for each j,

Ij

(Ph+u(x)−u(x))ρ(x)dx=0 ∀ρ∈ Pk1(Ij), (Ph+u)+j1 2

=u xj1

2

, (2.7)

Ij

(Phu(x)−u(x))ρ(x)dx=0 ∀ρ∈ Pk1(Ij), (Phu)j+1 2

=u xj+1

2

. (2.8)

For the special projections mentioned above, we have, by the standard approximation theory (Ciarlet, 1978), that

Ph±u(·)u(·)L2 C hk+1, (2.9)

where both here and belowCis a positive constant (which may have a different value at each occurrence) depending solely onu and its derivatives but independent ofh.In particular, in equation (2.9),C = Cuk+1, whereuk+1is the standard Sobolev(k+1)norm andC is a positive constant independent ofu.

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In the proof of the error estimates the following inverse properties are needed: for anyvhVhkthere exists a positive constantCindependent ofh, such that

vhΓ C h12vhL2, (2.10)

xvhL2 C h1vhL2, (2.11)

wherevhΓ is the usualL2norm on the cell interfaces of the mesh.

2.2.3 Functionals related to the L2norm. To get the superconvergence property of the method two functionals related to theL2norm of a function onIj are needed as defined in Cheng & Shu (2010):

Bj(f)=

Ij

f(x)xxj1 2

hj

d

dx f(x)xxj

hj

dx,

B+j(f)=

Ij

f(x)xxj+1 2

hj

d

dx f(x)xxj

hj

dx.

The functionals defined above have the following properties, which are essential to the proof of super- convergence.

LEMMA2.3 (Cheng & Shu, 2010) For any function f(x)∈C1onIj we have Bj (f)= 1

4hj

Ij

f2(x)dx+ f2(xj+1

2)

4 , (2.12)

B+j (f)= − 1 4hj

Ij

f2(x)dx− f2(xj1

2)

4 . (2.13)

The proof of this lemma is straightforward; see Cheng & Shu (2010).

2.2.4 Initial condition. To obtain the superconvergence property of the method, the initial condition of the numerical scheme should be chosen carefully to be compatible with the superconvergence error estimate. To this end we define an operator Ph as follows: for any functionu, then PhuVhk, and supposeqh,ph,rhVhkare the unique solutions (with given Phu) to

Ij

rhηdx+

Ij

phηxdx−phη|j+1

2 +phη+|j1

2 =0, (2.14a)

Ij

phξdx+

Ij

qhξxdx−qh+ξ|j+1

2 +q+hξ+|j1

2 =0, (2.14b)

Ij

qhψdx+

Ij

Phxdx−(Phu)ψ|j+1

2 +(Phu)ψ+|j1

2 =0, (2.14c)

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for anyψ, ξ, η∈Vhk, then we require

Ij((PhuPhu)−(Ph+qqh)+(Ph+rrh))ρdx=0 (2.15) for anyρ∈ Pk1onIj and

(PhuPhu)=(Ph+qqh)+−(Ph+rrh)+ atxj1

2. (2.16)

For the regular mesh considered in this paper we denoteλ=maxjhj/minjhj, which is a constant during mesh refinements. As to the operator defined above we have the following lemma.

LEMMA2.4 Phuexists and is unique. Moreover, there holds the error estimate

PhuPhuL2 C(λ,uk+4)hk+3/2. (2.17) The proof of this lemma is given in Appendix.

We would like to remark that the purpose for introducing the operator Phis only theoretical: it is needed for the technical proof of superconvergence. In actual numerical computation we have observed that we can use the usualL2projection ofuas the initial condition and still observe superconvergence;

see the numerical experiments in Section 3. Of course, if the standard L2 projection is used for the initial condition, then the superconvergence result does not hold att =0 nor for smallt. For later time the dissipativity in the PDE and the numerical scheme seems to help to recover the superconvergent performance.

2.3 Main results

Before we state the main results we would like to introduce the following notation:

eu=uuh=(u−Phu)+(Phuuh)=εu+ ¯eu, eq=qqh=(q−Ph+q)+(Ph+qqh)=εq+ ¯eq, ep= pph=(pPhp)+(Phpph)=εp+ ¯ep,

er =rrh=(r−Ph+r)+(Ph+rrh)=εr + ¯er. For the caseα0 we have the following error estimates.

THEOREM2.5 Letu,p=ux xbe the exact solution of the fourth-order problem (2.1), which is assumed to be sufficiently smooth, i.e.uk+4,utk+4,uttk+4andutttk+1are bounded uniformly for any time t ∈ [0, T]. Let uh, ph be the LDG solution of equation (2.2) when the diffusion alternating fluxes (2.3) are used. We choose the initial condition asuh(·,0)= Phu0. For regular triangulations of I = [0,2π], if the finite element space Vhk withk 1 is used, then there holds the following error estimate:

¯eu(·,t)2L2 + t

0 ¯ep(·,t)2L2dt Ce2C1th2k+3, (2.18)

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and, in particular,

¯eu(·,t)L2 CeC1thk+3/2,

whereC =C(α, β, λ,uk+4,utk+4,uttk+4,utttk+1)and both here and belowC1=C1(α, β)

0.

REMARK2.6 For the caseα0 we can chooseu˜h=u+h and take the diffusion alternating fluxes as ˆ

uh=u+h, qˆh=qh, pˆh =p+h, rˆh=rh. (2.19) Theorem 2.5 still holds in this case with the obvious change of the projections.

For the caseα=β =0 equation (2.1a) reduces to the biharmonic equation (1.2), and we have the following result.

THEOREM2.7 Letu, p = ux x be the exact solution of the fourth-order problem (1.2), which is as- sumed to be sufficiently smooth, i.e.uk+4,utk+4,uttk+4andutttk+1are bounded uniformly for any timet ∈ [0, T]. Letuh, ph be the LDG solution of equation (2.2) whenα=β =0 and dif- fusion alternating fluxes (2.3) are used. We choose the initial condition asuh(·,0)=Phu0. For regular triangulations of I = [0,2π], if the finite element spaceVhk withk 1 is used, then there holds the following error estimate:

¯eu(·,t)2L2+ t

0 ¯ep(·,t)2L2etC(1+t)2h2k+3, and, in particular,

¯eu(·,t)L2 C(1+t)hk+3/2, whereC =C(λ,uk+4,utk+4,uttk+4,utttk+1).

The proof of this theorem is similar to that for the previous theorem, except that we need to carefully evaluate and estimate several terms to obtain a linear growth bound without employing Gronwall’s inequality. The detailed proof is given in Appendix.

The case with the fluxes (2.19) is the same with the obvious change of the projections.

Note that, for the general cases including the antidiffusive caseβ >0, the exponential growth of the constant with respect to time in Theorem 2.5 is expected, as the exact solution may have such growth in time for small wave numbers.

2.4 Proof of Theorem2.5

By using the DG discretization operator, the LDG scheme (2.2) with the fluxes (2.3) can be written as

Ij

(uh)tρdx+αDIj(uh, ρ;uh)+βDIj(qh, ρ;qh+)+DIj(rh, ρ;rh+)=0, (2.20a)

Ij

rhηdx−DIj(ph, η; ph)=0, (2.20b)

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Ij

phξdx−DIj(qh, ξ;qh+)=0, (2.20c)

Ij

qhψdx−DIj(uh, ψ;uh)=0, (2.20d)

for anyρ, ψ, ξ, η∈Vhk.Since the exact solutionsu,q=ux,p=ux x,r =ux x xalso satisfy the scheme (2.2), we have therefore the error equations

Ij(eu)tρdx+αDIj(eu, ρ;eu)+βDIj(eq, ρ;eq+)+DIj(er, ρ;e+r )=0,

Ij

erηdx−DIj(ep, η;ep)=0,

Ij

epξdx−DIj(eq, ξ;e+q)=0,

Ij

eqψdx−DIj(eu, ψ;eu)=0,

which, by the properties of the projectionsPhandPh+, given in equations (2.7) and (2.8), is

Ij

(eu)tρdx+αDIjeu, ρ; ¯eu)+βDIjeq, ρ; ¯eq+)+DIjer, ρ; ¯e+r )=0, (2.21a)

Ij

erηdx−DIjep, η; ¯ep)=0, (2.21b)

Ij

epξdx−DIjeq, ξ; ¯e+q)=0, (2.21c)

Ij

eqψdx−DIjeu, ψ; ¯eu)=0, (2.21d)

for anyρ, ψ, ξ, η∈Vhk.Taking(ρ, ψ, ξ, η)=(¯eu,−¯er,e¯p,e¯q)in equation (2.21), adding them up and summing over all j, we obtain

I

eu)te¯udx+

I

¯ e2pdx+

I

u)te¯udx+

I

εpe¯pdx+

I

εre¯qdx−

I

εqe¯rdx+αD(¯eu,e¯u; ¯eu)

+βD(¯eq,e¯u; ¯eq+)+D(¯er,e¯u; ¯e+r )+D(¯eu,e¯r; ¯eu)−D(¯eq,e¯p; ¯e+q)−D(¯ep,e¯q; ¯ep)=0.

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Using the property of the operatorDin Lemma 2.1 we thus have

I

(e¯u)te¯udx+

I

¯ e2pdx+

I

u)te¯udx+

I

εpe¯pdx

+

I

εre¯qdx−

I

εqe¯rdx+α 2

j

[e¯u]2

j+12 +βD(¯eq,e¯u; ¯eq+)=0. (2.22) By takingξ = ¯euin equation (2.21c) and summing over all jwe get

D(¯eq,e¯u; ¯eq+)=

I

epe¯udx. (2.23)

Combining equations (2.22) and (2.23) we arrive at 1

2 d

dt¯eu2L2ep2L2

Iu)te¯udx−

Iεpe¯pdx−

Iεre¯qdx+

Iεqe¯rdx−β

I

epe¯udx. (2.24) It follows from the Cauchy–Schwarz inequality that

1 2

d

dt¯eu2L2 +1

ep2L2

I

u)te¯udx +

I

εpe¯pdx +

I

εre¯qdx +

I

εqe¯rdx + |β|

I

εpe¯udx +β2

2 ¯eu2L2. (2.25) On the other hand, using Lemma 2.2, equation (2.21) can be rewritten as

Ij

(eu)tρdx+αDIjeu, ρ; ¯eu)+

Ij

(e¯re¯q)xρdx+[¯ere¯q|j+1

2 =0, (2.26a)

Ij

erηdx−

Ij

ep)xηdx−[e¯p+|j1

2 =0, (2.26b)

Ij

epξdx−

Ij

(e¯q)xξdx−[e¯q|j+1

2 =0, (2.26c)

Ij

eqψdx−

Ij

eu)xψdx−[¯eu+|j1

2 =0. (2.26d) Denote

¯

eu=rj +dj(x)(x−xj)/hj, e¯q=bj+sj(x)(x−xj)/hj,

¯

ep=vj+wj(x)(x−xj)/hj, e¯r =lj +gj(x)(x−xj)/hj,

where rj,bj, vj,lj are constants and dj(x),sj(x), wj(x),gj(x) ∈ Pk1. First, taking ψ = dj(x) (xxj1

2)/hj in equation (2.26d), and using the definition ofBj, we have

Ij

eqdj(x)(x−xj1

2)/hjdx−Bj(dj)=0.

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By the property ofBj in Lemma 2.3 we obtain

Ij

d2j(x)dx 4

Ij

eqdj(x)(x−xj1 2)dx.

Defining piecewise polynomialsd(x)andφ1(x), such thatd(x)=dj(x)andφ1(x)=xxj1 2 onIj, and summing the above inequality over j, we get

dL2 4eqL2φ1L 4heqL2, (2.27) where we have used the fact thatφ1L =h.Similarly, takingξ =sj(x)(x−xj+1

2)/hj in equation (2.26c),η=wj(x)(x−xj1

2)/hj in equation (2.26b) and using the definition ofBj andB+j, we have

Ij

erwj(x)(x−xj1

2)/hjdx−Bj(wj)=0,

Ij

epsj(x)(x−xj+1

2)/hjdx−B+j (sj)=0.

By the properties ofBj andB+j in Lemma 2.3 we obtain

Ij

w2j(x)dx 4

Ij

erwj(x)(x−xj1 2)dx,

Ij

s2j(x)dx −4

Ij

epsj(x)(x−xj+1

2)dx.

Defining piecewise polynomialsw(x),s(x)andφ2(x), such that w(x) = wj(x),s(x) = sj(x)and φ2(x)=xxj+1

2 onIj, and summing the above inequality over j, we get

wL2 4erL2φ1L4herL2, (2.28) sL2 4epL2φ2L4hepL2, (2.29) where we have used the fact that φ1L = φ2L = h. Then, letting ρ = (gj(x)+βsj(x)) (xxj+1

2)/hj in equation (2.26a), we have

Ij

(eu)tρdx−α

Ij

¯

euρxdx+ ¯euρ+|j1

2

+

Ij

(e¯re¯q)xρdx =0,

which can be written as

Ij

(eu)t(gj(x)+βsj(x))(x−xj+1

2)/hjdx−αR1j +R2j =0,

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where

R1j =

Ije¯u((gj(x)+βsj(x))(xxj+1

2)/hj)xdx

rj1+1 2dj1

xj1

2

× gj

xj1

2

+βsj

xj1

2

=

Ij

dj(x)xxj

hj ((gj(x)+βsj(x))(x−xj+1

2)/hj)xdx +

rjrj1−1 2dj1

xj1

2 gj

xj1

2

+βsj

xj1

2

and

R2j =B+j (gjsj)= − 1 4hj

Ij

(gj(x)+βsj(x))2dx−1 4

gj

xj1

2

+βsj

xj1

2

2

.

Therefore,

Ij

(gj(x)+βsj(x))2dx4

Ij

(eu)t(gj(x)+βsj(x))(x−xj+1

2)dx−4αhjR1j. Summing the above inequality over all jwe arrive at

gs2L2 4(eu)tL2gsL2φ2L+4α

j

hjR1j

. (2.30)

Takingψ=1 in equation (2.26d) we get rjrj1−1

2dj1

xj1

2

=

Ij

eqdx−1 2dj

xj+1

2

.

So, the termhjR1j can be formulated as hjR1j =

Ij

dj(x)(x−xj)(gj(x)+βsj(x))/hjdx +

Ij

dj(x)(x−xj)(gj(x)+βsj(x))(x−xj+1

2)/hjdx +hj

Ij

eqdx−1 2dj

xj+1

2 gj

xj1

2

sj

xj1

2

.

By the inverse properties (2.10) and (2.11) we have the estimate

j

hjR1j

C(k)g+βsL2(dL2+heqL2), (2.31)

at Brown University on October 16, 2012http://imajna.oxfordjournals.org/Downloaded from

(13)

wherekis the degree of polynomials in the finite element spaceVhk. Combining equations (2.27), (2.30) and (2.31) together and recalling thatφ2L = x−xj+1

2L=h, we conclude that

g+βsL2 C(α,k)h((eu)tL2+ eqL2). (2.32) Thus,

gL2 g+βsL2 + |β|sL2 C(α, β,k)h((eu)tL2+ eqL2+ epL2). (2.33) Now, we return to the error equation (2.25). Note that(εu)t, εq, εpandεr are orthogonal to any piece- wise constant functions, then

I

u)te¯udx =

j

Ij

u)tdj(x)(x−xj)/hjdx

u)tL2dL2φL,

I

εpe¯pdx =

j

Ij

εpwj(x)(x−xj)/hjdx

εpL2wL2φL,

Iεre¯qdx =

j

Ijεrsj(x)(xxj)/hjdx

εrL2sL2φL,

I

εqe¯rdx =

j

Ij

εqgj(x)(x−xj)/hjdx

εqL2gL2φL,

I

εpe¯udx =

j

Ij

εpdj(x)(x−xj)/hjdx

εpL2dL2φL, whereφ=(x−xj)/hj. Then, equation (2.25) becomes

1 2

d

dt¯eu2L2 +1

ep2L2 φL

u)tL2dL2+ εpL2wL2+ εrL2sL2

+ εqL2gL2+ |β|εpL2dL2

2 2 ¯eu2L2. Using the approximation property of the projections (2.9) and the fact thatφL = 12, we get

1 2

d

dt¯eu2L2 +1

ep2L2 C hk+1(dL2 + sL2+ wL2+ gL2)+β2

2 ¯eu2L2, (2.34) where C = C(β,uk+4,utk+1). Substituting equations (2.27), (2.28), (2.29) and (2.33) into equation (2.34), we obtain

1 2

d

dt¯eu2L2 +1

ep2L2 C hk+2((eu)tL2+ eqL2+ epL2 + erL2)+β2

2 ¯eu2L2, (2.35)

at Brown University on October 16, 2012http://imajna.oxfordjournals.org/Downloaded from

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