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1 GAKUTO International Series Mathematical Sciences and Applications, Vol.28(2008) Proceedings of Fourth JSIAM-SIMMAI Seminar on Industrial and Applied Mathematics, pp A COMPUTATIONAL APPROACH TO CONSTRUCTIVE A PRIORI AND A POSTERIORI ERROR ESTIMATES FOR FINITE ELEMENT APPROXIMATIONS OF BI-HARMONIC PROBLEMS Mitsuhiro T. Nakao Faculty of Mathematics, Kyushu University Hakozaki, Fukuoka, Japan (mtnakao@math.kyushu-u.ac.jp) Kouji Hashimoto Graduate School of Informatics, Kyoto University Yoshida, Kyoto, Japan (hashimot@amp.i.kyoto-u.ac.jp) Kaori Nagatou Faculty of Mathematics, Kyushu University Hakozaki, Fukuoka, Japan (nagatou@math.kyushu-u.ac.jp) Abstract. In the numerical verification method of solutions for nonlinear fourth order elliptic equations, it is important to find a constant in the constructive a priori and a posteriori error estimates for the finite element approximation of bi-harmonic problems. We show these procedures by verified computational techniques using the Hermite spline functions for two dimensional rectangular domain. Several numerical examples which confirm the actual effectiveness of the method are presented. - AMS Subject Classification 65N15, 65N30 139

2 1 Introduction In this paper, we consider the guaranteed error bounds of the finite element approximations for the following equation: 2 u = f in Ω, u = n u = 0 on Ω, (1.1) where f L 2 (Ω) with a rectangular domain Ω in R 2, and n u denotes the outer normal derivative of u. 1.1 Notations In the below, setting Ω := (0, 1) 2 for simplicity, we denote the L 2 inner product on Ω by (, ) L 2 and the norm by L 2. We also denote the usual k-th order L 2 Sobolev space on Ω by H k (Ω) for any positive integer k as well as the space H 2 0(Ω) by H 2 0(Ω) := { v H 2 (Ω) : v = n v = 0 on Ω }. Let S h H 2 0(Ω), n dims h, be a finite element space, under some rectangular mesh, which is spanned by two dimensional Hermite spline functions {φ i } 1 i n with homogeneous boundary conditions in H 2 0 sense [4]. Moreover, we define the space S h, n dims h, which is spanned by the basis {φ i } 1 i n, as the finite element subspace of H 2 (Ω), not of H 2 0(Ω), satisfying S h S h but S h S h (n < n ). Namely, the set of base functions {φ i } 1 i n consists of the elements in {φ i } 1 i n and the Hermite spline functions corresponding to the boundary nodes(cf. [5]). Next, we define the H 2 0-projection P h : H 2 0(Ω) S h of v H 2 0(Ω) by ( v P h v, φ h ) L 2 = 0, φ h S h. Moreover, we also define the L 2 -projection P 0 : L 2 (Ω) S h of v L2 (Ω) by (v P 0 v, φ h) L 2 = 0, φ h S h. Let Sh x and Sy h denote the set of one dimensional Hermite spline functions on (0, 1) with homogeneous H0 2 boundary conditions in x and y directions, respectively. Then, S h is represented as the tensor product Sh x Sy h. Similarly, we have S h = Sx h Sy h, where Sh x, Sy h are spaces of one dimensional spline functions without boundary functions. In what follows, a parameter h stands for the maximum mesh size of the partition of the interval (0, 1). In the x-direction, for w H0(0, 2 1) and w L 2 (0, 1), we also define the projections P2 x : H0(0, 2 1) Sh x and P 0 x : L 2 (0, 1) Sh x by respectively. For P y 2 (D 2 xw D 2 xp x 2 w, D 2 xϕ h ) L 2 = 0, ϕ h S x h, and (w P x 0 w, ϕ h) L 2 = 0, ϕ h Sx h, and P y 0, analogously defined in the y-direction. 140

3 1.2 Motivation Let u h S h be an approximate solution of (1.1) satisfying ( u h, φ h ) L 2 = (f, φ h ) L 2 φ h S h. Then, note that we have u h = P h u by the definition and that the solution u of (1.1) belongs to H 2 0(Ω) H 4 (Ω)([1]). Therefore, in what follows, we will discuss on the error estimates for the projection operator P h. We now assume the following a priori error estimates. Assumption 1 For an arbitrary v H 2 0(Ω) H 4 (Ω), there exists a constant C 0 such that v P h v L 2 C 0 h 2 2 v L 2. Our main purpose of this paper is to find an a priori constant C 0 in the assumption 1 by using guaranteed numerical computations on computer. And as a bi-product of the arguments, we also show a method to get an a posteriori error bound for the approximate solution of the equation (1.1). In the numerical verification method of solutions for two dimensional Navier-Stokes problems(e.g., [2]), we need to enclose a solution of bi-harmonic equations with guaranteed error bounds. In such a situation, the above constant and a posteriori error estimates for the finite element approximation play an essential and important role. The basic techniques used in the below are extension of the method in [5] or [3] to the bi-harmonic problem. 1.3 Preliminary results We first introduce the following known results. Lemma 1 [4] For an arbitrary ψ H 2 0(Ω) H 4 (Ω), it follows that D 2 xψ D 2 xp x 2 ψ L 2 Ch 2 D 4 xψ L 2, (1.2) where the constant C can be taken as C = 1/π 2. Moreover, the estimate (1.2) is equivalent to the following inequality: ψ P x 2 ψ L 2 Ch 2 D 2 xψ D 2 xp x 2 ψ L 2. We now show the following inverse inequality for later use. Lemma 2 For ψ h S h, it follows that where κ = < D 2 xψ h L 2 κ h 2 ψ h L 2, 141

4 Proof : Note that it is sufficient to prove the concerning inequality only for one dimensional polynomial of degree 3 on the interval [0, h]. In [4], base functions for x- direction on [0, h] are given by ϕ 1 (x) = (x h) 2 (2x + h)/h 3, ϕ 2 (x) = x 2 (3h 2x)/h 3, ϕ 3 (x) = x(x h) 2 /h 2, ϕ 4 (x) = x 2 (x h)/h 2, for x [0, h]. Hence, setting ϕ h := a 1 ϕ 1 (x) + a 2 ϕ 2 (x) + a 3 ϕ 3 (x) + a 4 ϕ 4 (x) and using some guaranteed computations of eigenvalue bounds of a matrix, we obtain = 840 h 4 D 2 xϕ h 2 L 2 (0,h) 8400 h 4, ϕ h 2 L 2 (0,h) at a at a where a = (a 1, a 2, a 3 h, a 4 h) T. Here, in order to get the above bound, we used a direct calculation of the matrix eigenvalue. That is, denoting the first and the second matrices in the above by A and B, respectively, let B = D T D a Cholesky decomposition of B. Then, it is readily seen that the maximum eigenvalue of the symmetric matrix D T AD 1 presents a desired bound. By using a computer algebra system, we confirmed that it is equal to 10. Thus, we can take κ as κ = 8400 = Main Results In this section, we show the constructive a priori and a posteriori error estimations for approximate solutions of the equation (1.1), which are equivalent to the same error estimates for H 2 0-projection of the exact solution. Let define v h := P h v n n v i φ i S h and v h := P 0 v h a i φ i Sh, i=1 i=1 for an arbitrary v H 2 0(Ω) H 4 (Ω). Then, v h satisfies ( v h, φ h) L 2 = ( v h, φ h) L 2, = ( v h, φ h) L 2, φ h S h. (2.1) 142

5 And, for g 2 v L 2 (Ω), we set g h n g i φ i S h, i=1 so that (g h, φ h ) L 2 = (g, φ h ) L 2, φ h S h. (2.2) Moreover, we denote some matrices and vectors as A = (A ij) = ( φ j, φ i ) L 2 R n n, A = (A ij ) = ( φ j, φ i ) L 2 R n n, L = (L ij) = (φ j, φ i ) L 2 R n n, L = (L ij ) = (φ j, φ i ) L 2 R n n, M = (M ij ) = ( φ j, φ i ) L 2 R n n, N = (N ij ) = ( φ j, φ i ) L 2 R n n. and a = (a 1, a n ) T R n, v = (v 1, v n ) T, g = (g 1, g n ) T R n. Notice that g 2 L 2 = g h 2 L 2 + g g h 2 L 2. And, when we define the matrix Q R n n such that L = QQ T, it follows that Q T g E = g h L 2, where E means the Euclidean norm in R n. Under the above notations, the functions v h and v h are determined by solving the following matrix equations: A v = L g, and L a = M v, respectively. Then, we have the following estimates. Lemma 3 It follows that v h v h L 2 X g h L 2, g h v h L 2 Y g h L 2, where X Q 1 XQ T 1/2 E, Y Q 1 Y Q T 1/2 E. Here, setting Z L 1 MA 1 L, X LA 1 L Z T L Z, Y L NZ Z T N T + Z T A Z. Proof : First, for the estimate v h v h L 2, we have v h v h 2 L 2 = v h 2 L 2 v h 2 L 2 = v T A v a T L a = v T A v v T M T L 1 M v = g T (LA 1 L LA 1 M T L 1 MA 1 L) g. 143

6 Next, for the estimate g h v h L 2, it follows that g h v h 2 L 2 = (g h, g h ) L 2 (g h, v h ) L 2 ( v h, g h ) L 2 + ( v h, v h ) L 2 = (g h, g h ) L 2 + ( g h, v h ) L 2 + ( v h, g h ) L 2 + ( v h, v h ) L 2 = g T L g + g T N a + a T N T g + a T A a = g T L g g T NL 1 M v v T M T L 1 N T g + a T M T L 1 A L 1 M v = g T (L NL 1 MA 1 L LA 1 M T L 1 N T + LA 1 M T L 1 A L 1 MA 1 L) g. Thus by the above definitions of matrices X, Y and Z, we have v h v h 2 L 2 = gt X g, g h v h 2 L 2 = gt Y g, which prove the lemma taking account that Q T g E = g h L 2. Lemma 4 For an arbitrary ψ H 2 0(Ω), it follows that ψ P x 0 P y 0 ψ L 2 K ψ L 2, where K = ( (Cκ + 1) 2) 1/2, the constants C and κ are the same as in Lemma 1 and 2, respectively. Proof : From the lemma 1 and 2, it follows that Dx(ψ 2 P2 x ψ) Dx(P 2 0 x ψ P0 x P2 x ψ) L 2 Dx(ψ 2 P2 x ψ) L 2 + Dx( 2 P0 x (ψ P0 x P2 x ψ) ) L 2 Dxψ 2 L 2 + κ h P x 2 0 (ψ P2 x ψ) L 2 Dxψ 2 L 2 + κ h ψ P x 2 2 ψ L 2 Dxψ 2 L 2 + Ch 2 κ h 2 D2 xψ L 2 (Cκ + 1) Dxψ 2 L 2. Thus, we have D 2 x(ψ P x 0 P y 0 ψ) 2 L 2 = D2 x(ψ P y 0 ψ) + D 2 x(p y 0 ψ P y 0 P x 0 ψ) 2 L 2 = D 2 x(ψ P y 0 ψ) 2 L 2 + D2 x( P y 0 (ψ P x 0 ψ) ) 2 L 2 D 2 xψ 2 L 2 + D2 x(ψ P x 0 ψ) 2 L 2 D 2 xψ 2 L 2 + D2 x(ψ P x 2 ψ) D 2 x(p x 0 ψ P x 0 P x 2 ψ) 2 L 2 ( 1 + (Cκ + 1) 2) D 2 xψ 2 L 2, where we have used the result just above to obtain the last right-hand side. Similarly, it follows that D 2 yψ D 2 yp x 0 P y 0 ψ L 2 ( 1 + (Cκ + 1) 2) 1/2 D 2 y ψ L

7 Hence, we have the following estimation: ψ P0 x P y 0 ψ L 2 Dx(ψ 2 P0 x P y 0 ψ) L 2 + Dy(ψ 2 P0 x P y 0 ψ) L 2 ( 1 + ( C 2 κ + 1 ) ) 2 1/2 ( D 2 x ψ L 2 + Dyψ 2 L 2) ( (Cκ + 1) 2) 1/2 ( D 2 x ψ 2 L 2 + D2 yψ 2 L 2 ) 1/2 ( (Cκ + 1) 2) 1/2 ψ L 2, where, in order to derive the last inequality, we have used the well known equality ψ 2 L 2 = D 2 xψ 2 L 2 + D 2 yψ 2 L D xy ψ 2 L 2 for any ψ H 2 0(Ω) on an arbitrary domain Ω. Therefore, we obtain the constant K as in the lemma. Lemma 5 For an arbitrary ψ H 2 0(Ω), it follows that ψ P x 0 P y 0 ψ L 2 Ch 2 ψ L 2, where the constant C is the same as in Lemma 1. Proof : From the lemma 1, it follows that ψ P0 x P y 0 ψ 2 L 2 = ψ P 0 x ψ + P0 x ψ P0 x P y 0 ψ 2 L 2 = ψ P0 x ψ 2 L + P x 2 0 (ψ P y 0 ψ) 2 L 2 ψ P0 x ψ 2 L + ψ P y 2 0 ψ 2 L 2 ψ P2 x ψ 2 L + ψ P y 2 2 ψ 2 L 2 C 2 h 4 Dxψ 2 2 L + 2 C2 h 4 Dyψ 2 2 L 2 C 2 h 4 ψ 2 L 2, which completes the proof. Now, we show the following two main results of this paper. Theorem 1 (constructive a priori error estimates) The constant C 0 in Assumption 1 can be taken as C 0 = C [ (KX/(Ch 2 ) + Y ) ] 1/2, where the constants X, Y, C and K are defined in the previous lemmas 1, 3 and 4. Theorem 2 (a posteriori error estimates) For any v H0(Ω) H 2 4 (Ω), let v h := P h v S h and v h := P 0 v h Sh. Then, it follows that v v h L 2 K v h v h L 2 + Ch 2 2 v v h L 2, where C and K are defined in the lemmas 1 and

8 Proof : (proof of Theorem 1 and 2) First, for an arbitrary ψ H 2 0(Ω) and ψ 0 S h, we have ( v v h, ψ) L 2 = ( v v h, ψ ψ 0 ) L 2 = ( v v h, ψ ψ 0 ) L 2 + ( v h, ψ ψ 0 ) L 2 ( v h, ψ ψ 0 ) L 2 = ( v h v h, ψ ψ 0 ) L 2 + ( 2 v v h, ψ ψ 0 ) L 2 v h v h L 2 ψ ψ 0 L v v h L 2 ψ ψ 0 L 2. Thus, setting ψ := v v h H 2 0(Ω) and ψ 0 P x 0 P y 0 ψ S h, from the lemmas 4 and 5, we obtain the desired estimates in Theorem 2. Next, using Theorem 2, Lemma 3 and the property of the L 2 -projection, it follows that v v h L 2 K v h v h L 2 + Ch 2 g v h L 2 K v h v h L 2 + Ch ( ) 2 g h v h L 2 + g g h L 2 ( KX + Ch 2 Y ) g h L 2 + Ch 2 g g h L 2 = [ (KX + Ch 2 Y ) 2 + C 2 h 4 ] 1/2 g L 2 [ (KX/h 2 + CY ) ] 2 1/2 + C 2 h 2 g L 2, which immediately completes the proof of Theorem 1. 3 Numerical examples In this section, we present some numerical examples of a priori and a posteriori error estimates for the approximation of the bi-harmonic problem (1.1). Since the finite element solution u h S h of (1.1) is defined by ( u h, φ h ) L 2 = (f, φ h ) L 2 φ h S h, we have u h = P h u, and thus the above arguments can be applied to the error estimates for this approximate solution u h. That is, using the procedure in the previous section to define u h P 0 u h Sh, we obtain the a priori and a posteriori error estimates of the form and u u h L 2 C 0 h 2 f L 2, (3.1) u u h L 2 K u h u h L 2 + Ch 2 f u h L 2, (3.2) respectively. Here, constants C 0, K and C are same as in theorems in Section 2. We first show several computational results for the constructive a priori constants in Theorem 1 by Table

9 Table 1: Numerical results for the a priori constant 1/h C 0 X Y C 0 h 2 C 0 /C e e e e e e e e e e e e e e e e e e e e The constant C in the table is taken as C = 1/π 2. Next, we present some examples of the a posteriori error for the following bi-harmonic problem. 2 u = f in Ω, u = n u = 0 on Ω, (3.3) where Ω = (0, 1) 2 and f f(x, y) = 8 ( 3x 2 (1 x) 2 + xy(x 1)(y 1)(2x 1)(2y 1) + 3y 2 (1 y) 2). The exact solution of (3.3) is given by u u(x, y) = x 2 y 2 (1 x) 2 (1 y) 2. Table 2 shows numerical results for the a priori and a posteriori error estimates in (3.1) and (3.2), respectively. Note that f L 2 = 992/175 < Table 2: Numerical results for the a priori and a posteriori estimates in (3.1) and (3.2) 1/h (3.1) (3.2) u u h L 2 u h u h L 2 f u h L e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e e

10 (3.1)/h 2 (3.2)/h 2 u u h L 2 /h 2 All the computations were carried out by MATLAB on the Dell Precision 650 Workstation (Intel Xeon Dual CPU 3.20GHz). References [1] V.A. Kondratiev; Boundary problems for elliptic equations in domains with conical or angular points, Tran. Moscow Math. Soc. 16 (1967), [2] K. Nagatou, K. Hashimoto, M.T. Nakao; Numerical verification of stationary solutions for Navier-Stokes problems, MHF Preprint Series, Kyushu University, MHF [3] M.T. Nakao, N. Yamamoto, & Y. Watanabe, A posteriori and constructive a priori error bounds for finite element solutions of Stokes equations, Journal of Computational and Applied Mathematics 91(1998), [4] M.H. Schultz; Spline Analysis, Prentice-Hall, London, [5] N. Yamamoto, M.T. Nakao; Numerical verifications of solutions for elliptic equations in nonconvex polygonal domains, Numer. Math. 65 (1993),

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