Analytical and numerical solutions to an electrohydrodynamic stability problem

Abstract

A linear hydrodynamic stability problem corresponding to an electrohydrodynamic convection between two parallel walls is considered. The problem is an eighth order eigenvalue one supplied with hinged boundary conditions for the even derivatives up to sixth order. It is first solved by a direct analytical method. By variational arguments it is shown that its smallest eigenvalue is real and positive. The problem is cast into a second order differential system supplied only with Dirichlet boundary conditions. Then, two classes of methods are used to solve this formulation of the problem, namely, analytical methods (based on series of Chandrasekar–Galerkin type and of Budiansky–DiPrima type) and spectral methods (tau, Galerkin and collocation) based on Chebyshev and Legendre polynomials. For certain values of the physical parameters the numerically computed eigenvalues from the low part of the spectrum are displayed in a table. The Galerkin and collocation results are fairly closed and confirm the analytical results.

Authors

Călin-Ioan Gheorghiu
Tiberiu Popoviciu Institute of Numerical Analysis, Romanian Academy

F.I. Dragomirescu
Dept. of Math., Univ. ‘‘Politehnica” of Timisoara

Keywords

Linear hydrodynamic stability; bifurcation manifolds; high order eigenvalue problems; hinged boundary conditions; direct analytical methods; Fourier type methods; spectral methods.

References

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Paper coordinates

I.F. Dragomirescu, C.I. Gheorghiu, Analytical and numerical solutions to an electrohydrodynamic stability problem. Appl. Math. Comput., 216 (2010) 3718-3727.
doi: 10.1016/j.amc.2015.10.078

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Applied Mathematics and Computation

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Analytical and numerical solutions to an electrohydrodynamic stability problem

F.I. Dragomirescu a,∗, C.I. Gheorghiu b
a Dept. of Math., Univ. "Politehnica" of Timisoara, Piata Victoriei, No. 2, 300006 Timisoara, Romania
b "T. Popoviciu" Institute of Numerical Analysis, P.O. Box 68, 3400 Cluj-Napoca 1, Romania

1. Introduction

Nowadays the industry and ecology need more and more results from hydrodynamic stability theory for sophisticated fluid motions occurring in complicated circumstances. In certain of these situations, a direct application of numerical methods can lead one to false results due to the bifurcation problems of the stationary solutions set of the Navier-Stokes equations (or of some more general models) and to the dependence of the eigenvalue on physical parameters. That is why, an analytic along with a numerical study of the eigenvalue problems from hydrodynamic stability theory is highly requested. This is in fact one of the most difficult topic in hydrodynamic stability. The occurrence of false secular points in the linear stability of continua was first pointed out by Collatz in 1981 in his paper [4].

A considerable number of theoretical and numerical studies have been devoted to the interaction of electromagnetic fields with fluids. Rosenswieg [24] pointed out that there are three main categories on this subject, i.e. electrohydrodynamics (EHD), magnetohydrodynamics (MHD) and ferrohydrodynamics (FHD). Here we are interested in an eigenvalue problem in EHD which implies the presence of electric forces. The problem at hand consists into an eighth order differential equation, containing only even order derivatives, supplied with homogeneous boundary conditions for the even order derivatives up to sixth order, i.e. the so called hinged boundary conditions.

The main aim of this paper is to solve analytically as well as numerically this problem in order to get confidence in the later. In fact we are mainly interested in the low part of the spectrum of this problem.

With respect to the numerical methods we have to observe two important facts.

First, a straightforward application of the tau method based on Chebyshev polynomials leads to extremely ill conditioned matrices which are also fully populated (the asymptotic order of the entries varies between zero and O(N2×8)O\left(N^{2\times 8}\right) where NN is the spectral parameter). The eighth order Chebyshev differentiation matrices are also fairly bad conditioned. For N=29N=2^{9} the condition number of these matrices attains something of order O(1030)O\left(10^{30}\right) (see our paper [15]). Consequently, as we have shown, a direct application of the Chebyshev collocation method to this eighth order problem leads to huge instabilities.

Second, due to the fact that the boundary conditions imply a fairly challenging lacunar interpolation problem, the Galerkin and the collocation (pseudospectral) methods become directly inapplicable. It is worth noting in connection with this second point that Huang and Sloan, in their papers [20,21], consider a fairly general non lacunar interpolation problem with multiple nodes and then solve some fourth and sixth order eigenvalue problems. We also succeeded (see [13]) in solving a non-standard eigenvalue problem, i.e. an Orr-Sommerfeld equation supplied with boundary conditions containing the spectral parameter, concerning flows driven by surface tension gradients. As it is not the case with our problem, we follow our " D2D^{2"} strategy from [15], i.e. we rewrite the problem as a second order differential system supplied only with Dirichlet boundary conditions (also called clamped boundary conditions). This way, all the three spectral methods, namely tau, Galerkin and collocation can be efficiently applicable. They provide fairly accurate approximations for the low part of the spectrum at a modest computational cost.

The rest of the paper is organized as follows. In Section 2 we introduce the problem and show that whenever the physical parameters satisfy an "ellipticity" condition the smallest eigenvalue is real and positive. In Section 3, a direct analytical method based on the characteristic equation is used in order to solve the eigenvalue problem. In Section 4, we carry out the above transformation of the problem into a second order system supplied with Dirichlet boundary conditions and solve this problem by analytical methods which use Fourier expansions. In Section 5 we solve this eigenvalue problem, first by standard Chebyshev tau method and try to explain its lack of accuracy. We observe that the matrices involved in this method are highly non-normal. In the last subsection we solve the eigenvalue problem using our " D2D^{2} " strategy along with Galerkin methods. For various values of the physical parameters, the computed values of the critical Rayleigh number, are displayed in a table. For the considered numerical values of them, the numerical results confirm the analytical ones.

2. The statement of the problem

The linear stability of the stationary solution in an electrohydrodynamic convection model in a layer situated between the walls z=±0.5z=\pm 0.5, against normal mode perturbations, is governed by the following eigenvalue problem from [10]

{(D2a2)4FLa4F+Ra2(D2a2)F=0,z(0.5,0.5)F=D2F=D4F=D6F=0, at z=±0.5\left\{\begin{array}[]{l}\left(D^{2}-a^{2}\right)^{4}F-La^{4}F+Ra^{2}\left(D^{2}-a^{2}\right)F=0,\quad z\in(-0.5,0.5)\\ F=D^{2}F=D^{4}F=D^{6}F=0,\quad\text{ at }\quad z=\pm 0.5\end{array}\right.

Here FF, which represents the amplitude of the temperature field perturbation, stands for the eigenfunction in (1). The physical parameter aa represents the wavenumber, LL is a parameter effectively measuring the potential difference between the planes and RR stands for the Rayleigh number.

Electrohydrodynamic systems have important industrial application in the construction of devices using the electroviscous effect or charge entrainment, for instance EHD clutch development and EHD high voltage generators.

The linear stability of their steady states typically leads to high order differential eigenvalue problems.
Thus, Roberts in [23] investigated two electrohydrodynamic convection models, based on the Gross’ experiments [17]. They were concerned with a layer of insulating oil confined between two horizontal conducting planes, heated from above and cooled from below. In the first model, the dielectric constant is allowed to vary with the temperature. The homogeneous insulating fluid is assumed to be situated in a layer of depth dd (the fluid occupies the region between the planes z=±0.5dz=\pm 0.5d, which are maintained at uniform but different temperatures), with vertical, parallel applied gradients of temperature and electrostatic potential. The uniform electric field is applied in the zz direction. The second one, also investigated by Turnbull in [27,28], is characterized by a variation of the dielectric constant which is not important but the fluid is weakly conducting and its conductivity varies with temperature. The corresponding eigenvalue equation is simpler than (1) and has the form (see [26, p. 207])

(D2a2)3F+Ra2F+Ma2DF=0\left(D^{2}-a^{2}\right)^{3}F+Ra^{2}F+Ma^{2}DF=0 (2)

with MM the dimensionless parameter measuring the variation of the electrical conductivity with temperature. The boundary conditions, written for the case of rigid boundaries at constant temperatures, read (cf. [26])

F=D2F=D(D2a2)F=0 at z=±0.5F=D^{2}F=D\left(D^{2}-a^{2}\right)F=0\quad\text{ at }\quad z=\pm 0.5 (3)

Roberts [23] solved the problem (2), (3) numerically in order to obtain the

Rmin=mina2RR_{\min}=\min_{a^{2}}R

He found that when the parameter MM is increasing in the range 010000-1000, the minimum value of R,Rmin R,R_{\text{min }} is increasing from 1707.062 to 2065.034 . Unfortunately, a straightforward application of our " D2D^{2} " strategy to problem (2), (3) is impossible due to the odd order of differentiation contained in both differential equation and boundary conditions.

Straughan in his monograph [26] also investigated these EHD convection problems, developing a fully nonlinear energy stability analysis for non-isothermal convection problems in a dielectric fluid. A bifurcation analysis of the problem (2), (3) was performed by us in [7] revealing the false secular points on certain parameters surfaces. A numerical study completed the investigation of the eigenvalue problem.

A first important remark is in order at this moment. By standard variational arguments (integration by parts and the imposing of boundary conditions) a weak formulation of the problem (1) can be obtained. It reads:
find FH04(I)F\in H_{0}^{4}(I) and RR\in\mathbb{C} such that

1212(D4F)(D4V)𝑑z+2a2(2+3a2)1212(D3F)(D3V)𝑑z+4a61212(DF)(DV)𝑑z+a4(a4L)1212FV𝑑z\displaystyle\int_{-\frac{1}{2}}^{\frac{1}{2}}\left(D^{4}F\right)\left(D^{4}V\right)dz+2a^{2}\left(2+3a^{2}\right)\int_{-\frac{1}{2}}^{\frac{1}{2}}\left(D^{3}F\right)\left(D^{3}V\right)dz+4a^{6}\int_{-\frac{1}{2}}^{\frac{1}{2}}(DF)(DV)dz+a^{4}\left(a^{4}-L\right)\int_{-\frac{1}{2}}^{\frac{1}{2}}FVdz
=Ra2{1212(DF)(DV)𝑑z+a21212FV𝑑z},VH04(I),I[0.5,0.5]\displaystyle\quad=R\cdot a^{2}\left\{\int_{-\frac{1}{2}}^{\frac{1}{2}}(DF)(DV)dz+a^{2}\int_{-\frac{1}{2}}^{\frac{1}{2}}FVdz\right\},\quad\forall V\in H_{0}^{4}(I),\quad I\equiv[-0.5,0.5] (4)

with H04(I)H_{0}^{4}(I) representing the closure in the Sobolev space H4(I)H^{4}(I) of the set of infinitely differentiable compactly supported functions on I (cf. [2]).

Moreover, whenever the parameters aa and LL satisfy the "ellipticity" condition, i.e.

a4L0a^{4}-L\geqslant 0 (5)

the problem reduces to a minimization one, i.e.

R=infuH04(l)N(u)D(u)R=\inf_{u\in H_{0}^{4}(l)}\frac{N(u)}{D(u)} (6)

where

N(u):=1212(D4u)2𝑑z+2a2(2+3a2)1212(D3u)2𝑑z+4a61212(Du)2𝑑z+a4(a4L)1212u2𝑑zN(u):=\int_{-\frac{1}{2}}^{\frac{1}{2}}\left(D^{4}u\right)^{2}dz+2a^{2}\left(2+3a^{2}\right)\int_{-\frac{1}{2}}^{\frac{1}{2}}\left(D^{3}u\right)^{2}dz+4a^{6}\int_{-\frac{1}{2}}^{\frac{1}{2}}(Du)^{2}dz+a^{4}\left(a^{4}-L\right)\int_{-\frac{1}{2}}^{\frac{1}{2}}u^{2}dz

and

D(u):=a2{1212(Du)2𝑑z+a21212u2𝑑z}D(u):=a^{2}\left\{\int_{-\frac{1}{2}}^{\frac{1}{2}}(Du)^{2}dz+a^{2}\int_{-\frac{1}{2}}^{\frac{1}{2}}u^{2}dz\right\}

It is clear that the smallest (algebraic) eigenvalue is real and positive, i.e. there exists a first R>0R>0 which satisfies (1).
In spite of the fact that in both formulations (4) and (6) the order of differentiation is halved, it remains too high in the perspective of numerical computations.

3. The direct method

Most of the problems of hydrodynamic, electrohydrodynamic or hydromagnetic stability as well as bifurcation of solutions can be reduced to eigenvalue problems defined by systems of ordinary differential equations including a large set physical parameters. In the presence of more than one physical parameter and with a high order of differentiation in the system, it is, however, difficult to analyze how the most relevant eigenvalue of the system depends on parameters, since, in general, these systems are not selfadjoint and may have variable coefficients. That is why, a numerical study is usually performed in order to obtain the critical eigenvalues defining the neutral manifold.

The direct method based on the characteristic equation was first systematically applied to hydrodynamic stability problems by A . Georgescu and then extensively used by her group e.g. [11,12,7][11,12,7]. The method is one of the most simple methods to treat two-point problems for linear ordinary differential equations with constant coefficients. The characteristic equation associated with (1) reads (see [10])

(λ2a2)4La4+Ra2(λ2a2)=0\left(\lambda^{2}-a^{2}\right)^{4}-La^{4}+Ra^{2}\left(\lambda^{2}-a^{2}\right)=0 (7)

or, by denoting μ:=λ2a2\mu:=\lambda^{2}-a^{2}, it becomes

μ4La4+Ra2μ=0\mu^{4}-La^{4}+Ra^{2}\mu=0 (8)

By means of the direct method, we write the general form of the solution of the two-point boundary value problem (1) in terms of the roots of the characteristic equation. The general solution of the equation depends on the multiplicity of the roots λi\lambda_{i} of the characteristic equation associated with the eigenvalue problem. Whence the importance of discussing the multiplicity of λi\lambda_{i} (see also [11]).

If the λi\lambda_{i} ’s are distinct, then the general solution is a linear combination of hyperbolic sine and cosine functions. If λi\lambda_{i} are multiple, of mλim_{\lambda_{i}} order respectively, then the general solution is a product of a polynomial in zz by cosh(λiz)\cosh\left(\lambda_{i}z\right) and sinh(λiz)\sinh\left(\lambda_{i}z\right), of degree mλi1m_{\lambda_{i}}-1. Further, the introduction of the general solution into the boundary conditions leads to the secular equation.

The neutral manifolds, in particular the neutral curves, separate the domain of stability from the domain of instability. The bifurcation manifolds of the characteristic equation, or part of it, may be false secular manifolds.

In [10] an analytical investigation of the multiplicities of the Eq. (7) was performed. Although vanishing parameters ( a=0a=0, R=0,L=0R=0,L=0 ) are physically meaningless, for bifurcation reasons, these cases were also considered. When a=0a=0, writing the general solution, it was proven in [10] that no secular points exists. For a>0,L=0,R>0a>0,L=0,R>0 we point out that only specific points of the corresponding bifurcation manifolds of the characteristic equation are secular. In this case, the roots of the characteristic equation are

λi,i+4=±a2+μi,i=1,2,3,4\lambda_{i,i+4}=\pm\sqrt{a^{2}+\mu_{i}},\quad i=1,2,3,4

where

μ1=0,μ2=Ra23,μ3=1+i32Ra23,μ4=1i32Ra23\mu_{1}=0,\quad\mu_{2}=-\sqrt[3]{Ra^{2}},\quad\mu_{3}=\frac{1+i\sqrt{3}}{2}\sqrt[3]{Ra^{2}},\quad\mu_{4}=\frac{1-i\sqrt{3}}{2}\sqrt[3]{Ra^{2}}

The secular equation has the form

Δ=8i=13λi4k,j=1,jk3(λj2λk2)2i=13cosh(λi/2)=0\Delta=8\cdot\prod_{i=1}^{3}\lambda_{i}^{4}\cdot\prod_{k,j=1,j\neq k}^{3}\left(\lambda_{j}^{2}-\lambda_{k}^{2}\right)^{2}\cdot\prod_{i=1}^{3}\cosh\left(\lambda_{i}/2\right)=0 (9)

The equation cosh(λi/2)=0\cosh\left(\lambda_{i}/2\right)=0, the only one that can lead to secular points, has solutions for i=3i=3, i.e cosh(λ3/2)=0\cosh\left(\lambda_{3}/2\right)=0 if and only if cos(λ3/2)=0\cos\left(\lambda_{3}/2\right)=0. Thus λ3=(2n1)2π2\lambda_{3}=-(2n-1)^{2}\pi^{2}, and the only secular points are those situated on the manifolds

NCn:R=((2n1)2π2+a2)3a2,nNC_{n}:R=\frac{\left((2n-1)^{2}\pi^{2}+a^{2}\right)^{3}}{a^{2}},\quad n\in\mathbb{N} (10)

The critical value of the Rayleigh number belongs to NC1NC_{1} identical to the classical one from Chandrasekhar [3]. The secular manifold just found is confirmed in the following section by analytical methods based on Fourier series expansions. In order to obtain possible bifurcation sets of the characteristic equation, some other particular cases were investigated in [10]. The number of physical parameters, greater than two, as well as the high order of differentiation in the governing equation, hinder a systematic analytical investigation of the bifurcations of the involved manifolds. That is why, the problem required numerical methods, specific to bifurcation theory, in order to separate numerical solution of the characteristic equation and of the secular equation.

4. Methods based on Fourier series expansions

In order to apply these methods we rewrite the two-point boundary value problem (1) in a different form. First, we introduce the new vector function

𝐔:=(U1,U2,U3,U4)T\mathbf{U}:=\left(\begin{array}[]{llll}U_{1},&U_{2},&U_{3},&U_{4}\end{array}\right)^{T}

with

U1:=(D2a2)U4,U2:=(D2a2)U1,U3:=(D2a2)U2,U4:=FU_{1}:=\left(D^{2}-a^{2}\right)U_{4},\quad U_{2}:=\left(D^{2}-a^{2}\right)U_{1},\quad U_{3}:=\left(D^{2}-a^{2}\right)U_{2},\quad U_{4}:=F

This substitution turns the eighth order equation from (1) into the following system of second order ordinary differential equations

{U1(D2a2)U4=0U2(D2a2)U1=0U3(D2a2)U2=0(D2a2)U3La4U4+Ra2U1=0\left\{\begin{array}[]{l}U_{1}-\left(D^{2}-a^{2}\right)U_{4}=0\\ U_{2}-\left(D^{2}-a^{2}\right)U_{1}=0\\ U_{3}-\left(D^{2}-a^{2}\right)U_{2}=0\\ \left(D^{2}-a^{2}\right)U_{3}-La^{4}U_{4}+Ra^{2}U_{1}=0\end{array}\right.

Consequently, the boundary conditions simplify considerably and become

U1=U2=U3=U4=0 at z=±0.5.U_{1}=U_{2}=U_{3}=U_{4}=0\quad\text{ at }\quad z=\pm 0.5. (12)

It is important to underline that, in this way, the high order (hinged) boundary conditions from the problem (1) transform into simple Dirichlet boundary conditions. This was also the successful strategy in our previous work [15].

Most of the eigenvalue problems occurring in electrohydrodynamic stability theory consists of higher order ordinary differential equations with constant coefficients depending on physical parameters. Herein, the problem of linear stability in the electrohydrodynamic convection is an eighth order eigenvalue problem with constant coefficients depending on three parameters, namely a,Ra,R and LL. Consequently, the discussion of multiplicity of the roots of the characteristic equation when all the parameters are different from zero, becomes fairly laborious. In this way, the application of the analytic direct method becomes quite obscure and alternative methods must also be used. Some of these methods are based on Fourier series. In the
present context we consider two of the most known such methods: the Chandrasekhar-Galerkin method and the Budian-sky-DiPrima method.

With respect to the first one, the unknown functions are written in the form of expansions in Fourier series upon a complete set of trigonometric functions (in L2[I]L^{2}[I] ) which satisfy all boundary conditions. The characteristic equation is represented by the equality to zero of an infinite determinant.

The second one, is a direct expansion approach too, but the trigonometric functions are chosen such that they satisfy only part of the boundary conditions of the problem. In this case, the characteristic equation is the equality to zero of an infinite series.

Let us apply the Chandrasekhar-Galerkin method to (11), (12). To this aim, we expand the unknown functions U1,U2,U3U_{1},U_{2},U_{3}, U4U_{4} upon sets of orthonormal functions that satisfy all boundary conditions. Further we write each of the unknown functions in problem (11), (12) as a sum of an odd function and an even function. In this way, taking into account that an even function is equal to an odd one only if they are both null, the problem splits into the following two-point boundary value problems

{U1o(D2a2)U4o=0U2o(D2a2)U1o=0U3o(D2a2)U2o=0(D2a2)U3oLa4U4o+Ra2U1o=0\displaystyle\left\{\begin{array}[]{l}U_{1_{o}}-\left(D^{2}-a^{2}\right)U_{4_{o}}=0\\ U_{2_{o}}-\left(D^{2}-a^{2}\right)U_{1_{o}}=0\\ U_{3_{o}}-\left(D^{2}-a^{2}\right)U_{2_{o}}=0\\ \left(D^{2}-a^{2}\right)U_{3_{o}}-La^{4}U_{4_{o}}+Ra^{2}U_{1_{o}}=0\end{array}\right. (13)
U1o=U2o=U3o=U4o=0 at z=±0.5\displaystyle U_{1_{o}}=U_{2_{o}}=U_{3_{o}}=U_{4_{o}}=0\quad\text{ at }\quad z=\pm 0.5 (14)

for odd part, and

{U1e(D2a2U4e=0U2e(D2a2)U1e=0U3e(D2a2)U2e=0(D2a2)U3eLa4U4e+Ra2U1e=0\displaystyle\left\{\begin{array}[]{l}U_{1_{e}}-\left(D^{2}-a^{2}U_{4_{e}}=0\right.\\ U_{2_{e}}-\left(D^{2}-a^{2}\right)U_{1_{e}}=0\\ U_{3_{e}}-\left(D^{2}-a^{2}\right)U_{2_{e}}=0\\ \left(D^{2}-a^{2}\right)U_{3_{e}}-La^{4}U_{4_{e}}+Ra^{2}U_{1_{e}}=0\end{array}\right. (15)
U1e=U2e=U3e=U4e=0 at z=±0.5\displaystyle U_{1_{e}}=U_{2_{e}}=U_{3_{e}}=U_{4_{e}}=0\quad\text{ at }\quad z=\pm 0.5 (16)

for even part.
Assume that U1,U2,U3U_{1},U_{2},U_{3} and U4U_{4} are even functions of zz and for the sake of simplicity we will omit the indices in (15), (16). Anyway an analog analysis can be performed for the odd case.

However, better results are obtained for the even case (see [6] for such an example). Taking into account the boundary conditions (12), the unknown functions are expanded upon the orthonormal set in L2(I),{E2n1}n1L^{2}(I),\left\{E_{2n-1}\right\}_{n\geqslant 1}, where

E2n1(z):=2cos(2n1)πzE_{2n-1}(z):=\sqrt{2}\cos(2n-1)\pi z

i.e.

Uj(z):=n=1UjnE2n1(z),j=1,2,3,4U_{j}(z):=\sum_{n=1}^{\infty}U_{j_{n}}E_{2n-1}(z),\quad j=1,2,3,4

The series expansions of the derivatives occurring in (11) are obtained by the backward integration technique (see the monograph [9]). We substitute these expressions in (11) and impose the condition that the residuals be orthogonal to E2m1E_{2m-1}, m=1,2,m=1,2,\ldots. In this way, for the unknown coefficients UjnU_{j_{n}}, we get the system

{U1n+AnU4n=0U2n+AnU1n=0U3n+AnU2n=0AnU3n+Ra2U1nLa4U4n=0\left\{\begin{array}[]{l}U_{1_{n}}+A_{n}U_{4_{n}}=0\\ U_{2_{n}}+A_{n}U_{1_{n}}=0\\ U_{3_{n}}+A_{n}U_{2_{n}}=0\\ -A_{n}U_{3_{n}}+Ra^{2}U_{1_{n}}-La^{4}U_{4_{n}}=0\end{array}\right.

where An=(2n1)2π2+a2A_{n}=(2n-1)^{2}\pi^{2}+a^{2}. The following linear algebraic equation for the constant coefficients U4nU_{4_{n}} is obtained by eliminating Ujn,j=1,2,3U_{j_{n}},j=1,2,3 between the equations of (17)

An4U4nLa4U4nRa2AnU4n=0A_{n}^{4}U_{4_{n}}-La^{4}U_{4_{n}}-Ra^{2}A_{n}U_{4_{n}}=0 (18)

This means the secular equation R=An4La4a2AnR=\frac{A_{n}^{4}-La^{4}}{a^{2}A_{n}}. So, for n=1n=1, the surface

NCL:Rc=(π2+a2)4La4a2(π2+a2)NC_{L}:R_{c}=\frac{\left(\pi^{2}+a^{2}\right)^{4}-L\cdot a^{4}}{a^{2}\cdot\left(\pi^{2}+a^{2}\right)} (19)

gives us the critical points for L0L\neq 0. For L=0L=0, we get

R=An4a2An=((2n1)2π2+a2)3a2R=\frac{A_{n}^{4}}{a^{2}A_{n}}=\frac{\left((2n-1)^{2}\pi^{2}+a^{2}\right)^{3}}{a^{2}} (20)

which implies that the critical secular points ( R,0,aR,0,a ) belong to NC1NC_{1}. This validates the conclusion obtained in the previous section with the direct method.

The Budianski-DiPrima method is based on the Fourier expansion of all unknown functions upon total sets of functions which do not satisfy all boundary conditions of the problem. The unfulfilled boundary conditions lead to some constraints for the Fourier coefficients. In our case, we consider the unknown functions expanded upon the total set {F2n1}n\left\{F_{2n-1}\right\}_{n\in\mathbb{N}} in L2(I)L^{2}(I), where

F2n1(z):=2sin(2n1)πz,nF_{2n-1}(z):=\sqrt{2}\sin(2n-1)\pi z,\quad n\in\mathbb{N}

Then we substitute these expressions in (11), and impose the condition that the residuals be orthogonal onto F2m1F_{2m-1}, m=1,2,m=1,2,\ldots. We obtain the system

{U1n+AnU4n=22(1)nαU2n+AnU1n=22(1)nβU3n+AnU2n=22(1)nγAnU3n+Ra2U1nLa4U4n=22(1)nδ\left\{\begin{array}[]{l}U_{1_{n}}+A_{n}U_{4_{n}}=2\sqrt{2}(-1)^{n}\alpha\\ U_{2_{n}}+A_{n}U_{1_{n}}=2\sqrt{2}(-1)^{n}\beta\\ U_{3_{n}}+A_{n}U_{2_{n}}=2\sqrt{2}(-1)^{n}\gamma\\ -A_{n}U_{3_{n}}+Ra^{2}U_{1_{n}}-La^{4}U_{4_{n}}=2\sqrt{2}(-1)^{n}\delta\end{array}\right.

where α=DU4(0.5),β=DU1(0.5),γ=DU2(0.5),δ=DU3(0.5)\alpha=DU_{4}(0.5),\beta=DU_{1}(0.5),\gamma=DU_{2}(0.5),\delta=DU_{3}(0.5) are arbitrary constants generated by the unfulfilled boundary conditions in the backwards integration technique. The determinant of the system has the form

Δ=An4Ra2AnLa4\Delta=A_{n}^{4}-Ra^{2}A_{n}-La^{4}

Let us assume that Δ0\Delta\neq 0. Solving the system (21) and replacing the solution 𝐔\mathbf{U} into the constraints resulting from the boundary conditions, i.e.

n=1(1)n2Ujn=0,j=1,2,3,4\sum_{n=1}^{\infty}(-1)^{n}\sqrt{2}U_{j_{n}}=0,\quad j=1,2,3,4

the following linear algebraic system in the unknown α,β,γ,δ\alpha,\beta,\gamma,\delta is obtained

{αLa4+βAn3γAn2δAn=0αLa4An+β(La4Ra2An)+γAn3+δAn2=0αLa4An2+βAn(La4+Ra2An)+γ(La4Ra2An)δAn3=0α(An3Ra2)βAn2+γAn+δ=0\left\{\begin{array}[]{l}-\alpha La^{4}+\beta A_{n}^{3}-\gamma A_{n}^{2}-\delta A_{n}=0\\ \alpha La^{4}A_{n}+\beta\left(-La^{4}-Ra^{2}A_{n}\right)+\gamma A_{n}^{3}+\delta A_{n}^{2}=0\\ -\alpha La^{4}A_{n}^{2}+\beta A_{n}\left(La^{4}+Ra^{2}A_{n}\right)+\gamma\left(-La^{4}-Ra^{2}A_{n}\right)-\delta A_{n}^{3}=0\\ \alpha\left(A_{n}^{3}-Ra^{2}\right)-\beta A_{n}^{2}+\gamma A_{n}+\delta=0\end{array}\right.

However, taking into account that the constant α,β,γ,δ\alpha,\beta,\gamma,\delta are not all null, i.e. the determinant of the algebraic system (22) vanishes, we find that Δ=0\Delta=0. Consequently, the same conclusion arises: for L0L\neq 0 the critical secular points belong to NCLNC_{L} and for L=0L=0 the critical point belongs to the manifold NC1NC_{1} given by (10).

The problem represents a specific class of eigenvalue problems for which the parity of the derivatives in the ordinary differential equations and in the boundary conditions allows a splitting of the problems in two parts - an even part and an odd one, both leading to the same neutral curve. This choice simplified the numerical analysis, since simplified trigonometric orthogonal functions were used. They confirmed the bifurcation analysis in the case of a vanishing physical parameter.

5. Numerical methods

5.1. The Chebyshev tau method

The classical (standard) Chebyshev tau method has been applied successfully to many eigenvalue problem from hydrodynamic stability also (see for instance [1,5] and [8] to quote but a few). The pioneering paper was that of Orszag [22]. In the monograph [2] Section 6.4, it is thoroughly analyzed for the Orr-Sommerfeld problem. However, it is fairly clear that this method is universally applicable, i.e., for any type of boundary conditions.

At first, we shift the problem in [1,1][-1,1] by the transformation x=2zx=2z, and approximate each and every unknown function UiU_{i} by an expansion into the Chebyshev "phase" space, namely

UiUiN(x):=n=0N+kUi,nTn(x),i=1,2,3,4U_{i}\sim U_{i_{N}}(x):=\sum_{n=0}^{N+k}U_{i,n}T_{n}(x),\quad i=1,2,3,4 (23)

with kk the order of the linear ordinary differential operator that defines the eigenvalue problem. The real coefficients Ui,nU_{i,n} are unknown. They are determined by imposing that UiN(x)U_{i_{N}}(x) fulfill the system (11) and the boundary conditions (12). Consequently, we get

{A1𝐗=RB1𝐗𝟏bc±𝐗=𝟎bc𝟏bc𝐗=𝟎bc\left\{\begin{array}[]{l}A_{1}\cdot\mathbf{X}=RB_{1}\cdot\mathbf{X}\\ \mathbf{1}_{bc}^{\pm}\cdot\mathbf{X}=\mathbf{0}_{bc}\\ \mathbf{1}_{bc}\cdot\mathbf{X}=\mathbf{0}_{bc}\end{array}\right.

where the block matrices A1A_{1} and B1B_{1} are

A1:=\displaystyle A_{1}:= (I004D2+a2I4D2+a2II0004D2+a2II0004D2a2La4I)\displaystyle\left(\begin{array}[]{cccc}I&0&0&-4D^{2}+a^{2}I\\ -4D^{2}+a^{2}I&I&0&0\\ 0&-4D^{2}+a^{2}I&I&0\\ 0&0&4D^{2}-a^{2}&-La^{4}I\end{array}\right) (25)
B1:=\displaystyle B_{1}:= (000000000000a2I000),\displaystyle\left(\begin{array}[]{cccc}0&0&0&0\\ 0&0&0&0\\ 0&0&0&0\\ -a^{2}I&0&0&0\end{array}\right), (26)

and the unknown vector is

𝐗:=(U1,0,U1,1,U1,N+2,U2,0,,U2,N+2,U3,0,,U3,N+2,U4,0,,U4,N+2)T\mathbf{X}:=\left(U_{1,0},U_{1,1},\ldots U_{1,N+2},U_{2,0},\ldots,U_{2,N+2},U_{3,0},\ldots,U_{3,N+2},U_{4,0},\ldots,U_{4,N+2}\right)^{T}

Both matrices A1A_{1} and B1B_{1} have the dimension 4(N+1)×4(N+3)4(N+1)\times 4(N+3) and their submatrices D2,ID^{2},I and OO have each the dimension (N+1)×(N+3)(N+1)\times(N+3).

For the entries of the second order differentiation matrix D2D^{2} we used the recurrence relationships between the coefficients of the derivatives expansions from the well known monograph of Gottlieb and Orszag [16]. Thus we have

{D2[0,2j]=12(2j)3,j1,D2[i,i+2j]=(i+2j)4j(i+j),i,j1,0, elsewhere. \left\{\begin{array}[]{l}D^{2}[0,2j]=\frac{1}{2}(2j)^{3},\quad j\geqslant 1,\\ D^{2}[i,i+2j]=(i+2j)4j(i+j),\quad i,j\geqslant 1,\\ 0,\quad\text{ elsewhere. }\end{array}\right.

The matrix II is obtained by concatenating the identity matrix of order N+1,IN+1N+1,I_{N+1}, with two columns of zeros, i.e. I=[IN+100]I=\left[I_{N+1}00\right], and OO matrix has each and every entry equal with zero.

As Chebyshev polynomials satisfy Tk(±1)=(±1)k,k=0,1,2,T_{k}(\pm 1)=(\pm 1)^{k},k=0,1,2,\ldots, the matrices 𝟏bc±\mathbf{1}_{bc}^{\pm}and 𝟏bc\mathbf{1}_{bc}, which introduce the boundary conditions, have each dimension 4×4(N+3)4\times 4(N+3). They both contain four blocks, each of dimension 4×(N+3)4\times(N+3), such that

𝟏bc±:=[𝟏bc,1±𝟏bc,2±𝟏bc,3±𝟏bc,4±],𝟏bc:=[ones(4,N+3)ones(4,N+3)],\mathbf{1}_{bc}^{\pm}:=\left[\mathbf{1}_{bc,1}^{\pm}\mathbf{1}_{bc,2}^{\pm}\mathbf{1}_{bc,3}^{\pm}\mathbf{1}_{bc,4}^{\pm}\right],\mathbf{1}_{bc}:=[\operatorname{ones}(4,N+3)\ldots\operatorname{ones}(4,N+3)],

where

𝟏bc,k±(i,j)=(1)j1,1jN+3,1i4,1k4.\mathbf{1}_{bc,k}^{\pm}(i,j)=(-1)^{j-1},1\leqslant j\leqslant N+3,1\leqslant i\leqslant 4,1\leqslant k\leqslant 4.

The matrix 𝟎bc\mathbf{0}_{bc} is defined 𝟎bc:=𝐳𝐞𝐫𝐨𝐬(4,4(N+3)\mathbf{0}_{bc}:=\mathbf{zeros}(4,4(N+3), using for zeros and ones MATLAB notations.
The equations contained in (24) lead in fact to the generalized algebraic eigenvalue problem

𝐀𝐗=R𝐁𝐗\mathbf{A}\cdot\mathbf{X}=R\mathbf{B}\cdot\mathbf{X} (28)

with

𝐀=(A1𝟏bc±𝟏bc),𝐁=(B1𝟎bc𝟎bc)\mathbf{A}=\left(\begin{array}[]{c}A_{1}\\ \mathbf{1}_{bc}^{\pm}\\ \mathbf{1}_{bc}\end{array}\right),\mathbf{B}=\left(\begin{array}[]{c}B_{1}\\ \mathbf{0}_{bc}\\ \mathbf{0}_{bc}\end{array}\right)

which are square matrices of dimension 4(N+3)4(N+3).
The eigenvalue problem (28) was solved for various values of the parameters. For instance, when L=0,a>0L=0,a>0, the analytical study shows that no secular points occur except the points on NC1NC_{1}. For the classical case, i.e. L=0,a=4.92L=0,a=\sqrt{4.92}, the numerical evaluation of the Rayleigh number obtained by the Chebyshev tau method is not fairly close to the well known classical one from Chandrasekhar [3] ( Rcl=657.511R_{cl}=657.511 ). Unfortunately, we got only RCTAU =611.559R_{C_{\text{TAU }}}=611.559. Here and in the subsequent analysis the suffix cc in RCMETHOD R_{C_{\text{METHOD }}}, where METHOD signifies a specific method, stands for the computed critical value of RR, i.e. the smallest value.

Some comments on the lack of accuracy of this method are in order at this moment.
With respect to sparsity and conditioning, the "stiffness" matrices involved in the classical Chebyshev tau method are comparable with those involved in the Chebyshev collocation method, when these methods are used to solve usual second and fourth order eigenvalue problems (Helmholtz, complex Schroedinger, etc.). Anyway, the Galerkin matrices behave better than both with respect to these two parameters (see for instance our monograph [14]).

However the main drawback of Chebyshev spectral methods, tau, Galerkin as well as collocation, consists in the fact that, due to the non-uniform weight associated with the Cebyshev polynomials, they produce by discretization non-symmetric matrices.

There are two major concepts with respect to the measure of non-normality of square matrices. The first one is essentially due to P. Henrici [18]. For a square complex matrix AA the non-normality ratio H(A)H(A) is defined as

H(A):=(ε(AAAA))1/2/ε(A)H(A):=\left(\varepsilon\left(A^{*}A-AA^{*}\right)\right)^{1/2}/\varepsilon(A)

where AA^{*} is the conjugate transpose of AA and ε(A)\varepsilon(A) stands for the Frobenius norm of AA. We have the important estimation

0H(A)21/40\leqslant H(A)\leqslant 2^{1/4}

with H(A)=0H(A)=0 iff AA is normal, i.e. AAAA=0A^{*}A-AA^{*}=0.
The second concept, more recently introduced, is that of pseudospectrum of a matrix and is systematically treated by Trefethen (see for instance [29]).

It is also well known that the non-normality is responsible for a high spectral (with respect to eigenvalues) sensitivity. In this context, our numerical experiments reported in the above quoted monograph, showed that the discretization matrices of Chebyshev tau method have a non-normality ratio around 1 , and very important, it is quite independent of NN, for NN in range 26N2102^{6}\leqslant N\leqslant 2^{10}. It can be improved to something around 0.8 by suitable choice of trial and test functions. Roughly, the Galerkin method produces more normal discretization matrices. They have a non-normality ratio around 0.1 and this can be lowered to 0.01 when N=1024N=1024, which means matrices close to symmetry.

The matrices involved in the Chebyshev collocation method have an intermediate situation. Their non-normality ratio attains 0.4 when N=28N=2^{8}. All these quantitative estimations of non-normality were confirmed by the pseudospectra of the corresponding matrices.

All in all, one important cause in the lack of accuracy of Chebyshev tau method is the high non-normality of its finite dimensional counterpart.

5.2. Spectral Galerkin and collocation type methods

In the following, a Galerkin type spectral method is applied. In this approach the basis (trial) functions satisfy the boundary conditions and they are, along with the test functions, shifted Legendre and Chebyshev polynomials, respectively.

Let us consider for each unknown UiU_{i} the representation

Ui(z)=k=1NUi,kϕk(z),1i4U_{i}(z)=\sum_{k=1}^{N}U_{i,k}\phi_{k}(z),\quad 1\leqslant i\leqslant 4 (29)

where the complete set of orthogonal functions {ϕk}k=1,2,,NL2(I)\left\{\phi_{k}\right\}_{k=1,2,\ldots,N}\in L^{2}(I) is defined by

ϕk(z):=0.5zLk(t)𝑑t\phi_{k}(z):=\int_{-0.5}^{z}L_{k}(t)dt

with LkL_{k} the shifted Legendre polynomials on II, (see [19]). Then we have

ϕk(z)=Tk(z)Tk+2(z)\phi_{k}(z)=T_{k}^{*}(z)-T_{k+2}^{*}(z)

where TkT_{k}^{*} is the shifted Chebyshev polynomials on II. They satisfy the boundary conditions

ϕi(0.5)=ϕi(0.5)=0,k=1,2,,N\phi_{i}(-0.5)=\phi_{i}(0.5)=0,\quad k=1,2,\ldots,N

The system (11) can be written in terms of the expansion functions in the form

{k=1N[U1,kϕkU4,k(D2a2)ϕk]=0k=1N[U2,kϕkU1,k(D2a2)ϕk]=0k=1N[U3,kϕkU2,k(D2a2)ϕk]=0k=1N[U3,k(D2a2)ϕkLa4U1,kϕk+Ra2U1,kϕk]=0\left\{\begin{array}[]{l}\sum_{k=1}^{N}\left[U_{1,k}\phi_{k}-U_{4,k}\left(D^{2}-a^{2}\right)\phi_{k}\right]=0\\ \sum_{k=1}^{N}\left[U_{2,k}\phi_{k}-U_{1,k}\left(D^{2}-a^{2}\right)\phi_{k}\right]=0\\ \sum_{k=1}^{N}\left[U_{3,k}\phi_{k}-U_{2,k}\left(D^{2}-a^{2}\right)\phi_{k}\right]=0\\ \sum_{k=1}^{N}\left[U_{3,k}\left(D^{2}-a^{2}\right)\phi_{k}-La^{4}U_{1,k}\phi_{k}+Ra^{2}U_{1,k}\phi_{k}\right]=0\end{array}\right.

Imposing the condition that the left-hand side of the Eq. (30) to be orthogonal on ϕi,i=1,2,,N\phi_{i},i=1,2,\ldots,N we get an algebraic system in the unknown coefficients Ui,k,i=1,2,3,4U_{i,k},i=1,2,3,4, and k=1,,Nk=1,\ldots,N which determinant, equated to zero, represents the secular equation.

When L=0L=0 the reduced eigenvalue problem correspond to the classical Bé nard convection in the case of free-free boundaries [3], i.e.

{(D2a2)2U=Ra2F(D2a2)F=UF=U=DU=0 at z=±0.5\left\{\begin{array}[]{l}\left(D^{2}-a^{2}\right)^{2}U=-Ra^{2}F\\ \left(D^{2}-a^{2}\right)F=U\\ F=U=DU=0\quad\text{ at }\quad z=\pm 0.5\end{array}\right.
Table 1: Table 1
Numerical estimates for the Rayleigh number for various values of the parameters aa, LL obtained by Galerkin spectral methods based on shifted Legendre (SLP) and shifted Chebyshev (SCP) polynomials and on Chebyshev collocation method (CC) in comparison with the analytical ones obtained from (19).
aa LL RanalyticalR_{\text{analytical }} RSLP (N=6)R_{\text{SLP }}(N=6) RSCP(N=6)R_{SCP}(N=6) RCC(24N28)R_{\mathrm{CC}}\left(2^{4}\leqslant N\leqslant 2^{8}\right)
2 0 667.0098 667.030 667.013 667.0092
4.92\sqrt{4.92} 0 657.5133 657.543 657.527 657.5133
3 0 746.5276 746.54 746.530 746.5276
2 1 666.7214 666.742 666.725 666.7214
4.92\sqrt{4.92} 1 657.1806 657.208 657.192 657.1892
3 1 746.0506 746.067 746.053 746.0506
2 10 664.1258 664.146 664.129 664.1258
4.92\sqrt{4.92} 10 654.1866 654.193 654.177 654.1866
2 16 662.3954 662.399 662.416 35.8873

The numerical evaluations in this case agree with those from Chandrasekhar [3], i.e. for a=4.92a=\sqrt{4.92} we get RCSLP=657.543R_{C_{SLP}}=657.543, RCSCP=657.527R_{C_{SCP}}=657.527 and RCCC=657.5133R_{C_{CC}}=657.5133.

The index cc stands for the critical value of RR and the indices SLP, SCP and CC signify respectively the shifted Legendre polynomial method, the shifted Chebyshev polynomial method and Chebyshev collocation method.

Our numerical evaluations on RR for various methods and two sets of values of parameters aa and LL are concentrated in Table 1. The results are presented in comparison with the analytical ones showing a very good agreement.

It is important to observe that, all the values of the parameters aa and LL, except those from the last row of this table, satisfy a strict "ellipticity" condition (5), i.e. a4L>0a^{4}-L>0. The values of these parameters in the last row satisfy only the condition a4L=0a^{4}-L=0 and consequently the parameter RR lowers drastically in the CC method.

With respect to the Chebyshev collocation method for the eigenvalue problem (1) we refer to our previous paper [15]. Following the " D2D^{2} " strategy from this paper we effectively cope with the boundary value problem (11), (12).

It means that we have to solve the generalized algebraic eigenvalue problem

A1𝐗=RB1𝐗,A_{1}\cdot\mathbf{X}=RB_{1}\cdot\mathbf{X}, (32)

where the eigenvector is

𝐗:=(U1,1,U1,N1,U2,1,,U2,N1,U3,1,,U3,N1,U4,1,,U4,N1)T.\mathbf{X}:=\left(U_{1,1},\ldots U_{1,N-1},U_{2,1},\ldots,U_{2,N-1},U_{3,1},\ldots,U_{3,N-1},U_{4,1},\ldots,U_{4,N-1}\right)^{T}.

The above matrices A1A_{1} and B1B_{1}, are defined in a perfectly similar manner with (25) and (26) respectively.
However, it is important to mention that D2D^{2} stands, in this case, for the second order differentiation matrix (of dimension N1N-1 ) on the classical Chebyshev-Gauss-Lobatto nodes. The matrices II and OO are now square of dimension N1N-1.

This way, the Dirichlet boundary conditions (12) are imposed, as usual, by deleting the first and the last row and column. As in above quoted paper [15], the differentiation matrices come from the paper of Weideman and Reddy [30]. The MATLAB code eigwas used in order to solve the algebraic eigenvalue problem (32). The value of spectral parameter N=16N=16 was large enough in order to assure the accuracy of the first eigenvalue. Numerical experiments with NN between 262^{6} and 282^{8} do not improve the first eigenvalue.

Eventually, we have to notice two important aspects with respect to our " D2 " D^{2\text{ " }} strategy based on Chebyshev collocation method.

First, for the same spectral parameter NN, it furnishes the less large algebraic systems when compared with tau or Galerkin type methods, i.e. the matrices in (32) are square of order 4(N1)4(N-1). It is also very flexible with respect to the implementation process. One drawback of this method consists in the fact that it furnishes 3(N1)3(N-1) spurious eigenvalues. They correspond to the 3(N1)3(N-1) zero rows in the matrix B1B_{1} in (32) (the rank of matrix B1B_{1} equals ( N1N-1 )). However, this fact does not affect the low part of the spectrum which is computed fairly accurate.

Second, we need to emphasize that the applicability of Galerkin and collocation method depends essentially on the possibility to construct trial and test functions that satisfy all the boundary conditions of a given problem. They solve accurately even non-standard eigenvalue problems (see for instance Orr-Sommerfeld-Squire eigenvalue problem in [25]) or singularly perturbed eigenvalue problems (see the Viola’s eigenvalue problem in our previous quoted paper) but which are supplied with fairly simple boundary conditions. This is in fact the main disadvantage of these methods which make them less applicable than the tau method for problems involving complicated boundary conditions.

6. Conclusions

The linear stability problem of electrohydrodynamic convection between two parallel walls was accurately solved by two classes of analytical methods as well as by spectral methods. The eighth order eigenvalue problem was transformed into a second order system of differential equations supplied with (only!) Dirichlet boundary conditions. This new problem was first solved analytically by two methods based on Fourier series. The Fourier approximation was split into an even and an odd part. The analytical computations carried out on these two problems led to the same neutral curve. Then the Chebyshev Galerkin and Chebyshev tau along with our " D2D^{2} " collocation strategy, introduced in our previous paper [15], were used in
order to find the smallest eigenvalue of the original problem. From the physical point of view the computed numerical values of the Rayleigh number lead to the following conclusion: when the parameter which effectively measures the potential difference between the walls is increasing the stability domain is decreasing.

For some values of the physical parameters the bifurcation results are accurately confirmed by our numerical computations.

The accuracy of the numerical results, as well as, the efficiency and the modest cost of the implementation of the " D2D^{2} " strategy, shows once again its superiority over other spectral method to solve high order eigenvalue problems.

Acknowledgement

The first author would like to thank Prof. Adelina Georgescu for her encouragement, advice and support during the years of the author’s Ph.D. study. The work of the second author was partly supported by the Grant 2-CEx06-11-96.

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