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Title | Partial differential equations of electrostatic MEMS |
Creator |
Guo, Yujin |
Publisher | University of British Columbia |
Date Created | 2011-02-15T19:04:22Z |
Date Issued | 2011-02-15T19:04:22Z |
Date | 2007 |
Description | Micro-Electromechanical Systems (MEMS) combine electronics with micro-size mechanical devices in the process of designing various types of microscopic machinery, especially those involved in conceiving and building modern sensors. Since their initial development in the 1980s, MEMS has revolutionized numerous branches of science and industry. Indeed, MEMS-based devices are now essential components of modern designs in a variety of areas, such as in commercial systems, the biomedical industry, space exploration, telecommunications, and other fields of applications. As it is often the case in science and technology, the quest for optimizing the attributes of MEMS devices according to their various uses, led to the development of mathematical models that try to capture the importance and the impact of the multitude of parameters involved in their design and production. This thesis is concerned with one of the simplest mathematical models for an idealized electrostatic MEMS, which was recently developed and popularized in a relatively recent monograph by J. Pelesko and D. Bernstein. These models turned out to be an incredibly rich source of interesting mathematical phenomena. The subject of this thesis is the mathematical analysis combined with numerical simulations of a nonlinear parabolic problem u[sub t] = Δu - [See Thesis for Equation] on a bounded domain of R[sup N] with Dirichlet boundary conditions. This equation models the dynamic deflection of a simple idealized electrostatic MEMS device, which consists of a thin dielectric elastic membrane with boundary supported at 0 above a rigid ground plate located at -1. When a voltage -represented here by λ- is applied, the membrane deflects towards the ground plate and a snap-through (touchdown) may occur when it exceeds a certain critical value λ* (pull-in voltage). This creates a so-called pull-in instability which greatly affects the design of many devices. In order to achieve better MEMS design, the elastic membrane is fabricated with a spatially varying dielectric permittivity profile f (x). The first part of this thesis is focussed on the pull-in voltage λ* and the quantitative and qualitative description of the steady states of the equation. Applying analytical and numerical techniques, the existence of λ* is established together with rigorous bounds. We show the existence of at least one steady state when λ < λ* (and when λ = λ* in dimension N < 8), while none is possible for λ > λ*. More refined properties of steady states--such as regularity, stability, uniqueness, multiplicity, energy estimates and comparison results--are shown to depend on the dimension of the ambient space and on the permittivity profile. The second part of this thesis is devoted to the dynamic aspect of the parabolic equation. We prove that the membrane globally converges to its unique maximal negative steady-state when λ ≤ λ*, with a possibility of touchdown at infinite time when λ = λ* and N ≥ 8. On the other hand, if λ > λ* the membrane must touchdown at finite time T , which cannot take place at the location where the permittivity profile f ( x ) vanishes. Both larger pull-in distance and larger pull-in voltage can be achieved by properly tailoring the permittivity profile. We analyze and compare finite touchdown times by using both analytical and numerical techniques. When λ > λ*, some a priori estimates of touchdown behavior are established, based on which, we can give a refined description of touchdown profiles by adapting recently developed self-similarity methods as well as center manifold analysis. Applying various analytical and numerical methods, some properties of the touchdown set - such as compactness, location and shape - are also discussed for different classes of varying permittivity profiles f (x). |
Genre |
Thesis/Dissertation |
Type |
Text |
Language | Eng |
Collection |
Retrospective Theses and Dissertations, 1919-2007 |
Series | UBC Retrospective Theses Digitization Project [http://www.library.ubc.ca/archives/retro_theses/] |
Date Available | 2011-02-15T19:04:22Z |
DOI | 10.14288/1.0080410 |
Degree |
Doctor of Philosophy - PhD |
Program |
Mathematics |
Affiliation |
Science, Faculty of |
Degree Grantor | University of British Columbia |
Campus |
UBCV |
Scholarly Level | Graduate |
URI | http://hdl.handle.net/2429/31315 |
Aggregated Source Repository | DSpace |
Digital Resource Original Record | https://open.library.ubc.ca/collections/831/items/1.0080410/source |
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Partial Differential Equations of Electrostatic MEMS by Yujin Guo B . S c , China Three Gorges University, 2000 M . S c , Huazhong Normal University, 2003 A THESIS S U B M I T T E D I N P A R T I A L F U L F I L M E N T O F T H E R E Q U I R E M E N T S F O R T H E D E G R E E O F Doctor of Philosophy ' in The Faculty of Graduate Studies (Mathematics) The University of British Columbia July 2007 © Yujin Guo 2007 Abstract Micro-Electromechanical Systems (MEMS) combine electronics with micro-size mechanical de- vices in the process of designing various types of microscopic machinery, especially those in- volved in conceiving and building modern sensors. Since their initial development in the 1980s, M E M S has revolutionized numerous branches of science and industry. Indeed, MEMS-based devices are now essential components of modern designs in a variety of areas, such as in com- mercial systems, the biomedical industry, space exploration, telecommunications, and other fields of applications. As it is often the case in science and technology, the quest for optimizing the attributes of M E M S devices according to their various uses, led to the development of mathematical models that try to capture the importance and the impact of the multitude of parameters involved in their design and production. This thesis is concerned with one of the simplest mathematical models for an idealized electrostatic M E M S , which was recently developed and popularized in a relatively recent monograph by J . Pelesko and D. Bernstein. These models turned out to be an incredibly rich source of interesting mathematical phenomena. The subject of this thesis is the mathematical analysis combined with numerical simulations of a nonlinear parabolic problem u t = Au — on a bounded domain of RN with Dirich- let boundary conditions. This equation models the dynamic deflection of a simple idealized electrostatic M E M S device, which consists of a thin dielectric elastic membrane with bound- ary supported at 0 above a rigid ground plate located at —1. When a voltage -represented here by A - is applied, the membrane deflects towards the ground plate and a snap-through (touchdown) may occur when it exceeds a certain critical value A* (pull-in voltage). This cre- ates a so-called pull-in instability which greatly affects the design of many devices. In order to achieve better M E M S design, the elastic membrane is fabricated with a spatially varying dielectric permittivity profile f(x). The first part of this thesis is focussed on the pull-in voltage A* and the quantitative and qualitative description of the steady states of the equation. Applying analytical and numerical techniques, the existence of A* is established together with rigorous bounds. We show the existence of at least one steady state when A < A* (and when A = A* in dimension N < 8), while none is possible for A > A*. More refined properties of steady states -such as regularity, stability, uniqueness, multiplicity, energy estimates and comparison results- are shown to depend on the dimension of the ambient space and on the permittivity profile. The second part of this thesis is devoted to the dynamic aspect of the parabolic equation. We prove that the membrane globally converges to its unique maximal negative steady-state when A < A*, with a possibility of touchdown at infinite time when A = A* and N > 8. On the other hand, if A > A* the membrane must touchdown at finite time T, which cannot take place at the location where the permittivity profile f(x) vanishes. Both larger pull- in distance and larger pull-in voltage can be achieved by properly tailoring the permittivity ii Abstract profile. We analyze and compare finite touchdown times by using both analytical and numerical techniques. When A > A*, some a priori estimates of touchdown behavior are established, based on which, we can give a refined description of touchdown profiles by adapting recently developed self-similarity methods as well as center manifold analysis. Applying various analytical and numerical methods, some properties of the touchdown set -such as compactness, location and shape— are also discussed for different classes of varying permittivity profiles f(x). i i i Table of Contents Abstract i i Table of Contents iv List of Tables vi List of Figures vi i Acknowledgements ix Statement of Co-Authorship x 1 Introduction 1 1.1 Electrostatic M E M S devices 1 1.2 P D E s modeling electrostatic M E M S 2 1.2.1 Analysis of the elastic problem 2 1.2.2 Analysis of electrostatic problem 4 1.3 Overview and some comments 7 2 Pull-In Voltage and Steady-States 14 2.1 Introduction 14 2.2 The pull-in voltage A* . 17 2.2.1 Existence of the pull-in voltage 17 2.2.2 Monotonicity results for the pull-in voltage 19 2.3 Estimates for the pull-in voltage 22 2.3.1 Lower bounds for A* 22 2.3.2 Upper bounds for A* 23 2.3.3 Numerical estimates for A* 26 2.4 The branch of minimal solutions 28 2.4.1 Spectral properties of minimal solutions 29 2.4.2 Energy estimates and regularity 31 2.5 Uniqueness and multiplicity of solutions 37 2.5.1 Uniqueness of the solution at A = A* 37 2.5.2 Uniqueness of low energy solutions for small voltage 39 2.5.3 Second solutions around the bifurcation point 40 2.6 Radially symmetric case and power-law profiles 41 iv Table of Contents 3 Compactness along Lower Branches 47 3.1 Introduction 47 3.2 Mountain Pass solutions 51 3.3 Minimal branch for power-law profiles 55 3.4 Compactness along the second branch 61 3.4.1 Blow-up analysis 61 3.4.2 Spectral confinement 68 3.4.3 Compactness issues 72 3.5 The second bifurcation point 74 3.6 The one dimensional problem 75 4 Dynamic Deflection 76 4.1 Introduction 76 4.2 Global convergence or touchdown 78 4.2.1 Global convergence when A < A* 78 4.2.2 Touchdown at finite time when A > A* 79 4.2.3 Global convergence or touchdown in infinite time for A = A* 82 4.3 Location of touchdown points 87 4.4 Estimates for finite touchdown times 91 4.4.1 Comparison results for finite touchdown time 91 4.4.2 Explicit bounds on touchdown times 93 4.5 Asymptotic analysis of touchdown profiles 97 4.5.1 Touchdown profile: f{x) = 1 97 4.5.2 Touchdown profile: variable permittivity 99 4.6 Pull- in distance 101 5 Refined Touchdown Behavior 107 5.1 Introduction 107 5.2 A priori estimates of touchdown behavior 109 5.2.1 Lower bound estimate 112 5.2.2 Gradient estimates 113 5.2.3 Upper bound estimate 116 5.3 Refined touchdown profiles 121 5.3.1 Refined touchdown profiles for N = 1 124 5.3.2 Refined touchdown profiles for N > 2 126 5.4 Set of touchdown points • • 127 5.4.1 Radially symmetric case • 128 5.4.2 One dimensional case 131 6 Thesis Summary 134 6.1 Stationary Case 134 6.2 Dynamic Case 134 Bibliography 136 List of Tables 2.1 Numerical values for pull-in voltage A* with the bounds given in Theorem 2.1.1. Here the exponential permittivity profile is chosen as (2.3.21) 2.2 Numerical values for pull-in voltage A* with the bounds given in Theorem 2.1.1. Here the power-law permittivity profile is chosen as (2.3.21) 4.1 Computations for finite touchdown time T with the bounds T*, TQ^\, T\%\ and T2,A given in Proposition 4-4-3. Here the applied voltage A = 20 and the profile is chosen as (4-4-^3) 4.2 Numerical values for finite touchdown time T at different applied voltages A = 5, 10, 15 and 20, respectively. Here the constant permittivity profile f(x) = 1 is chosen 4.3 Numerical values for pull-in voltage A*: Table (a) corresponds to exponential profiles, while Table (b) corresponds to power-law profiles List of Figures 1.1 The simple electrostatic MEMS device 3 2.1 Plots of u(0) versus X for the constant permittivity profile f(x) = 1 defined in the unit ball J3i(0) C RN with different ranges of N. In the case of N > 8, we have A* = (QN — 8)/9 16 2.2 Plots of X* versus a for a power-law profile (heavy solid curve) and the exponen- tial profile (solid curve). The left figure corresponds to the slab domain, while the right figure corresponds to the unit disk 26 2.3 Plots ofu(0) versus X for profile f(x) = \x\a (a > 0) defined in the slab domain (N = 1). The numerical experiments point to a constant a* > 1 (analytically given in (2.6.10),) such that the bifurcation diagrams are greatly different for different ranges of a: 0 < a < 1, 1 < a < a* and a > a* 43 2.4 Top figure: Plots of u(0) versus X for 2 < N < 7, where u(0) oscillates around the value A* defined in (2.6.12) andu* is regular. Bottom figure: Plots ofu(Q) versus X for N > 8: when 0 < a < a**, there exists a unique solution for (S)\ with X € (0,A*) and u* is singular; when a > a**, u(0) oscillates around the value A* defined in (2.6.12) and u* is regular 45 3.1 Top figure: plots of u(0) versus X for the case where f(x) = 1 is defined in the unit ball -Bi(O) C RN with different ranges of dimension N, where we have X* = (67V —8)/9 for dimension N > 8. Bottom figure: plots ofu(0) versus X for the case where f(x) = 1 is defined in the unit ball Bi(0) C M.N with dimension 2 < N <7, where X* (resp. X%) is the first (resp. second) turning point 48 4.1 Left Figure: u versus x for X = 4.38. Right Figure: u versus x for X = 4.50. Here we consider (4.3.1) with f(x) = \2x\ in the slab domain 88 4.2 Left Figure: u versus r for X = 1.70. Right Figure: u versus r for X = 1.80. Here we consider (4.3.1) with f(r) = r in the unit disk domain 88 4.3 Left Figure: plots of u versus x for different f(x) at X = 8 and t = 0.185736. Right Figure: plots of u versus x for different X with f(x) = \2x\ and t = 0.1254864 92 4.4 Plots of the pull-in distance \u(0)\ = |u*(0)| versus a for the power-law profile (heavy solid curve) and the exponential profile (solid curve). Left figure: the slab domain. Right figure: the unit disk 102 vn List of Figures 4.5 Left figure: plots ofu versus \x\ at A = A* for a = 0, a = 1, a = 3, anda = 10, in i/ie unit disk for the power-law profile. Right figure: plots ofu versus \x\ at A = A* for a = 0, a = 2, a = 4, and a = 10, in £/ie unit disk for the exponential profile. In both figures the solution develops a boundary-layer structure near \x\ = 1 as OL is increased 103 4.6 Bifurcation diagram of w (0) = —7 versus XQ from the numerical solution of (4-6.6) 103 4.7 Comparison of numerically computed X* (heavy solid curve) with the asymptotic result (dotted curve) from (4-6.7) for the unit disk. Left figure: the exponential profile. Right figure: the power-law profile 104 4.8 Left figure: plots ofu versus x at A = A* in the slab domain. Right figure: plots ofu versus \x\ at A = A* in the unit disk domain 105 4.9 Left figure: plots ofu versus x at A = A* in the slab domain. Right figure: plots ofu versus \x\ at A = A* in the unit disk domain 106 5.1 Left figure: plots of u versus x at different times with f(x) = 1 — x2 in the slab domain, where the unique touchdown point is x = 0. Right figure: plots of u versus r = \x\ at different times with f(r) = 1 — r2 in the unit disk domain, where the unique touchdown point is r = 0 too 129 5.2 Left figure: plots of u versus x at different times with f(x) = e~x in the slab domain, where the unique touchdown point is x = 0. Right figure: plots of u versus r = \x\ at different times with f(r) = e~r in the unit disk domain, where the unique touchdown point is r = 0 too 130 5.3 Left figure: plots of u versus x at different times with f(x) = ex _ 1 in the slab domain, where the unique touchdown point is still at x = 0. Right figure: plots of u versus r — \x\ at different times with f(r) — er _ 1 in the unit disk domain, where the touchdown points satisfy r = 0.51952 130 5.4 Left figure: plots of u versus x at different times with f(x) = 1/2 — x/2 in the slab domain, where the unique touchdown point is x = —0.10761. Right figure: plots of u versus r = \x\ at different times with f(x) = x + 1/2 in the slab domain, where the unique touchdown point is x = 0.17467 131 5.5 Plots ofu versus x at different times in the slab domain, for different permittivity profiles f[a](x) given by (5.4.5). Top left (a): when a = 0.5, two touchdown points are at x = ±0.12631. Top right (b): when a = 1, the unique touchdown point is at x = 0. Bottom Left (c): when a = 0.785, touchdown points are observed to consist of a closed interval [—0.0021255,0.0021255]. Bottom right (d): local amplified plots of (c) 132 vi i i Acknowledgements M y greatest gratitude goes to my supervisor, Nassif Ghoussoub. Without his expert guidance, enormous patience, constant encouragement, and continuing quest for mathematical rigor, this thesis would not have been possible. I deeply acknowledge his generosity with his time, and his invaluable suggestions and insightful comments. I would like to thank my collaborators Michael J . Ward, Zhenguo Pan and Pierpaolo Esposito, from whom I have benefited a lot. I am particularly grateful to Michael J . Ward, whose graduate course led me to learn about the P D E models of electrostatic M E M S , and the pioneering work of J . Pelesko. I would also like to thank Professor Louis Nirenberg for pointing me to the pioneering work of Joseph and Lindgren, and eventually to the extensive mathematical literature on nonlinear eigenvalue problems. I will always be grateful to the P D E team at U B C (whether faculty, postdocs, or graduate students), and in particular Ivar Ekeland, Tai-Peng Tsai, Stephen Gustafson, Daniele Cassani, Abbas Maomeni, Y u Yan, and Meijiao Guan for their constant support. Many thanks also go to Danny Fan for her great help over the past three years. Financial support from Research Assistantship under Nassif Ghoussoub (2003-2004), Chi - K i t Wat Scholarship (2004-2005), T. K . Lee Scholarship (2005-2006) and U . B . C. Graduate Fellowships (2004-2007), is gratefully acknowledged. Finally, I would like to extend my thanks to my parents and my wife who have given me constant support and encouragement during my studies at U B C . ix Statement of Co-Authorship The numerical results in sections 2.3.3 were published in: [1] Y . Guo, Z. Pan and M . J . Ward, Touchdown and pull-in voltage behavior of a MEMS device with varying dielectric properties, S I A M , J . Appl . Math. 66 (2005), 309-338. Most of the results in Chapter 2 have been published in: [2] N . Ghoussoub and Y . Guo, On the partial differential equations of electrostatic MEMS devices: stationary case, S I A M , J . Math. Anal . 38 (2007), 1423-1449. The main results of Chapter 3 are due to appear in the following paper in press: [3] P. Esposito, N . Ghoussoub and Y . Guo, Compactness along the branch of semi-stable and unstable solutions for an elliptic problem with a singular nonlinearity, Comm. Pure Appl . Math. , accepted (2006). Sections 4.5 and 4.6 can be found in the paper [1] mentioned above, and while the main results of sections 4.1-4.4 come from the following paper which is also in press: [4] N . Ghoussoub and Y . Guo, On the partial differential equations of electrostatic MEMS devices II: dynamic case, N o D E A Nonlinear Diff. Eqns. Appl . , accepted (2007). The main results of Chapter 5 can be found in the paper: [5] Y . Guo, On the partial differential equations of electrostatic MEMS devices III: refined touchdown behavior, submitted (2006). x Chapter 1 Introduction The roots of micro-system technology lie in the technological developments accompanying World War II, and in particular the work around radar stimulated research in the synthesis of pure semiconducting materials. These materials, especially pure silicon, have become the main components of integrated and modern technology of Micro-Electromechanical Systems ( M E M S ) . The advent of M E M S has revolutionized numerous branches of science and industry, and their applications are continuing to nourish, as they are becoming essential components of modern sensors in areas as diverse as the biomedical industry, space exploration, and telecom- munications. A comprehensive overview of the rapidly developing field of M E M S technology can be found in the relatively recent monograph by Pelesko and Bernstein [52]. Not only is this book a rich source of information about the incredibly vast area of applications of M E M S , but also it contains justifications and derivations of the fundamental partial differential equations that model such devices. It is the mathematical analysis and the numerical simulations of these equations that concern us in this thesis. In this introduction, we shall first briefly recall some of the industrial applications of M E M S while referring the reader to the book of Pelesko and Bernstein mentioned above for a more comprehensive survey. For the convenience of the reader, we shall also include a derivation of the simplest P D E modeling electrostatic M E M S devices, which is by now a well known and broadly accepted mathematical model. 1.1 Electrostatic MEMS devices The state of the art is best summarized by the following description of Pelesko and Bernstein in the book [52]: "Spurred by rapid advances in integrated circuit manufacturing, microsystems process technology is already well developed. As a result, researchers are increasingly focusing their attention on device engineering questions. Foremost among these is the question of how to provide accurate, controlled, stable locomotion for M E M S devices. Just as what has been recognized for some time by several scientists and engineers, it is neither feasible nor desirable to attempt to reproduce modes of locomotion used in the macro world. In fact, the unfavorable scaling of force with device size prohibits this approach in many cases. For example, magnetic forces, which are often used for actuation in the macro world, scale poorly into the micro domain, decreasing in strength by a factor of ten thousand when linear dimensions are reduced by a factor of ten. This unfavorable scaling renders magnetic forces essentially useless. A t the micro level, researchers have proposed a variety of new modes of locomotion based upon thermal, biological, and electrostatic forces". The use of electrostatic forces to provide locomotion for M E M S devices is behind the mathematical model that we address in this thesis. Experimental work in this area dates back to 1967 and the work of Nathanson et. al. [49]. 1 Chapter 1. Introduction In their seminal paper, Nathanson and his coworkers describe the modeling and manufacture of, experimentation with, a millimeter-sized resonant gate transistor. These early M E M S de- vices utilized both electrical and mechanical components on the same substrate resulting in improved efficiency, lowered cost, and reduced system size. Nathanson and his coworkers also introduced a simple lumped mass-spring model of electrostatic actuation. In an interesting parallel development, the British scientist, G . I. Taylor [55] investigated electrostatic actuation at about the same time as Nathanson. While Taylor was concerned with electrostatic deflec- tion of soap films rather than the development of M E M S devices, his work spawned a small body of the literature with relevance to M E M S . Since Nathanson and Taylor's seminal work, numerous investigators have been continually exploring new uses of electrostatic actuation, such as Micropumps, Microswitches, Microvalves, Shuffle Motor and etc. See [52] for more details on how these devices use electrostatic forces for their operation. 1.2 PDEs modeling electrostatic MEMS A key component of some M E M S systems is the simple idealized electrostatic device shown in Figure 1.1. The upper part of this device consists of a thin and deformable elastic membrane that is held fixed along its boundary and which lies above a parallel rigid grounded plate. This elastic membrane is modeled as a dielectric with a small but finite thickness. The upper surface of the membrane is coated with a negligibly thin metallic conducting film. When a voltage V is applied to the conducting film, the thin dielectric membrane deflects towards the bottom plate. A similar deflection phenomenon, but on a macroscopic length scale, occurs in the field of electrohydrodynamics. In this context, Taylor [55] studied the electrostatic deflection of two oppositely charged soap films, and he predicted a critical voltage for which the two soap films would touch together. A similar physical limitation on the applied voltage occurs for the M E M S device of Figure 1.1, in that there is a maximum voltage V* -known as pull-in voltage- which can be safely applied to the system. More specifically, if the applied voltage V is increased beyond the critical value V * , the steady-state of the elastic membrane is lost, and proceeds to snap through at a finite time creating the so-called pull-in instability (cf. [29, 30, 32, 50]). The existence of such a pull-in voltage was first demonstrated for a lumped mass-spring model of electrostatic actuation in the pioneering study of [49], where the restoring force of the deflected membrane is modeled by a Hookean spring. In this lumped model the attractive inverse square law electrostatic force between the membrane and the ground plate dominates the restoring force of the spring for small gap sizes and large applied voltages. This leads to snap-through behavior whereby the membrane hits the ground plate when the applied voltage is large enough. Following closely the analysis in [32, 52], we shall now formulate the partial differential equations that models the dynamic deflection w = w(x',y',t') of the membrane shown in Figure 1.1. 1.2.1 Analysis of the elastic problem We shall apply Hamilton's least action principle and minimize the action S of the system. Here the action consists of the superposition of the kinetic energy, the damping energy and the potential energy in the system. The pointwise total of these energies is the Lagrangian C 2 Chapter 1. Introduction Figure 1.1: The simple electrostatic MEMS device. for the system. We then have S = J CdX'dt' = Kinetic Energy + Damping Energy + Potential Energy (12 1) = : Ek + Ed + Ep , where 0 ' is the domain of the membrane with respect to (x',y'). In this subsection, dX' denotes dx'dy', and the gradient V (and the Laplace operator A ' ) denotes the differentiation only with respect to x' and y!. For the dynamic deflection w = w(x', y', t') of the membrane, the kinetic energy Ek is * Jti Jn1 where p is the mass density per unit volume of the membrane, and A is the thickness of the membrane. The damping energy E^ is assumed to be Ed = $ f2 [ tfdX'dt', (1.2.3) 2 Jti Jn' where a is the damping constant. For this model, the potential energy Ep is composed of Ep = Stretching Energy + Bending Energy. (1-2-4) It is reasonable to assume that the stretching energy in the elastic membrane is proportional to the changes in the area of the membrane from its un-stretched configuration. Since we assume the membrane is held fixed at its boundary, we may write the stretching energy as Stretching Energy := - /x( / y/l + \V'w\2dX'dt' - | f i ' | ( i 2 - *i)) - (1-2.5) Jti Jn' Here the proportionality constant / i , is simply the tension in the membrane. We linearize this expression to obtain Stretching Energy := / * f \Vw\2dX'dt'. (1.2.6) 2 Ju Jn1 Chapter 1. Introduction The bending energy is assumed to be proportional to the linearized curvature of the membrane, that is t Bending Energy := / * / \A'w\2dX'dt'. (1.2.7) 2 Jt! JQ' Here the constant D is the fiexural rigidity of the membrane. For the total potential energy Ep we now have E p = - f2 f (^\Vw\2 + ^\A'w\2)dX'dt'. (1.2.8) Jti Jo,' 2 2 Combining (1.2.1) - (1.2.3) and (1.2.8) now yields that C = + \ t f - | | V ' t S | 2 - § | A ' £ | 2 . (1.2.9) According to Hamilton's principle, we should minimize / t 2 / , + f™ 2 - f | v ' ^ 2 - § \A '™\ 2) d x ' d t '> (i-2-io) which implies - v i a Euler-Lagrange variational calculus- that the elastic membrane's deflection w satisfies p A ^ + a ^ - f i A ' w + DA'2w = 0. (1.2.11) 1.2.2 Analysis of electrostatic problem We now analyze the electrostatic problem of Figure 1.1 and we allow the dielectric permittivity £2 — £2(2', y') of the elastic membrane to exhibit a spatial variation reflecting the varying di- electric permittivity of the membrane. Therefore, in view of (1.2.11) we assume the membrane's deflection w satisfying P A W ^ + D A ' 2 ™ = - f l V ' * l 2 ' ( L 2 - 1 2 ) where the term on the right hand side of (1.2.12) denotes the force on the elastic membrane, which is due to the electric field. We suppose that such force is proportional to the norm squared of the gradient of the potential and couples the solution of the elastic problem to the solution of the electrostatic problem. A derivation of such source term may be found in [42]. We now apply dimensionless analysis to equation (1.2.12). We scale the electrostatic po- tential with the applied voltage V , time with a damping timescale of the system, the x' and y' variables with a characteristic length L of the device, and z' w with the size of the gap d between the ground plate and the undeflected elastic membrane. So we define w = - , * = x = T , y = T , z = 7 , t = —2, (1.2.13) and substitute these into equation (1.2.12) to find ^ + ^ - A w + ^ = - A ( S ) [ £ W + ( S ) 2 ] i n fi' ( L 2-1 4 ) 4 Chapter 1. Introduction where Q is the dimensionless domain of the elastic membrane. Here the parameter 7 satisfies ( 1 , , 5 > and the parameter 5 measures the relative importance of tension and rigidity and it is defined by (1.2.16) The parameter e is the aspect ratio of the system e = | , (1-2.17) and the parameter A is a ratio of the reference electrostatic force to the reference elastic force and it is defined by In view of equation (1.2.12), and in order to further understand membrane's deflection, we need to know more about the electrostatic potential 4> inside the elastic membrane. In the actual design of a M E M S device there are several issues that must be considered. Typically, one of the primary device design goals is to achieve the maximum possible stable steady-state deflection, referred to as the pull-in distance, with a relatively small applied voltage V . Another consideration may be to increase the stable operating range of the device by increasing the pull- in voltage V* subject to the constraint that the range of the applied voltage is limited by the available power supply. This increase in the stable operating range may be important for the design of microresonators. For other devices such as micropumps and microvalves, where snap- through (or called touchdown) behavior is explicitly exploited, it is of interest to decrease the time for touchdown, thereby increasing the switching speed. One way of achieving larger values of V* while simultaneously increasing the pull-in distance, is to use a voltage control scheme imposed by an external circuit in which the device is placed (cf. [53]). This approach leads to a nonlocal problem for the deflection of the membrane. A different approach is to introduce a spatial variation in the dielectric permittivity of the membrane, which was theoretically studied in [29-32, 50? ? ]. In the following we discuss the electrostatic potential <f> by introducing a spatial varying dielectric permittivity into our simple M E M S model. The idea is to locate the region where the membrane deflection would normally be largest under a spatially uniform permittivity, and then make sure that a new dielectric permittivity £2 is largest -and consequently the profile f(x,y) smallest- in that region. We assume that the ground plate, located at z' = 0, is a perfect conductor. The elastic membrane is assumed to be a uniform thickness A = 2t. The deflection of the membrane at time t' is specified by the deflection of its center plane, located at z' = w(x' ,y' ,t'). Hence the top surface is located at z' — w(x', y', t') + t, while the bottom of the membrane is located at z' = w(x', y', t') — 1. We also assume that the potential between the membrane and ground plate, cpi, satisfies A 0 i = O , (1.2.19) 5 Chapter 1. Introduction <pi{x',y',0)=0 in fi', (1.2.20) where we assume that the fixed ground plate is held at zero potential. The potential inside the membrane, 02, satisfies V • (e2V<f>2) = 0, (1.2.21) fa(x',y',w + i) = V in O ' . (1.2.22) Defining ^i = y , i>2 = y (1.2.23) together with (1.2.13), and applying dimensionless analysis again, the electrostatic problem reduces to d2ip 7,d2ip d2tbs * ! M s < * £ > + £ < * £ > ) - ° ' — ^ — a - " * ) tp = 0 , £ = 0 (ground plate); ip = 1, z = tu + i (upper membrane surface), (1.2.25) together with the continuity of the potential and the displacement fields across z = w — c. Here ip is the dimensionless potential scaled with respect to the applied voltage V , and, as before, e = d/L is the device aspect ratio. In general, we note that one has little hope of finding an exact solution ip from (1.2.24) and (1.2.25). However, we can simplify the system by examining a restricted parameter regime. In particular, we consider the small-aspect ratio limit e = d/L 1. Physically, this means that the lateral dimensions of the device in Figure 1.1 are larger compared to the size of the gap between the undeflected membrane and ground plate. In the small-aspect ratio limit c C l , equation (1.2.24) gives = 0. Further, the asymptotical solution of ip which is continuous across z = w — i is { ipL-^r,,, 0 < z < w - L , 1 + iL$iifx-iw + l ) ) t w - t < z < w + L. (1-2-26) To ensure that the displacement field is continuous across z = w — L to leading order in e, we impose that dip, dip. where the plus or minus signs indicate that ^ is to be evaluated on the upper or lower side of the bottom surface z = w — L of the membrane, respectively. This condition determines tpi in (1.2.26) as *L=[1 + — (1-2.27) From (1.2.26) and (1.2.27), we observe that the electric field in the z-direction inside the membrane is independent of z, and is given by J ^ ^ r i - f ^ ^ r 1 - - ^ forKl. (1.2.28) 6 Chapter 1. Introduction In engineering parlance, this approximation is equivalent to ignoring fringing fields. Therefore, in the small-aspect ratio limit E < 1, the governing equation (1.2.14) is simplified from (1.2.28) into 7 ^ o " + -H7 - Aio + 5A2w = ^ i n Q - (1.2.29) at1 at eiw2. We now suppose the membrane is undeflected at the initial time, that is w(x,y,0) = 1. Since the boundary of the membrane is held fixed, we have w(x,y,t) = 1 on the boundary of fi at any time t > 0. We now also assume that the membrane's thickness A = 2dt satisfies A = 2di -C 1 which gives 7 <C 1 in view of (1.2.15), and assume that the elastic membrane has no rigidity which gives 5 = 0 in view of (1.2.16). Therefore, by using further simplification, the dynamic deflection w = w(x,t) of the membrane on a bounded domain fi in R 2 , is found to satisfy the following parabolic problem ^ _ A u , = - ^ M f o r x e ^ , (1.2.30a) at w(x,t) = l for xedCL, (1.2.30b) w(x,0) = l for x e f i , (1.2.30c) where the parameter A > 0 is called the applied voltage in view of relation (1.2.18), and while the nonnegative continuous function f(x) characterizes the varying dielectric permittivity of the elastic membrane, in the point of the relation f(x)= , T £ \ . . (1.2.31) £2(Lx,Ly) Therefore, understanding dynamic deflection of our M E M S model is equivalent to studying solutions of (1.2.30). 1.3 Overview and some comments The main contents of this thesis are divided into two major parts, each consisting of two chapters. Part I: Pull-In Voltage and Stationary Deflection The first part of this thesis is focussed on pull-in voltage and stationary deflection of the elastic membrane satisfying (1.2.30). For convenience, by setting w = 1 — u we study the following semilinear elliptic problem with a singular nonlinearity 0 < u < 1 in Q, K• > x u = 0 on dCl, where A > 0 denotes the applied voltage and the nonnegative continuous function f(x) char- acterizes the varying dielectric permittivity of the elastic membrane. Mathematically, we consider the domain Q C RN with any dimension N > 1. (S)\ was firstly studied by Pelesko 7 I Chapter 1. Introduction in [50], where the author focussed on lower dimension N = 1 or 2, and he considered either f(x) > C > 0 or f(x) — \x\a. In my joint work with Pan and Ward [32], we studied (S)\ for a more general profile f(x) which can vanish somewhere. In the past two years, (S)\ was further extended and sharpened in our series work [22, 29]. The main results of Chapter 2 can be found in [29]. In §2.2 we mainly show the existence of a specific pull-in voltage in the sense A* := A*( f i , / ) = sup | A > 0 | (S)\ possesses at least one solution j . (1.3.1) The definition of A* shows that for A < A*, there exists at least one solution for (S)\; while for A > A*, there is no solution for (S)\. In §2.2 we also study pull-in voltage's dependence on the size and shape of the domain, as well as on the permittivity profile. These properties wil l help us in §2.3 establish some lower and upper bound estimates on the pull-in voltage, see Theorem 2.1.1. In particular, we shall prove in Theorem 2.1.1(5) that if f(x) = \x\a with a > 0 and B\ is a unit ball in RN, then we have > , , R , , Q x (2 + a)(3iV + a - 4 ) A (#1, \x\ ) = , provided N > 8 and 0 < a < a**{N) := 4-6Af+3^5(Af-2)_ In Chapter 2, we also consider issues of uniqueness and multiplicity of solutions for (S)\ with 0 < A < A*. The bifurcation diagrams in Figure 2.1 of §2.1 show the complexity of the situation, even in the radially symmetric case. One can observe from Figure 2.1 that the number of branches -and of solutions- is closely connected to the space dimension, a fact that we analytically discuss in §2.4, by focussing on the very first branch of solutions considered to be "minimal" in the following way. Definition 1.3.1. A solution u\(x) of (S)\ is said to be minimal if for any other solution u of (S)\ we have u\(x) < u(x) for all x G fi. We shall prove that for any 0 < A < A*, there exists a unique minimal solution u\ of {S)\ such that H\t\(u\) > 0. Moreover, for each x £ Q,, the function A —> u\(x) is strictly increasing and differentiable on (0, A*). On the other hand, one can introduce for any solution u of (S)\, the linearized operator at u defined by LUi\ = —A — ^l^l and its eigenvalues {^^(u) ; k = 1,2,...}. The first eigenvalue is then simple and is given by: HltX(u) = inf { < £ u , A 0 , t f ) H i ( n ) ; <A e C^iSl), Jj<l>(x)\2dx = l } . Stable solutions (resp., semi-stable solutions) of (S)\ are those solutions u such that /ui^(u) > 0 (resp., fiit\(u) > 0). We note that there already exist in the literature many interesting results concerning the properties of the branch of semi-stable solutions for Dirichlet boundary value problems of the form — Au = Xh(u) where h is a regular nonlinearity (for example of the form e" or (1 + u)p for p > 1). See for example the seminal papers [20, 43, 44] and also [15] for a survey on the subject and an exhaustive list of related references. The singular situation was considered in a very general context in [48], and the analysis of Chapter 2 is completed to allow 8 Chapter 1. Introduction for a general continuous permittivity profile f(x) > 0. Our main results in this direction are stated in Theorem 2.1.2, where fine properties of steady states -such as regularity, stability, uniqueness, multiplicity, energy estimates and comparison results- are shown to depend on the dimension of the ambient space and on the permittivity profile. More precisely, Theorem 2.1.2 gives that if 1 < TV < 7 then -by means of energy estimates- one has sup^ 6 ( 0 || ux ||oo< 1 and consequently, u* = l im u\ exists in C2'a((l) with 0 < a < 1 and is a solution for (S)\* such that /ii,A* (u*) = 0. In particular, u* -often referred to as the extremal solution of problem {S)\- is unique. On the other hand, if TV > 8, f{x) = \x\a with 0 < a < a**(N) := 4 ~ 6 j V + y ( J V " 2 ) 2+q and Q is the unit ball, then the extremal solution is necessarily u*(x) = 1 — \x\ 3 and is therefore singular. In general, the function u* exists in any dimension, does solve {S)\> in a suitable weak sense, and is the unique solution in an appropriate class. The above result says that it is, however, a classical solution in dimensions 1 < N < 7, and this will allow us to start another branch of non-minimal (unstable) solutions. Indeed, following ideas of Crandall-Rabinowitz [20], we show in §2.5 that, for 1 < TV < 7 and for A close enough to A*, there exists a unique second branch U\ of solutions for (S)\, bifurcating from u*, with HiAU\)<0 while fi2,x(Ux)>0. (1.3.2) In §2.6 we present some numerical evidences for various conjectures relating to the case where permittivity profile f(x) = \x\a is denned in a unit ball. The bifurcation diagrams show four possible regimes -at least if the domain is a ball: A . There is exactly one branch of solution for 0 < A < A*. This regime occurs when TV > 8, and if 0 < a < a**{N) := 4 ~ 6 i V + 3 ^ ; v ~ 2 ) . The results of this section actually show that in this range, the first branch of solutions "disappears" at A* which happens to be equal t 0 A 4 a , A 0 = ( 2 + a ) ( T + a - 4 ) . B . There exists an infinite number of branches of solutions. This regime occurs when • TV = 1 and a > a* := - \ + \\fin]2. • 2 < JV < 7 and a > 0; . N > 8 and a > a**(N) := 4 ~ 6 j V + 3 f (*-2>. In this case, A*(a, N) < A* and the multiplicity becomes arbitrarily large as A approaches -from either side- A»(a, N) at which there is a touchdown solution u (i.e., || u \\oo= 1)- C. There exists a finite number of branches of solutions. In this case, we have again that \*(a,N) < A*, but now the branch approaches the value 1 monotonically, and the number of solutions increase but remains finite as A approaches A*(a, N). This regime occurs when N = 1 and 1 < a < a* := - \ + \^27/2. D. There exist exactly two branches of solutions for 0 < A < A* and one solution for A = A*. The bifurcation diagram vanishes when it returns to A = 0. This regime occurs when N = 1 and 0 < a < 1. 9 Chapter 1. Introduction The main results of Chapter 3 are available in [22]. Note from Chapter 2 that the com- pactness of minimal branch solutions of (S)\ holds in 1 < TV < 7 for any profile f(x). In §3.3 we extend such compactness to higher dimension TV > 8, provided that Q is a unit ball and f(x) = | z | Q satisfies a > a**(N) := 4 ~ 6 j V + 3 ^ (yv -2 ) ^ Analytically, this provides a clear dis- tinction between the case where the permittivity profile f(x) is bounded away from zero, and where it is allowed to vanish somewhere. Once the compactness of minimal branch solutions for (S)\ holds, then the standard Crandall-Rabinowitz theory [20] implies the existence of a second solution U\ of (S)\ on the deleted left neighborhood of A*, where U\ satisfies M I , A ( C / A ) < 0 while /Z 2 ,A(£/A ) > 0. (1.3.3) In §3.2 using truncation we shall provide the mountain pass variational characterization of such branch U\. In Chapter 3, we are also interested in continuing the second branch t i l l the second bifur- cation point, by means of the implicit function theorem. Suppose 2 < TV < 7 and / £ C(Cl) satisfies k f(x) = (j[\x-pi\at)g(x), g(x)>C>0mn (1.3.4) i=l for some points pi £ and exponents on > 0. Let (A n )„ be a sequence such that A„ —> A £ [0, A*] and let un be an associated solution of (S)\n such that M2,n := M2,A„(u») > 0. ' (1.3.5) Then in §3.4 we shall use blow-up analysis of elliptic P D E to prove the compactness of un. We expect that such a result should be true for radial solutions on the unit ball for TV > 8, a > a^, and / G C(Cl) as in (3.3.1). As far as we know, there are no compactness results of this type in the case of regular nonlinearities, marking a substantial difference with the singular situation. We define the second bifurcation point in the following way for (5) \ : A^ = inf {(3 > 0 : 3 a curve Vx € C([/3, A*]; C2{Q)) of solutions for {S)x s.t. / Z 2 , A ( V A ) > 0 , V A = | 7 A V A € ( A * - M * ) } . Assume / € C(Cl) to be of the form (1.3.4). Then for 2 < TV < 7 we shall prove in §3.5 that A2 £ (0, A*) and for any A £ (A^A*) there exist at least two solutions u\ and V\ for (S)\, so that fH,x(Vx)<0 while M 2 , A ( ^ A ) > 0 . In particular, for A = A2, there exists a second solution, namely V * := l im V\ so that A|Aj M i , A * ( n < 0 and M 2 ) A . ( V * ) = 0. We note that the second branch cannot approach the value A = 0 as illustrated by the bifur- cation diagram in Figure 3.1. Now let V\, A £ (/?, A*) be one of the curves appearing in the definition of A2 . B y (1.3.3), we have that Ly^,\ is invertible for A £ (A* — S, A*) and, as long as it remains invertible, we 10 Chapter 1. Introduction can use the Implicit Function Theorem to find V\ as the unique smooth extension of the curve U\ (in principle U\ exists only for A close to A*). We now define A** in the following way A** = inf{/3 > 0 : VA G (/?, A*) 3 Vx solution of (S)x so that M2,A (V a ) > 0, Vx = U~x for A G (A* - 6, A*)}. Then, A2 < A** and there exists a smooth curve Vx for A G (A**, A*) so that Vx is the unique maximal extension of the curve U\. This is what the second branch is supposed to be. If now A2 < A**, then for A G (A2, A**) there is no longer uniqueness for the extension and the "second branch" is defined only as one of potentially many continuous extensions of U\. In dimension 1, we have a stronger but somewhat different compactness result. Recall that ^fc,A„(wn) is the k—th eigenvalue of LUnixn counted with their multiplicity. Let / be a bounded interval in R and / G Cl{I) be such that / > C > 0 in I. Suppose ( u „ ) n is a solution sequence for (S)xn on I, where A „ - » A £ (0,A*]. Assume for any n G N and k large enough, we have Hk<n := Hk,\„(un) > 0- Then in §3.6 we shall prove the compactness of un. Note that the multiplicity result in dimension 2 < N < 7 holds also in dimension 1 for any A G (A^A*) . Part II: Dynamic Deflection and Touchdown Behavior The second part of this thesis is devoted to the dynamic deflection and touchdown behavior of (1.2.30). When f(x) = 1, there already exist some results for touchdown (quenching) behavior of (1.2.30) since 1980s, see [38, 39, 46] and references therein. However, since the profile f(x) is assumed to be varying and vanish somewhere for M E M S models, the dynamic behavior of (1.2.30) turns out to be a more rich source of interesting mathematical phenomena. So far the dynamic behavior of (1.2.30) with varying profile has been investigated in [26, 30-32]. Based on [30, 32], in Chapter 4 we focus on the dynamic problem of (1.2.30) in the form ^ - A u = - ^ > f o r ( L 3 - 6 a ) at (1 — v,y u(x,t) = 0 for x G dtt, u{x,0) = 0 for x G Q . (1.3.6b) Recall that a point XQ G 0 is said to be a touchdown point for a solution u(x,t) of (1.3.6), if for some T G (0,+oo], we have l im u(x0,tn) = 1. T is then said to be a -finite or infinite- touchdown time. For each such solution, we define its corresponding -possibly infinite- "first touchdown time": Tx(fl,f,u) = inf {t G (0,+oo]; supu(x,t) = l ) . In §4.2, we analyze the relationship between the applied voltage A, the permittivity profile / , and the solution u of (1.3.6). More precisely, for A* defined as in (1.3.1), we show in §§4.2.1 & 4.2.3 that if A < A*, then the unique dynamic solution of (1.3.6) must globally converge to its unique minimal steady-state; while we shall prove in §4.2.2 that if A > A*, then the unique dynamic solution of (1.3.6) must touchdown at finite time. Note that in the case where the unique minimal steady-state of (1.3.6) at A = A* is singular, which can happen if N > 8, above analysis shows the possibility of touchdown at infinite time. In §4.3 we first compute global convergence or touchdown behavior of (1.3.6) for different applied voltage A, and we then prove rigorously the following surprising fact exhibited by the 11 Chapter 1. Introduction numerical simulations: the permittivity profile / cannot vanish in any isolated set of finite-time touchdown points. §4.4 is focussed on the analysis and estimate of finite touchdown time, which often translates into useful information concerning the speed of the operation for many M E M S devices such as R F switches or micro-valves. In §4.5 we discuss touchdown profiles by the method of asymptotic analysis, and our pur- pose is to look insights into the refined touchdown rate. §4.6 is devoted to the pull-in distance of M E M S devices, referred to as the maximum stable deflection of the elastic membrane before touchdown occurs. We provide numerical results for pull-in distance with some explicit exam- ples, from which one can observe that both larger pull-in distance and pull-in voltage can be achieved by properly tailoring the permittivity profile. Some interesting phenomena are also observed there. The purpose of Chapter 5 is to discuss the refined touchdown behavior of (5.1.1) (i.e., (1.2.30)) at finite touchdown time. In §5.2 we shall derive some a priori estimates of touchdown profiles under the assumption that touchdown set of u is a compact subset of fi. Note that whether the compactness of touchdown set holds for any f(x) satisfying (5.1.2) is a quite challenging problem. In §5.2 we first prove that the compactness of touchdown set holds for the case where the domain Q is convex and f(x) satisfies the additional condition §£ < 0 on Qc5 := {x € Q : dist(x, dfi) < 5} for some 5 > 0. (1.3.7) where v is the outward unit norm vector to dQ.. Whether the assumption (1.3.7) can be removed is still open. Under the compactness assumption of touchdown set, in §5.2.1 we establish the lower bound estimate of touchdown profiles and we also prove an interesting phenomenon: finite-time touchdown point of u is not the zero point of f(x), see Theorem 5.1.1. In §5.2.2 we estimate the derivatives of touchdown solution u, see Lemma 5.2.4; and as a byproduct, an integral estimate is also given in Theorem 5.2.5 of §5.2.2. Motivated by Theorem 5.1.1, the key point of studying touchdown profiles is a similarity variable transformation of (5.1.1). For the touchdown solution u = u(x,t) of (5.1.1) at finite time T, we use the associated similarity variables y^-^ZjL, s=-log(T-t), u(x,t) = (T — t)*wa(y, s), (1.3.8) where a is any interior point of O. Then wa(y,s) is defined in Wa := {(y, s) : a + ye~s/2 € Q,s > s' = —logT}, and it solves „ , „ 1 \pf(a + ye~2) p(wa)s - V • (pVwa) - -pwa + H J y / = 0, " wa where p(y) = e~^2^4. Here wa(y,s) is always strictly positive in Wa. The slice of Wa at a given time s 1 is denoted by Q a ( s 1 ) := WaC\ {s = s1} = e3 / 2 ( f i - a). Then for any interior point a of Q., there exists SQ = So(a) > 0 such that B3 := {y : \y\ < s} C O a (s) for s > s0. We introduce the frozen energy functional Ea[wa](3) = l f p\Vwa\2dy-\ [ pw2ady- f ^ ^ - d y . (1.3.9) 1 JB, 6 J B s J B s WA 12 Chapter 1. Introduction By estimating the energy Ea[wa](s) in Bs, in §5.2.3 we shall prove the upper bound estimate of wa, see Theorem 5.2.10. Applying certain a priori estimates of §5.2, we establish refined touchdown profiles in §5.3, using self-similarity methods and center manifold analysis. We note that for N > 2, we are only able to apply Theorem 5.3.5 to study the refined touchdown profiles for special touchdown points -such as x = 0 in the radial case- and the situation is widely open for more general cases. Adapting various analytical and numerical techniques, we focus in §5.4 on the set of touch- down points. In §5.4.1 we discuss the radially symmetric case of (5.1.1), and we prove there that suppose f(r) = f(\x\) satisfies (5.1.2) and f'(r) < 0 in a bounded ball BR(0) C RN with N > 1, then r = 0 is the unique touchdown point of u, which is the maximum value point of / ( r ) = /(|a:|), see Theorem 5.1.4 and Remark 5.1.1. For the one dimensional case, Theorem 5.1.4 already implies that touchdown points must be unique when the permittivity profile f(x) is uniform. In §5.4.2 we further discuss the one dimensional case of (5.1.1) for varying profile f(x), where numerical simulations show that the touchdown set may consist of a discrete set or a finite compact subsets of the domain. Finally, a summary of this thesis is given in Chapter 6. 13 Chapter 2 Pull-in Voltage and Steady-States 2.1 Introduction In this Chapter we study pull-in voltage and stationary deflection of the elastic membrane satisfying (1.2.30), such that our discussion is centered on the following elliptic problem where A > 0 characterizes the applied voltage, while nonnegative f(x) describes the varying permittivity profile of the elastic membrane shown in Figure 1.1. We focus on the stable and semi-stable stationary deflections of the membrane, while the unstable case is considered in Chapter 3, and the dynamic case in Chapters 4 and 5. Throughout this Chapter and unless mentioned otherwise, solutions for (S)x are taken in the classical sense. The permittivity profile f(x) wil l be allowed to vanish somewhere, and will be assumed to satisfy This Chapter is organized as follows. In §2.2 we mainly show the existence of a specific pull-in voltage in the sense and we also study its dependence on the size and shape of the domain, as well as on the permittivity profile. These monotonicity properties will help us establish in §2.3 new lower and upper bound estimates on the pull-in voltage. We shall write \Q\ for the volume of a domain ft in RN and P(Cl) := JQQOIS for its "perimeter", with CJN referring to the volume of the unit ball B\(0) in RN. We denote by u.n the first eigenvalue of —A on HQ(Q) and by 4>N the corresponding positive eigenfunction normalized with j^cp^dx = 1. Theorem 2.1.1. Assume f is a function satisfying (2.1.1) on a bounded domain Q in RN, then there exists a finite pull-in voltage A* := X*(Cl,f) > 0 such that 1- If0<\< A*, there exists at least one solution for (S)\. 2. If A > A*, there is no solution for (S)\. f e Ca(Q) for some a £ (0,1], 0 < / < 1 and / > 0 on a subset of O of positive measure. (2.1.1) A*(fi, / ) = sup{A > 0 | (S)\ possesses at least one solution}, 14 Chapter 2. Pull-In Voltage and Steady-States 3. The following bounds on A* hold for any bounded domain fi; (8N 6 i V - 8 \ _ J _ / " V ^ / O I O A A : = m a x | - , ^ - | — ( M ) < A (f i) , (2.1.2a) m i n { ^ = 2 T i n f ^ ^ 4- If Q is a strictly star-shaped domain, that is if x • v(x) > a > 0 for all x G dQ, where i/(x) is the unit outer normal at x G dCl, and if f = 1, then A ( Q ) - A s - 8aN\n\ • ( 2 ' 1 - 3 ) In particular, if£l = B\ (0) C RN then we have the bound A*(^(0) ) < H ± ^ ! . 5. / / / ( z ) = |a;| a with a > 0 and is a 6a// o/ radius R, then we have V ( * „ . | x | » ) > A . W - • n m i { 4 ' 2 + < '»f + ' " , ' 2 + ' » " ^ - | - ' > - 4 ' } R - ^ . ( 2X4) Moreover, ifN>8andO<a< a**{N) := i-6N+3^(N-'2); w e have y(B1,\xn=i2 + a ) i 3 N 9 + a - ' ) . (2-1.5) In §2.3.3 we give some numerical estimates on A* to compare them with the analytic bounds given in Theorem 1.1 above. Note that the upper bound A i is relevant only when / is bounded away from 0, while the upper bound A 2 is valid for all permittivity profiles. However, the order between these two upper bounds can vary in general. For example, in the case of exponential permittivity profiles of the form f(x) = ea^ _ 1 ) on the unit disc, one can see that A i is a better upper bound than A 2 for small a, while the reverse holds true for larger values of a. The lower bounds in (2.1.2) and (2.1.4) can be improved in small dimensions, but they are optimal -at least for the ba l l - in dimension larger than 8. We also consider issues of uniqueness and multiplicity of solutions for (S)\ with 0 < A < A*. The bifurcation diagrams in Figure 2.1 show the complexity of the situation, even in the radially symmetric case. One can see that the number of branches -and of solutions- is closely connected to the space dimension, a fact that we establish analytically in §4, by focussing on the very first branch of solutions considered to be "minimal" in the following way. Definition 2.1.1. A solution u\(x) of (S)\ is said to be minimal if for any other solution u of (S)\ we have u\(x) < u(x) for all x G f i . 15 Chapter 2. Pull-In Voltage and Steady-States Figure 2.1: Plots o/u(0) versus X for the constant permittivity profile f(x) = 1 defined in the unit ballBi(0) C RN with different ranges ofN. In the case ofN > 8, we have X* = (6iV—8)/9. One can also consider for any solution u of (S)\, the linearized operator at u denned by Lu,\ — —A — (illu)l a n ( i i t s eigenvalues {nk,\{u);k = 1,2,...}. The first eigenvalue is then simple and is given by fihX(u) = inf | ( L U ) A 0 , 0 ) ^ ( n ) ; 0 £ C0°°(ft), j^\<l>{x)\2dx = l j . Stable solutions (resp., semi-stable solutions) of (S)\ are those solutions u such that /j,\tx{u) > 0 (resp., > 0)- Our main results in this direction can be stated as follows. Theorem 2.1.2. Assume f is a function satisfying (2.1.1) on a bounded domain Q in RN, and consider X* :— X*(Cl,f) as defined in Theorem 2.1.1. Then the following hold: 1. For any 0 < A < A * , there exists a unique minimal solution ux of {S)\ such that M I , A ( U A ) > 0. Moreover, for each x £ Cl, the function A —> ux(x) is strictly increas- ing and differentiable on (0 ,A*) . 2. If 1 < N < 7 then -by means of energy estimates- one has s u p A 6 ( 0 A . ) || u\ \\oo< 1 and consequently, u* — l im u\ exists in C2'a(Cl) with 0 < a < 1 and is a solution for {S)x* such that u.\t\*(u*) = 0. In particular, u* -often referred to as the extremal solution of problem (S)\- is unique. 3. On the other hand, if N > 8, f{x) = \x\a with 0 < a < a**{N) := 4 - 6 j V + y ( J V ~ 2 ) and 2+a Cl is the unit ball, then the extremal solution is necessarily u*(x) = 1 — \x\ 3 and is therefore singular. We note that, in general, the function u* exists in any dimension, does solve (S)A* in a suitable weak sense, and is the unique solution in an appropriate class. The above theorem says that it is, however, a classical solution in dimensions 1 < N < 7, and this will allow us to start another branch of non-minimal (unstable) solutions. Indeed, we show in §2.5 -following ideas 16 Chapter 2. Pull-In Voltage and Steady-States of Crandall-Rabinowitz [20]- that, for 1 < N < 7, and for A close enough to A*, there exists a unique second branch U\ of solutions for (S)\, bifurcating from u*, with HiAUx)<0 while H2,x{Ux)>0. (2.1.6) In Chapter 3, we shall provide a variational (mountain pass) characterization of these unstable solutions and more importantly, we establish -under the same dimension restriction as above— a compactness result along the second branch of unstable solutions leading to a -nonzero- second bifurcation point. Issues of uniqueness, multiplicity and other qualitative properties of the solutions for (S)\ are still far from being well understood, even in the radially symmetric case which we consider in §2.6. Some of the classical work of Joseph-Lundgren [43] and many that followed can be adapted to this situation when the permittivity profile is constant. However, the case of a power-law permittivity profile f(x) = \x\a defined in a unit ball already presents a much richer situation. In §2.6 we present some numerical evidence for various conjectures relating to this case, some of which will be tackled in Chapter 3. A detailed and involved analysis of compactness along the unstable branches will be discussed there, as well as some information about the second bifurcation point. 2.2 The pull-in voltage A* In this section, we first establish the existence and some monotonicity properties for the pull-in voltage A*, which is defined as X*(Cl, / ) = sup{A > 0 | (S)\ possesses at least one solution} . (2.2.1) In other words, A* is called pull-in voltage if there exist uncollapsed states for 0 < A < A* while there are none for A > A*. We then study how A*( f i , / ) varies with the domain fl, the dimension N and the permittivity profile / . 2.2.1 Existence of the pull-in voltage For any bounded domain T in RN, we denote by fir the first eigenvalue of V>r the corresponding positive eigenfunction normalized with s u p i e r ipr = with any domain T in RN the following parameter: va = sup {firH(inf V>r); T domain of RN, T D Cl} , (2.2.2) where H is the function H(t) = ^ + ^ . Theorem 2.2.1. Assume f is a function satisfying (2.1.1) on a bounded domain Cl in RN, then there exists a finite pull-in voltage A* := A*(f2,/) > 0 such that 1. if X < A*, there exists at least one solution for (S)\; 2. if A > A*, there is no solution for (S)\. - A onff^(r) and by = 1. We also associate 17 Chapter 2. Pull-in Voltage and Steady-States Moreover, we have the lower bound A W ) > ^ T T V (2-2-3) s u p x e n fix) Proof: We need to show that (S)\ has at least one solution when A < i / n ( sup n f{x))~l. Indeed, it is clear that u = 0 is a subsolution of [S)\ for all A > 0. To construct a supersolution of {S)\, we consider a bounded domain T D with smooth boundary, and let (fir,ipr) be its first eigenpair normalized in such a way that sup 0*0 = 1 and inf ipr(x) := s\ > 0. We construct a supersolution in the form tp = Aipr where A is a scalar to be chosen later. First, we must have Ai[>r > 0 on dQ, and 0 < 1 — Atpr < 1 in Q, which requires that 0 < A < 1. We also require - A * - ( T % * - ° i n Q ' ( 2 ' 2 ' 4 ) which can be satisfied as long as: * * A i n ( 2 - 2 - 5 ) or Xsupf(x) <p(A,T) :=^mi{g(sA); s£ [*i(r),l]}, (2.2.6) n where g(s) = s ( l - s ) 2 . In other words, A*sup/(a;) > sup{/3( J4,T); 0 < a < l,T D fj}, and n therefore it remains to show that vn = sup {/3(A, r); 0 < a < 1, T D ft}. (2.2.7) For that, we note first that inf O(J4S) = min{s(j4si),5(4)}. se[si,i] We also have that g{Asi) < g{A) if and only if A2{sl - 1) - 2i4(sf - 1) + (si - 1) < 0 which happens if and only if A2{s\ + s\ + 1) - 2A(s\ + 1) + 1 > 0 or if and only if either A < A- or J4 > A+ where _ s i + 1 + _ 1 A _ si + 1 - y / i l _ 1 + s 2 + 1 + s i s i + 1 - y'sT ' ~ s 2 + 1 + s i s i + 1 + v^T ' Since < 1 < a+, we get that f ff(^si) if 0 < ^ < A _ , G(A) = inf 5 (i4s) = I (2.2.8) [ 5 ( A ) if A _ < A < 1. 18 Chapter 2. Pull-in Voltage and Steady-States We now have that = g'(Asi)si > 0 for all 0 < A < A— And since A- > | , we have dA <U = g'(A) < 0 for all A- < A < 1. It follows that sup inf g(As) = sup G(A) = G(A-) = g(A-) 0<a<l s€[si,l] 0<a<l = I (1 I )2 (si + 1 + x / s i ) 3 = ff(infnVr)), which proves our lower estimate. Now that we know that A* > 0, pick A e (0,A*) and use the definition of A* to find a A £ (A, A*) such that (S)x has a solution u^, ( 1 - " A ) 2 ' and in particular — Aux > ^1^2 for x £ Q, which then implies that ux is a supersolution of (S)\. Since u = 0 is a subsolution of (S)x, then we can conclude again that there is a solution ux of (S)x for every A <E (0, A*). It is also easy to show that A* is finite, since if (S)x has at least one solution 0 < u < 1, then, by integrating against the first (positive) eigenfunction ipn, we get + CO > fia > fia f mjjn = - / u ^ a = ~ [ ^ n A u = A / / / " ^ 2 d a ; - A / ^ ^ d x Jn Jo Jo Jo l 1 _ u) Jo (2.2.9) and therefore A* < +oo. The definition of A* implies that there is no solution of (S)\ for any A > A*. • 2.2.2 Monotonicity results for the pull-in voltage In this subsection, we give a more precise characterization of A*, namely as the endpoint for the branch of minimal solutions. This wil l allow us to establish various monotonicity properties for A* that wil l help in the estimates given in the next subsections. First we give a recursive scheme for the construction of minimal solutions. T h e o r e m 2.2.2. Assume f is a function satisfying (2.1.1) on a bounded domain Q in RN, then for any 0 < A < A*(f2,/) there exists a unique minimal positive solution u\ for (S)\. It is obtained as the limit of the sequence {un(X;x)} constructed recursively as follows: UQ = 0 in Q and, for each n > 1, —Aun = \ 2 , xeQ; (1 - un-iY (2.2.10) 0 < u n < 1. £ £ Q ; un = 0, x e d£l. 19 Chapter 2. Pull-In Voltage and Steady-States Proof: Let u be any positive solution for (S)\, and consider the sequence {un(X;x)} defined in (2.2.10). Clearly u(x) > uo = 0 in ft, and whenever u(x) > un-\ in Q, then -Mu-un) = X f ( x ) [ ^ 2 - ^ - ^ ) > 0 , xetl, u — un = 0, x £ dCl. The maximum principle and an immediate induction yield that 1 > u(x) > un in for all n > 0. In a similar way, the maximum principle implies that the sequence {un(X;x)} is monotone increasing. Therefore, {un(X;x)} converges uniformly to a positive solution u\(x), satisfying u(x) > u\{x) in Q,, which is a minimal positive solution of (S)\. It is also clear that u\ is unique in this class of solutions. • Remark 2.2.1. Let g(x, £, fi) be the Green's function of the Laplace operator, with g(x, £, fi) = 0 on dQ. Then the iteration in (2.2.10) can be replaced by UQ = 0 in Q, and for each n > 1, U n ( A ; x) = \Ja . (2.2.11) u n (A; a;) = 0, a; £ 9 f i . The same reasoning as above yields that limn—too un(X; x) = UA(X ) for all a; £ Q . The above construction of solutions yields the following monotonicity result for the pull-in voltage. Proposition 2.2.3. IfCli C fl2 and if f is a function satisfying (2.1.1) on Q.2, then A*(fii) > X*(Q,2) and the corresponding minimal solutions satisfy un (X,x) < un2(X,x) on fii for every 0 < A < A*(f i 2 ) . Proof: Again the method of sub/supersolutions immediately yields that A*(fii) > X*(Q.2). Now consider, for i = 1,2, the sequences {un(X,x,Q.i)} on fij defined by (2.2.11) where g(x,£,Qi) are the corresponding Green's functions on Oj. Since fix C £l2, we have that g(x,£, Qi) < g(x,t;,£l2) on Q\. Hence, it follows that ui(X,x,Q2) = X f f{0g(x,£,tt2)d£ >xf / ( 0 « / ( a : , ^ n i K = «i(A)a;,n] Jn2 JOi ) on Q\. B y induction we conclude that un(X, x, £l2) > un(X,x, Qi) on Cl\ for all n. On the other hand, since un(X,x,Q2) < un+i(X,x,Q2) on Q2 for n, we get that un(X,x,Cli) < un2(X,x) on fii, and we are done. • We also note the following easy comparison results, and we omit the details. Corollary 2.2.4. Suppose f\,f2 : fi —> R are two functions satisfying (2.1.1) such that / j (a:) < f2(x) on Q., then X*(Q.,f\) > X*(D,,f2), and for 0 < A < A*(fi, f2) we have ui(X,x) < u2(X,x) on Q, where u\(X,x) (resp., u2(X,x)) are the unique minimal positive solution of -Au = 0 $ (resp., -Au = ^ ^ i ) on 9. and u = 0 on dQ. Moreover, if f2(x) > f\(x) on a subset of positive measure, then u\(X,x) < u2(X,x) for all x £ Q.. 20 Chapter 2. Pull-in Voltage and Steady-States We shall also need the following result which is adapted from [6] (Theorem 4.10) where it is proved for regular nonlinearities. Proposition 2.2.5. For any bounded domain T in R N and any function f satisfying (2.1.1) on Y, we have \*(Tj)>\*(BR,n where B R = BR(0) is the Euclidean ball in R N with radius R > 0 and with volume \ B R \ = |r|, and where f* is the Schwarz symmetrization of f. Proof: For any bounded T C R N , define its symmetrized domain T* = BR to be the ball {a; : |a;| < R} with |r| = \ B R \ . If u is a real-valued function on T, we define its symmetrized function u* : V* — BR —> R by u*(x) = sup{^i: x G B R ( ^ ) } where BR(H) is the symmetrization of the superlevel set T(u.) = {x G : \x < u(x)} (i.e., BR(n) = T(n)*). If h and g are continuous functions on T, then the following inequality holds (See Lemma 2.4 of [6]) / hgdx< f h*g*dx. (2.2.12) Jr JBR As in Theorem 4.10 of [6], we consider for any A G (0, \ * { B R ) ) the minimal sequence {un} for (S\) in T as defined in (2.2.10), and let {vn} be the minimal sequence for the corresponding Schwarz symmetrized problem: A/*(a) ( i - v y v = 0 x G dBR (2.2.13b) ^ = T T ^ x£BR, (2.2.13a) with 0 < v < 1 on BR = T * . Since A G (0, X * ( B R ) ) , we can consider the corresponding minimal solution vx for (2.2.136). As in Theorem 2.2.2 we have 0 < vn < vx < 1 on B R for all n > 1. We shall show that {un} also satisfies 0 < u * < vx < 1 on B R for all n > 1. We now write J (a = u>N\x\N) for f*{x), and un{a — u>N\x\N) for u*(x). Applying (2.2.12) and the argument for (4.9) in [6], we obtain that u0 = v$ = 0 in (0, R), and for each n > 1, dun da H — P f. L y^dr > 0 in (0,R), (2.2.14) QW Jo [\-un-iY and „ da a(a) J0 [l-vn-{)2 with g(a) = [ N U J 1 J n a ^ N ~ ^ I N } 2 > 0. We claim that for any n > 1, we have «n(o) < «n(a) a e (0, fl). (2.2.16) In fact, for n = 1 we have du\/da > dvi/da, and integration yields that -u\(a) = u\(R) - ui(a) >v\(R)—vi(a) = —v\(a), and hence u\(a) < vi(a) on [0,^]. (2.2.16) is now proved by induction. Suppose it holds for n < k — 1, then one gets from (2.2.14) and (2.2.15) that dv,k/da > dvk/da, which establishes (2.2.16) for all n > 1. 21 Chapter 2. Pull-in Voltage and Steady-States Therefore, the minimal sequence {un(x)} on T is bounded by m a x x e s H v x ( x ) < 1, and again as in the proof of Theorem 2.2.2, there exists a minimal solution ux for (S)\ on T. This 2.3 Estimates for the pull-in voltage In this section, analytically and numerically we shall discuss estimates of pull-in voltage A*. For that we shall write for the volume of a domain Q in R N and P(Q) := J 9 Q dS for its "perimeter", with LJN referring to the volume of the unit ball -Bi(O) in R N . We denote by H N the first eigenvalue of —A on HQ(CI) and by <pn the corresponding positive eigenfunction normalized with J f i <l>ndx = 1. 2.3.1 Lower bounds for A* While the lower bound in (2.2.3) is useful to prove existence, it is not easy to compute. The following proposition gives more computationally accessible lower estimates for A*. Proposition 2.3.1. Assume f is a function satisfying (2.1.1) on a bounded domain Q in R N , then we have the following lower bound: means A*(I\ / ) > \*{BR, /*). (2.3.1) Moreover, if f(x) = \x\a with a > 0 and ft is a ball of radius R, then we have w D i (A(2 + a){N + a) (2 + q)(3JV + a - 4) A*{B R , \x\a) > max £ '-, i ^ (2.3.2) Finally, ifN>8andO<a< a**(N) := 4 ~ 6 J V + y A r ~ 2 ) , we have \*(B1,\x\a) = (2 + a)(3N + a - 4 ) 9 (2.3.3) Proof: Setting .R it suffices - i n view of Proposition 2.2.5- and since sup / * = sup / Br a to show that (2.3.4) for the case where = BR. In fact, the function w(x) = | (1 — ^ - ) satisfies on BR 2N _ 2N(1 - I)2 1 3R2 ~ 3R2 (1 - 1 ) 2 8N f(x) ~ 2 7 i ? 2 s u P f i / [ i _ 1 ( 1 - J ^ ) ] 2 8N / (a) 2 7 i ? 2 s u p n / ( l - ™ ) 2 " 22 Chapter 2. Pull-in Voltage and Steady-States So for A < 07R2N—f; w is a supersolution of (S)\ in B R . Since on the other hand WQ = 0 is a subsolution of (S)\ and wo < w in then there exists a solution of (S)\ in which proves a part of (2.3.4). A similar computation applied to the function v(x) = 1 — ( ^ ) 5 shows that v is also a supersolution as long as A < gj§r^~j- In order to prove (2.3.2), it suffices to note that w(x) = | ( l — ^ + ° ) is a supersolution for (S)x on BR provided A < 4 ( 2 + ^ + q + q ) , and that u(a;) = 1 - ( ^ ) ^ is a supersolution for (S)x on B f i , provided A < ^ 2 + a ^24- t a ~ 4 ^ • In order to complete the proof of Proposition 2.3.1, we need to establish that the function u*(x) = 1 — l^l2^ is the extremal function as long as N > 8 and 0 < a < a**(N) = 4-6N+3VE(N-2) ^ rp n j g w i j j t n e n y ^ j j t j i a t £ Q r g u c n dimensions and these values of a, the voltage A = ( 2 +») ( 3 ^+»- 4 ) i s exactly the pull-in voltage A*. First, it is easy to check that u* is a ffo(Q)-weak solution of (S)\*. Since ||u*||oo = 1> and by the characterization of Theorem 2.5.1 below, we need only to prove that / m2> [ T ^ S s ^ 2 V^GffoHO) . (2.3.5) Jn Jn {*• ~ u ) However, Hardy's inequality gives for TV > 2: for any <f> £ H Q ( B I ) , which means that (2.3.5) holds whenever 2A* < ^ N ~ ^ or, equivalently, if N > 8 and 0 < a < a** = *-™+*f<>»-*), • Remark 2.3.1. The above lower bounds can be improved at least in low dimensions. First note from (2.3.2) that if N > then A 2 = ( 2+")( 3^+Q- 4) [ s the better lower bound and is actually sharp on the ball as soon as N > 8 and a < a**. For lower dimensions, the best lower bounds are more complicated even when one considers supersolutions of the form v(x) = a(l - (^ ) f e ) and optimize X(a,k,R) over a and k. For example, in the case where a = 0, JV = 2 and R — 1, one can see that a better lower bound can be obtained via the supersolution v(x) = — M 1 ' 6 ) - 2.3.2 Upper bounds for A* We note that (2.2.9) already yields a finite upper bound for A*. However, Pohozaev-type arguments can be used to establish better and more computable upper bounds. For a general domain fi, the following upper bounds on A*(fi) were established in [50] and [32], respectively. Proposition 2.3.2. (1) Assume f is a function satisfying (2.1.1) on a bounded domain in M.N such that info. / > 0, then A W ^ A ^ ^ O n f / ) - 1 . (2.3.6) 23 Chapter 2. Pull-in Voltage and Steady-States (2) If we only suppose that f > 0 on a set of positive measure, then A * ( f t , / ) < A 2 = ^ ( / f<Pndx)-\ (2.3.7) 3 Jn Proo f : (1). We multiply the equation (S)\ by <f>n, integrate the resulting equation over ft, and use Green's identity to obtain J ^ ( - m u + ( ^ } ) 2 )fo dx = 0. (2.3.8) Since C := info / > 0 and <fo > 0, the equality in (2.3.8) is impossible when A C - fiQU + 7- r~ > 0, for all x e ft. (2.3.9) (1 - u ) 2 A simple calculation using (2.3.9) shows that (2.3.9) holds when A > A i , where A\ is given in (2.3.6). This completes the proof of Proposition 2.3.2(1). As shown below, the bound (2.3.6) on A* is rather good when applied to the constant permittivity profile f(x) = 1. However, this bound is useless when the minimum of f(x) on 12 is zero, and cannot be used to estimate A* for the power-law permittivity profile f(x) = \x\a with a > 0. Therefore, it is desirable to obtain a bound on A* that depends more on the global properties of / . Such a bound was established in [32] and here is a sketch of its proof. (2). Mult iply now (S)\ by 0n ( l — u)2, and integrate the resulting equation over ft to get / \f(j>ndx= / <fo(l -u)2Audx. (2.3.10) Jn Jn Using the identity V • (Hg) = 5V • H + H • Vg for any smooth scalar field g and vector field H, together with the Divergence theorem, we calculate [ \f<pQdx= [ {\-u)24>QS7u-vdS+ J V u - V [ 0 n ( l - w ) 2 ] dx, (2.3.11) Jn Jdn Jn where v is the unit outward normal to 9ft. Since </>n = 0 on 9ft, the first term on the right-hand side of (2.3.11) vanishes. B y calculating the second term on the right-hand side of (2.3.11) we get: / \f(j>o.dx = - f 2(1 - u)4>Q\Vu\2dx + f (1 - u)2Vu • V0ndx (2.3.12a) Jn Jn Jn < - I \V0n • V [(1 - uf] dx. (2.3.12b) Jn 6 The right-hand side of (2.3.12b) is evaluated explicitly by / \f<t>ndx<-\ I (l-u)sW^n-udS-^ f (1 - u)3</>ndx. (2.3.13) Jn 6 Jan 6 Jn For 0 < u < 1, the last term on the right-hand side of (2.3.13) is positive. Moreover, u — 0 on 9ft so that fgn V(J)Q • vdS = —fiQ since fn(t>ndx = 1. Therefore, if (S\) has a solution, then (2.3.13) yields A in This proves that there is no solution for A > A 2 , which gives (2.3.7). >Jf<fadx<!f. (2.3.14) 24 Chapter 2. Pull-in Voltage and Steady-States Remark 2.3.2. The above estimate is not sharp, at least in dimensions 1 < N < 7, as one can show that there exists 1 > a(Cl, N) > 0 such that A < ^ ( l - a ( f i , J V ) ) ( [ ffadx)-1. (2.3.15) Jn Indeed, this follows from inequality (2.3.13) above and Theorem 2.4.5 below where it will be shown that in these dimensions, there exists 0 < C(Q,N) < 1 independent of A such that | | U A| |OO < C(Q,N) for any minimal solution u\. It is now easy to see that a(Cl,N) can be taken to be a{Cl,N) := ( l - C ( f i , i V ) ) 3 / fodx. Jn We now consider problem (S)\ in the case where Q C RN is a strictly star-shaped domain containing 0, meaning that Q. satisfies the additional property that there exists a positive constant a such that x • v > a > 0 for all x G 9 f i , (2.3.16) where v is the unit outer normal to dtt. P r o p o s i t i o n 2.3.3. Suppose f = 1 and that the strictly star-shaped smooth domain C RN satisfies (2.3.16). Then the pull-in voltage A*(Q) satisfies: A V O W A (N + 2)2P(Q) X ( n ) - A a - 8aN\Q\ • ( 2 - 3 ' 1 7 ) where \Q\ is the volume and P(fl) is the perimeter of CI. In particular, ifQ is the Euclidean unit ball in M.N, then we have the bound v o w ) < ^ ± £ . P r o o f : Recall Pohozaev's identity: If u is a solution of A u + Xg(u) = 0 for i 6 l l , u = 0 for x € dQ, then NX [ G(u)dx-^-^X f ug{u)dx = ]- [ {x • v)(-^fdS, (2.3.18) Jn 2 Jn 2 Jdn a v where G(u) = J™ g(s)ds. Applying this with g(u) — JJZ^S a n d G(u) = yields 2ja {l-uf 2jdnK >ydv> a / f u \ 2 a\2 / f dx (2.3.19) 2P(fl) W n ( l - u ) dx y l^ur2) 25 Chapter 2. Pull-in Voltage and Steady-States where we have used the Divergence Theorem and Holder's inequality M2 Since fu(N + 2-2Nu) f r N + 2^2 +{N + 2) 2-, 8N < (N + 2)2 f dx 8N f we deduce from (2.3.19) that (N + 2) 2 > aX la (I dx a\\Cl\ 8N ~ P{Q) Jn (1 - u)2 - P(Q) ' which implies the upper bound (2.3.17) for A*. Finally, for the special case where Q = B\(0) C RN, we have a = 1 and = N and hence the bound A*(Bi(0)) < A 3 = • 2.3.3 N u m e r i c a l e s t i m a t e s for A* In this subsection, we apply numerical methods to discussing the bounds of A*. In the com- putations below we shall consider two choices for the domain ft, ft: [-1/2,1/2] (slab); ft : x2 + y2 < 1 (unit disk). (2.3.20) (a). A* versus a (slab) (b). A* versus a (unit disk) Figure 2.2: Plots of A* versus a for a power-law profile (heavy solid curve) and the exponential profile (solid curve). The left figure corresponds to the slab domain, while the right figure corresponds to the unit disk. 26 Chapter 2. Pull-In Voltage and Steady-States Exponential Profiles: ft a A A* Ai A 2 slab 0 1.185 1.401 1.462 3.290 slab 1.0 1.185 1.733 1.878 4.023 slab 3.0 1.185 2.637 3.095 5.965 slab 6.0 1.185 4.848 6.553 10.50 unit disk 0 0.593 0.789 0.857 1.928 unit disk 0.5 0.593 1.153 1.413 2.706 unit disk 1.0 0.593 1.661 2.329 3.746 unit disk 3.0 0.593 6.091 17.21 11.86 Table 2.1: Numerical values for pull-in voltage A* with the bounds given in Theorem 2.1.1. Here the exponential permittivity profile is chosen as (2.3.21). For the permittivity profile, following [32] we consider slab : f(x) = |2a;|Q (power-law); f{x) = e a ( x 2 - 1 / 4 ) (exponential), (2.3.21a) unit disk : f{x) = |a:| a (power-law); f(x) = e " ( W 2 - i ) (exponential), (2.3.21b) with a > 0. To compute the bounds A i and A 2 , we must calculate the first eigenpair nn and <f>n of —A on ft, normalized by j^(j>n dx = 1, for each of these domains. A simple calculation yields that M n = 7 r 2 - <t>n = | sin [̂ (̂ + ^)J (Slab); (2.3.22a) Ha = z\ « 5.783, <j>n = -^J0(z0\x\) (Unit Disk) . (2.3.22b) Here Jo and J\ are Bessel functions of the first kind, and ZQ « 2.4048 is the first zero of Jo(z). The bounds A i and A 2 can be evaluated by substituting (2.3.22) into (2.1.2b). Notice that A 2 is, in general, determined only up to a numerical quadrature. In Figure 2.2(a) we plot the saddle-node value A* versus a for the slab domain. A similar plot is shown in Figure 2.2(b) for the unit disk. The numerical computations are done using B V P solver C O L S Y S [2] to solve the boundary value problem (S)\ and Newton's method to determine the saddle-node point. Theorem 2.1.1 guarantees a finite pull-in voltage for any a > 0, while A* is seen to increase rapidly with a. Therefore, by increasing a, or equivalently by increasing the spatial extent where f(x) 1, one can increase the stable operating range of the M E M S capacitor. In Table 2.1 we give numerical results for A*, together with the bounds given by Theorem 2.1.1, in the case of exponential permittivity profiles, while Table 2.2 deals with power-law profiles. From Table 2.1, we observe that the bound A i for A* is better than A 2 for small values of a. However, for a ^> 1, we can use Laplace's method on the integral defining A 2 to obtain for the exponential permittivity profile that Ah2 Ai = ^ a , A 2 ~ c 2 a 2 . (2.3.23) 27 Chapter 2. Pull-in Voltage and Steady-States Power-Law Profiles: SI a A c (a) A* Ai A 2 slab 0 1.185 1.401 1.462 3.290 slab 1.0 3.556 4.388 oo 9.044 slab 3.0 11.851 15.189 oo 28.247 slab 6.0 33.185 43.087 oo 76.608 unit disk 0 0.5.93 0.789 0.857 1.928 unit disk 1.0 1.333 1.775 00 3.019 unit disk 5.0 7.259 9.676 00 15.82 unit disk 20 71.70 95.66 00 161.54 Table 2.2: Numerical values for pull-in voltage A* with the bounds given in Theorem 2.1.1. Here the power-law permittivity profile is chosen as (2.3.21). Here b\ = 7r2, CI = 1/4, c 2 = 1/3 for the slab domain, and b\ = z 2 , c\ = 1, c 2 = 4/3 for the unit disk, where ZQ is the first zero of Jo (z) = 0. Therefore, for a ^> 1, the bound A 2 is better than A i . A similar calculation can be done for the power-law profile, see Table 2.2. For this case, it is clear that the lower bound A c (a) in (2.1.4) is better than A in (2.1.2a), and the upper bound Ai is undefined. However, by using Laplace's method, we readily obtain for a 1 that A 2 ~ a 2 / 3 for the unit disk and A 2 ~ 4 a 2 / 3 for the slab domain. Therefore, what is remarkable is that Ai and A 2 are not comparable even when / is bounded away from 0 and that neither one of them provides the optimal value for A*. This leads us to conjecture that there should be a better estimate for A*, one involving the distribution of / in Q., as opposed to the infimum or its average against the first eigenfunction 2.4 The branch of minimal solutions In the rest of this Chapter, we consider issues of uniqueness and multiplicity of solutions for (5)A with 0 < A < A*. The bifurcation diagrams in Figure 2.1 show the complexity of the situation, even in the radially symmetric case. One can see that the number of branches -and of solutions- is closely connected to the space dimension. In this section, we focus on the very first branch of solutions considered to be "minimal". The branch of minimal solutions corresponds to the lowest branch in the bifurcation dia- gram, the one connecting the origin point A = 0 to the first fold at A = A*. To analyze further the properties of this branch, we consider for each solution u of (S)\, the operator L ^ = - A - ( T ^ ( 2 A 1 ) associated with the linearized problem around u. We denote by ni(X, u) the smallest eigenvalue of LUtx, that is, the one corresponding to the following Dirichlet eigenvalue problem - A 0 - ^ ^ , 0 = i 4 x e Q , 0 = 0 x e d f l . (2.4.2a) (1 — u)* 28 Chapter 2. Pull-in Voltage and Steady-States In other words, i n t & { w - » w - . ) - y > * A solution u for (S)\ is said to be stable (resp., semi-stable) if ni(X,u) > 0 (resp., /J,I(\,U) > 0). 2.4.1 Spectral properties of minimal solutions We start with the following crucial lemma, which shows among other things that semi-stable solutions are necessarily minimal solutions. Lemma 2.4.1. Let f be a function satisfying (2.1.1) on a bounded domain Q in RN, and let A* := A*(Q, / ) be as in Theorem (2.1.1). Suppose u is a positive solution of [S)\, and consider any -classical- supersolution v of (S)x, that is, -Av > ,yy > z e f t , (2.4.3a) A/ ( s ) 0 < v(x) < 1 x S ft (2.4.3b) v = 0 xedn. (2.4.3c) If H\{\,u) > 0, then v > u on Q, and if ^\{X,u) = 0, then v = u on Q. P roof : For a given A and x S CI, use the fact that f(x) > 0 and that t —> ̂ {ffia is convex on (0,1), to obtain — A(u + T(V — u)) — . r ^ > 0 1 6 ( 1 , (2.4.4) for T e [0,1]. Note that (2.4.4) is an identity at r = 0, which means that the first derivative of the left-hand side for (2.4.4) with respect to T is nonnegative at r = 0, 2Xf{x) (l-u) v-u = 0, xGdQ. (2.4.5b) A{v - u) - ^ . A 3 {v - u) > 0, x e f t , (2.4.5a) Thus, the maximal principle implies that if ni(\,u) > 0, we have v > u on fi, while if /xi(A,u) = 0, then Lemma 2.16 of [20] gives - A(v - u ) - fX^X\(v-u)=Q xeQ. (2.4.6) (1 — u)6 In the latter case the second derivative of the left-hand side for (2.4.4) with respect to r is nonnegative a r = 0 again, - T ^ ^ i i v - u f ^ O * G f i , (2.4.7) ( l - u ) 4 From (2.4.7) we deduce that v = u in \ QQ> where n 0 = { x e n - . f ( x ) = 0 for x € Q} . (2.4.8) 29 Chapter 2. Pull-in Voltage and Steady-States On the other hand, (2.4.6) reduces to —A(v — u) = 0 x s Q o i v — u = 0 x £ dClo , which implies v = u on CIQ. Hence if /ii(X,u) = 0 then v = u on CI, which completes the proof of Lemma 2.4.1. • T h e o r e m 2.4.2. Assume f is a function satisfying (2.1.1) on a bounded domain CI in M.N, and consider the branch A —> u\ of minimal solutions on (0, A*). Then the following hold: 1. For each x £ CI, the function A —* u\(x) is differentiable and strictly increasing on (0, A*). 2. For each A £ (0, A*), the minimal solution u\ is stable and the function A —> := / ^ I ( A , U A ) is decreasing on (0, A*). P roo f : Consider A i < A 2 < A*, their corresponding minimal positive solutions uXl and u\2 and let u* be a positive solution for (S)\2. For the monotone increasing series {un(Xi;x)} defined in (2.2.10), we then have u* > uo(Ai;:r) = 0, and if un-\(Xi;x) < u* in CI, then - A K - u „ ) = / ( , ) [ I ^ - i r - ^ ] > 0 , x£Cl u* — un = 0, x £ dCl. So we have u„(Ai;a;) < u* in CI. Therefore, uXl = l im , , - ^u n (X i ; x ) < u* in CI, and in particular uXl < u\2 in CI. Therefore, > 0 for all x £ CI. That A —> is decreasing follows easily from the variational characterization of / Z ^ A , the monotonicity of A —•> u\, as well as the monotonicity of (1 — u)~3 with respect to u. Now we define A** = sup {A; UA is a stable solution for (5)A}. It is clear that A** < A*, and to show the equality, it suffices to prove that there is no minimal solution for (5)^ with fi > A**. For that, suppose w is a minimal solution of (S)\*>+5 with 5 > 0, then we would have for A < A**, (i — w)2 (l-wy Since for 0 < A < A** the minimal solutions u\ are stable, it follows from Lemma 2.4.1 that 1 > w > u A for all 0 < A < A**. Consequently, u = l imA /A** wA exists in C x ( f i ) and is a solution for (S)A**- N O W from the definition of A**, we necessarily have ^I ,A** = 0, hence by again applying Lemma 2.4.1, we obtain that w = u and S = 0 on CI, which is a contradiction, and hence A** = A*. Since each u\ is stable, then by setting . F ( A , U A ) := —A — jjz^^p: W E S E T that Fux(X,ux) is invertible for 0 < A < A*. It then follows from the implicit function theorem that ux(x) is differentiable with respect to A. Finally, by differentiating (S)A with respect to A, and since A —> u\(x) is non-decreasing, we get A du* 2A/(s) dux _ fix) ^ n _ dA ( 1 - « J 3 dX ~ ( 1 - u J 2 ^ > o , x£dci. dX 30 Chapter 2. Pull-in Voltage and Steady-States Applying the strong maximum principle, we conclude that > 0 on Q for all 0 < A < A*, and the theorem is proved. • Remark 2.4.1. Lemma 3 of [20] yields /xi(l ,0) as an upper bound for A** - at least in the case where info / > 0 on Q. Since A** = A*, this gives another upper bound for A* in our setting. It is worth noting that the upper bound in Theorem 2.1.1 gives a better estimate, since in the case where / = 1, we have fi{l,0) = nn/2, while the estimate in Theorem 2.1.1 gives for an upper bound. 2.4.2 Energy estimates and regularity We start with the following easy observations. L e m m a 2.4.3. Let f be a function satisfying (2.1.1) on a bounded domain Q in RN. Then, 1. Any (weak) solution u in HQ(Q) of ( S ) \ then satisfies ^lu^dx < oo. 2. / / i n fo / > 0 and N > 3, then any solution u such that f/(l —u) £ L3N/2(Q) is a classical solution. Proof : (1) Since u £ H Q ( Q ) is a positive solution of ( S ) \ , we have Jn (1 - w) 2 Jn 1 - « Jn (1 - " ) 2 Jn which implies that with e > 0. Therefore, by choosing e > 0 small enough, we conclude that Ja ^ l U ) 2 < °o • £ 2N (2) Suppose u is a weak solution such that £ which means that JJ^I L 3 p / 2 ( f t ) . B y Sobolev's theorem we can already deduce that u £ C° ' a ( f i ) with a = 2- ^ . To get more regularity, it suffices to show that u < 1 on fi, but then if not we consider xo £ Cl such that u(x0) = ||tt|]o(Sl) = 1> t n e n we have \1 - u(x)\ = \u(xo) - u(x)\ < C\xo - x\a on Cl. This inequality shows that if p > ^ then we have oo > [ f f{-X\\pdx >C [ \x- x0r3padx = C f \x- x0\-Ndx = oo, 7n ( 1 - w ) 3 Jn Jn a contradiction, which implies that we must have < 1- ' Note that the above argument cannot be applied to the case where f(x) > 0 vanishes on £1, and therefore we have to use the iterative scheme outlined in the next theorem. 31 Chapter 2. Pull-in Voltage and Steady-States Theorem 2.4.4. Let f be a function satisfying (2.1.1) on a bounded domain Q in R N . Then for any constant C > 0 there exists 0 < K(C, N) < 1 such that a positive weak solution u of [S)\ (0 < A < A*) is a classical solution and || u ||c(n)< K(C,N) provided 1. N = land\\T^w\\LHn)<C, 2. N>2and\\T^¥\\LN/2((i)<C. Proof: We prove this theorem by considering the following three cases separately: (1) If N = 1, then for any I > 0 we write using the Sobolev inequality with constant K{1) > 0, K{1) || ( l - ^ - i - l H ^ < / I V K l - u ) " 1 - ! ] ! 2 Jo. = \ [ Vu.V[(l-u)-3-l] 3 J n = U / ( i - U ) - 2 [ ( i - u ) - 3 - i ] J n (2.4.9) < CI + C f 8/(1 -u)~2 J{(l-u)- 3>/} +C [ f[(l- u)~3 + 2(1 - u)-2 + 4(1 - u)-1} [(1 - u)-1 - l ] 2 J{( i -«)" 3 >/} < CI + C + C || (1 - n ) - - 1 | | 2 . ( { ( 1 _ u ) - 3 , / } ) j{ii_u)_3>_n ^ < CI + C + Ce(I) || (1 - u ) " 1 - 1 ||Joe, . with e(I) = / T — ^ . „, where Lemma 2.4.3(1) is applied in the second inequality. 7{(i- u)-s>/} (1 - « ) 3 From the assumption / / ( l - u ) 3 € L 1 ( f t ) , we have e(J) —> 0 as I —> oo. We now choose I such that e(I) < so that the above estimates imply that || (1 — u ) - 1 — 1 | |L°°< K{C). Standard regularity theory for elliptic problems now implies that 1/(1 — u) S C 2 , a ( f i ) . Therefore, u is classical, and there exists a constant K(C, N) which can be taken strictly less than 1 such that II u Hc(n)— K(C,N) < 1. (2) Assuming N = 2, we need to show that (1 - u ) - 1 G L P ( Q ) for any p > 1. (2.4.10) F i x p > 1 and let us introduce TfcU = min {u , 1 — k}, the truncated function of u at level 1 — k, 0 < k < 1. For ft small, we take (1 - T / j u ) - 1 - 1 £ #o(^) 3 5 a t e s t function for {S)y. [ | V r » * | a = / W ( ( 1 _ r f c t t ) - i _ ! ) < / W < C < + o o (2.4.11 32 Chapter 2. Pull-in Voltage and Steady-States Note that the classical consequence of the Moser-Trudinger inequality gives: there exists C > 0 so that J < ? ° < C exp (^\\v\\2Hiia)) Vw G H0\n), p > 1. (2.4.12) Since now log ( r r f ^ ) e #o(^)> (2-4.12) and (2.4.11) now yield that for any p > 1: / n ( l - ^ ) - < C i e x P ( ^ / j V l o g ^ ) , 2 ) < C 2 where C\, C 2 denote positive constants depending only on p and C. Taking the limit as k —> 0 and using that u < 1, we get the validity of (2.4.10). (3) The case when 7Y > 2 is more elaborate, and we first show that (1 — u)~l G L 9 ( f i ) for all q G ( l ,oo). Since u G H Q ( Q ) is a solution of {S)\, we already have JQ ^ j ^ a < C1. Now we proceed by iteration to show that if JQ ^_Jy+2S < C f ° r some # > 0, then / n ^_uyi*(i+e) with 2* = Indeed, for any constant 0 > 0 and £ > 0 we choose a test function 0 = [(1 — u)~3 — 1] min{( l — u)~2e,£2}. By applying this test function to both sides of (S)\, we have A f f(l - u)-2[(l - u)~3 - 1] min{( l - u)~2e, £2} Jn = f V u • V [((1 - u)'3 - 1) min{( l - u)~2e, £2}] n (2.4.13) = 3 / | V u | 2 ( l - u ) - 4 m i n { ( l - u ) - 2 e , ^ 2 } Jn +29 f | V u | 2 ( l - ^ - ^ [ ( l - u)~3 - 1]. J{(i-u)-e<e} We now suppose JQ ^ _ ^ 2 + 2 ^ < C. We then obtain from (2.4.13) and the fact that ^2U)S ^ Ci ( T ^ d i l - ! ) 2 whenever (1 - u)'3 > I > 1 that: 33 Chapter 2. Pull-in Voltage and Steady-States with ^ |V[((1 - w ) - 1 - 1) min{(l - W ) - 0 , f } ] | 2 <2 f | V u | 2 ( l - u ) - 4 m i n { ( l - u ) - 2 V 2 } Jn +262 / | V u | 2 ( l - u)~2e-2 \(1 - u)-1 - l l 2 = 2 / | V u | 2 ( l - u)~4 min{(l - u)~2e, t2} Jn J{(i-u)-<><e} L ( 1 - ' » ) 3 1 - u ( l - i i ) 2 J <CX [ / ( l - w ) - 2 [ ( l - u ) - 3 - l ] m i n { ( l - u ) - 2 9 ^ 2 } Jn <CX f f(l-u)-5mm{{l-u)-2e,e2} Jn <CI + C [ / ( l - u)-5 min{(l - u)-26, t2} J{(l-u)-*>I) <CI + C [ / ( l - u)~3 [(1 - u)-1 - l ] 2 min{(l - u)'26, £2} ^ C I + C \ [ ( 7 1 ^ 3 ) ^ * L^{(l-u)-3>/} J <CI + Ce(I) f ^ [ ( ( l - w ) - 1 - 1 ) m i n { ( l - u ) - V } ] | 2 U ( l - « ) - 3 > / } ( ( l - ^ ) 3 ) (2.4.14) From the assumption / / ( l - u)3 £ L 2 (Q) we have e(J) —> 0 as / -» 00. We now choose J such that e(I) = 2^5, and the above estimates imply that / \V[(l-u)-°-1-(l-u)-e}\2<CI, J{{l-u)-<><e} 34 Chapter 2. Pull-in Voltage and Steady-States where the bound is uniform with respect to i. This estimate leads to < CI + C f (1 - u)-29-3\Wu\ J{(i-u)-e<e} V U | 2 {(l-u)-e<e) ' <CI + C/e + Ce I (I- u)-2e-4\Vu'2 <CI+ f [Ce{l - u)-29'4 + C/e] J {i e<e} Cl / f ( l - u ) - 2 e - 4 | J{{\-u)-l)<l} with e > 0. This means that for e > 0 sufficiently small / Iwii-u)-6-^2 = [ (e + i)2(i-u)-2e-4\vu\2 <c. J{(i-u)-e<e} J{(i-u)-e<e} Thus we can let I —> oo and we get that (1 — u)~e~l G Hl{0.) <—> L 2 * ( 0 ) , which means that / n (i_u)2*(i+8) < C. B y iterating the above argument for 0; + 1 = ^ 5 ( ^ - 1 + 1) for i > 1 and starting with 6»o = 0, we find that 1/(1 - u) G Li(Q) for all g G (1,00). Standard regularity theory for elliptic problems applies again to give that 1/(1 - u) G C 2 , a ( Q ) . Therefore, u is a classical solution and there exists a constant 0 < K(C, N) < 1 such that || u ||C(n)< K(C,N) < 1. This completes the proof of Theorem 2.4.4. • Theorem 2.4.5. For any dimension 1 < N < 7 there exists a constant 0 < C(N) < 1 independent of X such that for any 0 < A < A* the minimal solution u\ satisfies || ux ||c(n)< C(N). Consequently, u* — l im u\ exists in the topology of C 2 , a ( Q ) with 0 < a < 1. It is the unique classical solution for [S)\* and satisfies n\t\*(u*) = 0. This result will follow from the following uniform energy estimate on the minimal solutions ux. Proposition 2.4.6. There exists a constant C(p) > 0 such that for each X G (0, A*), the minimal solution ux satisfies \\^JU ^\\LP{U) ^ a s l°n9 as p < 1 + ̂ + 2 ^ / | . Proof: Since minimal solutions are stable, we have A I , 2^X\^w2dx < - f wAwdx = f \Vw\2dx (2.4.15) Jn(l-uj Jn Jn for all 0 < A < A* and nonnegative w G HQ(Q). Setting w = (1 -uxY - 1 > 0, where -2-VQ<i<0, (2.4.16) then (2.4.15) becomes rJn(l-uxr-2\Wux\2dx>X^2[1 l _ l ^ 2 f i X ) d x . (2-4.17) 35 Chapter 2. Pull-in Voltage and Steady-States On the other hand, multiplying (S)\ by y ^ K l _ ux)2% 1 ~~ 1] a n c ^ a P P l y m § integration by parts yield that . • 2 r [ i _ ( i _ „ A ) 2 i - i ] / ( a ; ) _ /n Hence (2.4.17) and (2.4.18) reduce to ' / n ( i - . ) * - » l v . , | » * - ^ / _Xi2 2% fix) -lJQ(l-u,)2 Jn(l-ux)3 2 ( 1 - « J 2 f f(x) y n ( i - « j 3 - da;. > A(2 + 2i fix) Ux)3-2i dx. From the choice of i in (2.4.16) we have 2 + jfzr > ^- ^ ° (2-4.19) implies that fix) f Haul dx < c f — < C )3-i t da; /3=3? 3-2i . J3^ 3 ( l - u J 3 - i / 3 - 2 dx where Holder's inequality is applied. From the above we deduce that fix) In {I U j 3 - 2 i dx<C. Further we have / Jn fix) ( 1 - « J 3 3-2i 3 dx _ f f=M / ' Jn 3 ' ) 3 - 2 t dx Therefore, we get that where - i n view of (2.4.16)- \3-2i dx<C. ( 1 - U J 3 "LP 3 - 2 i , 4 /2 (2.4.18) (2.4.19) (2.4.20) (2.4.21) (2.4.22) (2.4.23a) (2.4.23b) P r o o f of T h e o r e m 2.4.5: The existence of u* as a classical solution follows from Proposition 2.4.6 and Theorem 2.4.4, as long as y < 1 + | + 2 ^ / | , which happens when N < 7. Since fj,it\ > 0 on the minimal branch for any A < A*, we have the limit M^A* > 0. If now Mi,A* > 0 the implicit function theorem could be applied to the operator Lu^t\*, and would allow the continuation of the minimal branch A i—> ux of classical solutions beyond A*, which is a contradiction, and hence ^ I , A * = 0. The uniqueness in the class of classical solutions then follows from Lemma 2.4.1. • 36 Chapter 2. Pull-in Voltage and Steady-States 2.5 Uniqueness and multiplicity of solutions The purpose of this section is to discuss uniqueness and multiplicity of solutions for (S)\. 2.5.1 Uniqueness of the solution at A = A* We first note that in view of the monotonicity in A and the uniform boundedness of the first branch of solutions, the extremal function defined by u*(x) = l im u\(x) always exists, and can always be considered as a solution for (5)A* in a generalized sense. Now if there exists 0 < C < 1 such that || ux ||c(fi)< C for each A < A* -just like in the case where 1 < N < 7- then we have seen in Theorem 2.4.5 that u* is unique among the classical solutions. In the sequel, we tackle the important case when u* is a weak solution (i.e., in HQ(CI)) of (S)\* but with the possibility that ||«*||oo = 1- Here and in the sequel, u wil l be called a /^(P^-weak solution of (S)\ if 0 < u < 1 a.e. while u solves (S)\ in the weak sense of HQ(CI). We shall borrow ideas from [10, 14], where the authors deal with the case of regular nonlin- earities. However, unlike those papers where solutions are considered in a very weak sense, we consider here a more focussed and much simpler situation. We establish the following useful characterization of the extremal solution. Theorem 2.5.1. Assume f is a function satisfying (2.1.1) on a bounded domain Cl in M.N. For A > 0, consider u £ HQ(CI) to be a weak solution of (S)\ (in the HQ(CI) sense) such that || u ||L°°(fj)= 1- Then the following assertions are equivalent: 1- Mi,A > 0, that is u satisfies / n I W | 2 - / n . f ^ F ^ 2 V * e H ° ( n ) ' ( 2 - 5 ' 1 } 2. A = A* and u = u*. We need the following uniqueness result. Proposition 2.5.2. Assume f is a function satisfying (2.1.1) on a bounded domain Cl in WLN. Let u\, U2 be two HQ(Cl)-weak solutions of(S)\ so that nxt\(ui) > 0 for i = 1,2. Then u\ = u2 almost everywhere in Cl. Proof: For any 9 € [0,1] and <p £ H^(Cl), 4> > 0, we have that = A i / ( I ) ( ( T ^ 7 + W ^ ? - (i - «„, - a - " 0 due to the convexity of 1/(1 — u)2 with respect to u. Since I Q ^ = = 0, the derivative of Ie,<j, at 6 = 0,1 provides / V ( « l - « 2 ) V 0 - [ ^ ^ K - ^ ^ O , Jn Jn (1 - U2) f V ( « i - U 2 ) V 0 - / '2Xf{x)Ju1-U2)^<0 Jn Jn (1 - ui) 37 Chapter 2. Pull-in Voltage and Steady-States for any <p G H Q ( Q , ) , <f> > 0. Testing the first inequality on (f> = (u\ — u2) and the second one on (ui — u2)+, we get that Jn [ | V h - n2)-f - ( n r § 5 « « l - » 2 ) " ) 2 ] < 0 , Since /UI,A(UI) > 0, we have 1) either /XI,A(UI) > 0 and then u\ < u2 a.e., 2) or u-it\(u\) = 0, which then gives / V ( u i - u2)V<A - / , 2 A / ( a r i 3 ( m - ^2)0 = 0 (2.5.2) Jn (1 — ui) where 0 = (ui - u 2 ) + . Since Iej > 0 for any 9 € [0,1] and = del^ = 0, we get that: Let Z0 = {x G ft : / ( x ) = 0}. Clearly, (m - u2)+ = 0 a.e. in ft \ Z0 and, by (2.5.2) we get: | V ( u i - u 2 ) + | 2 = 0. / Jn Hence, u i < u 2 a.e. in ft. The same argument applies to prove the reversed inequality: u 2 < u\ a.e. in ft. Therefore, u i = u2 a.e. in ft, and the proof is complete. • Since || u\ ||< 1 for any A G (0,A*), we need - i n order to prove Theorem 2.5.1- only to show that (5)A does not have any .ffo(ft)-weak solution for A > A*. B y the definition of A*, this is already true for classical solutions. We shall now extend this property to the class of weak solutions by means of the following result. P r o p o s i t i o n 2.5.3. Ifw is a Hl{£l)-weak solution of (S)\, then for any e G (0,1) there exists a classic solution w£ of (S)\(x-Sy Proo f : First we prove that for any ip G C 2([0,1]) concave function so that ip(0) = 0, we have that f ViP(w)\7<p> f A / J ( « > ) y (2.5.3) Jn Jn (1 - wY for any ip G HQ(Q), tp > 0. Indeed, by concavity of ip we get: / Vip{w)Vtp= / ip{w)VwWip= / WwW(ip(w)tp) - / ip\w)ip\V Jn Jn , , Jn v ' Jn ' A / (x) w\2 Jn ( 1 - u ; ) 2 for any tp G C§°(ft), <p > 0. B y density, we get (2.5.3). 38 Chapter 2. Pull-In Voltage and Steady-States Now let e G (0,1), and define V > e M : = l - ( e + ( l - e ) ( l - t o ) 3 ) 5 , 0 < w < 1. Since ip£ G C 2([0,1]) is a concave function, ip£(0) = 0 and V > e H = ( l - e ) ' , 5 ( 5 ) : = ( 1 - S ) - 2 , ' by (2.5.3) we obtain that for any <p G HQ(CI), tp > 0: / V ^ W V ^ > / A / ( a ) ^ H y = A ( l - e ) / mgiMw))? Ja Ja (1 - ™) Jn = / A ( l - £ ) / ( * ) n ( 1 - V e H ) 2 ^ ' Hence, ipe(w) is a iJo(ft)-weak supersolution of (S)x(i-e) so that 0 < i>£{w) < 1 — £3 < 1. Since 0 is a subsolution for any A > 0, we get the existence of a i?Q(ft)-weak solution we of (5) A (i_ £ ) so that 0 < we < 1 — £ 3 . B y standard elliptic regularity theory, we is a classical solution of (S)x(i-e)- ' 2.5.2 Uniqueness of low energy solutions for small voltage In the following we focus on the uniqueness when A is small enough. We first define nonminimal solutions for (S)\ as follows. D e f i n i t i o n 2.5.1. A solution 0 < u < 1 is said to be a nonminimal positive solution of (S)\, if there exists another positive solution v of [S)\ and a point i £ ( l such that u(x) > v(x). L e m m a 2.5.4. Suppose u is a nonminimal solution of (S)\ with A G (0, A*). Then fii(X,u) < 0, and the function w = u — u\ is in the negative space of LUt\ = —A — 2^l^l • Proo f : For a fixed A G (0, A*), let ux be the minimal solution of [S)\. We have w = u — ux > 0 in ft, and X(2-u-ux)f n . „ -Aw- v X \ 2 W = 0 m Q -(1 -u)2{l - u x y Hence the strong maximum principle yields that ux < u in ft. Let fto = {x G ft : f{x) = 0} and ft/ft0 = {x G ft : f(x) > 0}. Direct calculations give that -A(u - ux) - -^{u - ux) 2Xf (1-u)3 i i 2 / 0 , x G f t 0 ; ( 2 - 5 . 4 ) From this we get (Lu,,w, W) = X 1 ^ f [ ^ - L ^ - - ^ ^ ( u - u J ] (u - ux)< 0. (2.5.5) 39 Chapter 2. Pull-in Voltage and Steady-States Now we are able to prove the following uniqueness result. Theorem 2.5.5. For every M > 0 there exists 0 < \\{M) < A* such that for A G (0, \\{M)) the equation (S)\ has a unique solution v satisfying 1- 11 (i-^,)3 111 ^ M and the dimension N = 1, 2. || ( 1/„)311 i+ e < M for some e > 0 and N = 2, 3- 1 1 ( 1 ^ 1 1 ^ / 2 < M andN>2. Proof: For any fixed A G (0, A*), let ux be the minimal solution of (S)\, and suppose {S)\ has a nonminimal solution u. The preceding lemma then gives This implies in the case where N > 2 that ^ ( 7 n i i i ^ i * ) * ( / n < - ^ ) J S ' (u-ux)*^dx) , which is a contradiction if A < C ^ unless u = u . . If iV = 1, then we write 2 M W C ( l ) | | ( « - ux)\t < A £ T f T ^ s - « J 2 ^ < 2A||(u - u j ^ ^ T f T ^ • and the proof follows. A similar proof holds for dimension N = 2. • Remark 2.5.1. The above gives uniqueness for small A among all solutions that either stay away from 1 or those that approach i t slowly. We do not know whether, i f A is small enough, any positive solution v of (S)\ satisfies fQ(l — v) 5~dx < M for some uniform bound M independent of A. Numerical computations do show that we may have uniqueness for small A -at least for radially symmetric solutions- as long as AT > 2. 2 . 5 . 3 S e c o n d s o l u t i o n s a r o u n d t h e b i f u r c a t i o n p o i n t Our next result is quite standard. Lemma 2.5.6. Suppose there exists 0 < C < 1 such that \\ ux ||C(ft)< C for each A < A*. Then there exists 5 > 0 such that the solutions of (S)\ near (X*,ux.) form a curve p(s) = {(A(s),u(s)) : |s| < 6}, and the pair (X(s),v(s)) satisfies A(0) = A*, A'(0) = 0, A"(0) < 0, and u(0) = ux., v'(0){x) > 0 in ft. (2.5.6) 40 Chapter 2. Pull-in Voltage and Steady-States In particular, if 1 <N <7, then for A close enough to A* there exists a unique second branch U\ of solutions for [S)\, bifurcating from u*, such that Hi,\{Vx)<Q while ti2,x(Ux)>0. (2.5.7) P roof : The proof is similar to a related result of Crandall and Rabinowitz (cf. [19, 20]), so we wil l be brief. First, the assumed upper bound on ux in C1 and standard regularity theory show that if / e C(ft) then || ux | | c 2 , a { f l ) < C < 1 for some 0 < a < 1 (while if / € L°°, then II u \ l l c i Q ( f l ) — C < ^ Allows that {(A,u A )} is precompact in the space R x C2'a, and hence we have a limiting point (A*, ux,) as desired. Since ^_{}X^2 is nonnegative, Theorem 3.2 of [19] characterizes the solution set of (S)\ near (A*,u A»): A(0) = A*, A'(0) = 0, vjfi) = ux, and v'(0) > 0 in ft. The same computation as in Theorem 4.8 in [19] gives that A"(0) < 0. In particular, if 1 < N < 7 then our Theorem 4.5 gives the compactness of u* = ux,, and the theory of Crandall and Rabinowitz in [20] then implies that, for A close enough to A*, there exists a unique second branch U\ of solutions for (S)\, bifurcating from u*, such that HiAUx) < 0 while H2,x{Ux) > 0. • Remark 2.5.2. A version of these results wil l be established variationally in next Chapter. Indeed, we shall give there a variational characterization for both the stable and unstable solutions u\,U\ in the following sense: For 1 < N < 7, there exists 5 > 0 such that for any A € (A* — 5, A*), the minimal solution u\ is a local minimum for some regularized energy functional J E < \ on the space HQ(Q), while the second solution U \ is a mountain pass for the functional J £ I \ . 2.6 Radially symmetric case and power-law profiles In this section, we discuss issues of uniqueness and multiplicity of solutions for (S)\ when Q is a symmetric domain and when / is a radially symmetric permittivity profile. Here, one can again define the corresponding pull-in voltage A*(0 , / ) requiring the solutions to be radially symmetric, that is A*(ft, / ) = sup {A; (S)\ has a radially symmetric solution}. P r o p o s i t i o n 2.6.1. Let Q be a symmetric domain and let f be a nonnegative bounded radially symmetric permittivity profile on Q. Then the minimal solutions of(S)\ are necessarily radially symmetric and consequently A*(ft, / ) = A*(ft, / ) . Moreover, if ft is a ball, then any radial solution of (S)\ attains its maximum at 0. Proof : : It is clear that A*(ft , /) < A*(ft , / ) , and the reverse wil l be proved if we establish that every minimal solution of (S)\ with 0 < A < A*(ft , /) is radially symmetric. But this is a straightforward application of the recursive scheme defined in Theorem 2.2.2 which gives a radially symmetric function at each step and therefore the resulting limiting function -which is the minimal solution- is radially symmetric. For any radially symmetric u(r) of (S)\ defined in the ball of radius R, we have ur(0) = 0 and _ U r r _ U r = _ _ _ i n (0,fl), 41 Chapter 2. Pull-in Voltage and Steady-States Multiplying by r ^ - 1 , we get that - ^ = \{ r - u )* ^ °> a n d therefore ur < 0 in (0,R) since uT(0) = 0. This shows that u(r) attains its maximum at 0. • The bifurcation diagrams shown in the introduction actually reflect the radially symmetric situation, and our emphasis in this section is on whether there is a better chance to analyze mathematically the higher branches of solutions in this case. Now some of the classical work of Joseph-Lundgren [43] and many that followed can be adapted to this situation when the permittivity profile is constant. However, the case of a power-law permittivity profile f(x) = \x\a defined in a unit ball already presents a much richer situation. We now present various analytical and numerical evidences for various conjectures relating to this case, some of which will be further discussed in Chapter 3. Power-law permittivity profiles Consider the domain ft to be a unit ball JBi(O) C RN (N > 1), and let f(x) = \x\a {a > 0). We analyze in this case the branches of radially symmetric solutions of (S)\ for A € (0, A*]. In this case, (S)\ reduces to N - 1 Xra -ur = 0 < r < 1, r (1 - u ) 2 u ' ( 0 ) = 0 , u( l ) = 0. Here r = |a;| and 0 < u = u(r) < 1 for 0 < r < 1. Looking first for a solution of the form u{r) = 1 - (3w(P) with P = jr, where 7 , (3 > 0, equation (2.6.1) implies that (2.6.1) N - l 7 2 / % " + V ^ ' ) = XPa 1 P ~ ' (32ja w2 ' We set w(0) = 1 and A = f2+a(33. This yields the following initial value problem: w" + N - l pa W 1 ' P > 0 , (2.6.2) «/(0) = 0 , io(0) = 1. Since u(l) = 0 we have (3 = l/wij). Therefore, we conclude that u(0) = 1 (2.6.3) A i u 3 (7 ) ' where 1^(7) is a solution of (2.6.2). As was done in [50], one can numerically integrate the initial value problem (2.6.2) and use the results to compute the complete bifurcation diagram for (2.6.1). We show such a computation of u(0) versus A defined in (2.6.3) for the slab domain (N = 1) in Figure 2.3. In 42 Chapter 2. Pull-In Voltage and Steady-States this case, one observes from the numerical results that when N = 1, and 0 < a < 1, there exist exactly two solutions for (S)\ whenever A e (0,A*). On the other hand, the situation becomes more complex for a > 1 as u(0) —> 1. This leads to the question of determining the asymptotic behavior of w(P) as P —> oo. Towards this end, we proceed as follows. N i l a n d t(x) — |x|™ with different r a n g e s of c Figure 2.3: Plots of u(0) versus A for profile f(x) — \x\a (a > 0) defined in the slab domain (N = 1). The numerical experiments point to a constant a* > 1 (analytically given in (2.6.10)) such that the bifurcation diagrams are greatly different for different ranges of a: 0 < a < 1, 1 < a < a* and a > a*. Setting rj = logP and w(P) — PBV{ri) > 0 for some positive constant J5, we obtain from (2.6.2) that 3 Q - 2 B po-iyii + ( 2 B + N _ 2)P*- Z V' + B(B + N- 2)Pa~lV = —^T Choosing B - 2 = a - 2B so that B = (2 + a) /3, we get that 3AT + 2 o - 2 , (2 + a)(3N + a-A) J_ v + 3 "I" 9 y 2 - We can already identify from this equation the following regimes. Case 1. Assume that N = 1 and 0 < a < 1. (2.6.4) (2.6.5) (2.6.6) In this case, there is no equilibrium point for (2.6.5), which means that the bifurcation diagram vanishes at A = 0, from which one infers that in this case, there exist exactly two solutions for A € (0, A*) and just one for A = A*. Case 2. N and a satisfy either one of the following conditions: JV = 1 and a > 1, N > 2. (2.6.7a) (2.6.7b) 43 Chapter 2. Pull-In Voltage and Steady-States There exists then an equilibrium point Ve of (2.6.5) which must be positive and satisfies V3 = ? , . (2 + a)(3iV + a - 4 ) Linearizing around this equilibrium point by writing V = V e + Cear}, 0 < C « 1 , we obtain that This reduces to with 2 3iV + 2 a - 2 (2 + a)(3iV + a - 4 ) 7 + 3 * + § = 0 - 3N + 2a - 2 " . cr ± = ± Z— , (2.6.9a) 6 6 A = - 8 a 2 - (24JV - 16)a + (9JV2 - 84JV + 100). (2.6.9b) We note that cr± < 0 whenever A > 0. Now define 1 1 [27 „ 4 - 6 ^ + 3 ^ ( ^ - 2 ) / A r ^ „ , , N 2 + 2 V T ' 4 ( ^ ^ 8 ) . (2.6.10) Next, we discuss the ranges of 7Y and a such that A > 0 or A < 0. Case 2. A. N and a satisfy either one of the following: N = 1 with 1 < a < a*, (2.6.11a) N > 8 with 0 < a < a** . (2.6.11b) In this case, we have A > 0 and / 9 \ 1 „ 3N+2a-2-*/K _ M ( 2 + « ) ( 3 N + « - 4 ) ) + ^ ^ + " "< ™ Further, we conclude that _ 2+q / 9 \ 1 „ „ JV -2 i y/E — P " ( ( 2 + a)(3iV + a - 4 ) ) & S In both cases, the branch monotonically approaches the value 1 as r\ —> +oo. Moreover, since A = 7 2 + a / w 3 ( 7 ) , we have (2 + a)(3AT + a - 4 ) A ~ A* = -^—^ as 7—>oo, (2.6.12) which is another important critical threshold for the voltage. In the case (2.6.11a) illustrated by Figure 2.3, we have A* < A*, and the number of solutions increase but remains finite as A approaches A*. On the other hand, in the case of (2.6.116) 44 Chapter 2. Pull-in Voltage and Steady-States illustrated by Figure 2.4, we have A* = A*, and there seems to be only one Case 2.B. N and a satisfy any one of the following three: N = 1 with a> a* , 2<N<7 with a > 0, N > 8 with a>a**. Figure 2.4: Top figure: Plots ofu(0) versus A for 2 < N < 7, where u(0) oscillates around the value A» defined in (2.6.12) and u* is regular. Bottom figure: Plots o/u(0) versus A for N > 8: when 0 < a < a**, there exists a unique solution for (S)\ with A € (0, A*) and u* is singular; when a > a**, u(0) oscillates around the value A* defined in (2.6.12) and u* is regular. In this case, we have A < 0 and V ~ ((2 + a ) W + a - 4)) ' + ^ - ^ - ( f f i + < » ) + - - I - — branch of solutions. (2.6.13a) (2.6.13b) (2.6.13c) 45 Chapter 2. Pull-In Voltage and Steady-States We also have for P —* + 0 0 , " ~ P " ( p + « ) ( W + . - 4 ) ) ' + O t P - ^ < ^ o 9 P + <*) + . . . , (2.6.14) and from the fact that A = "f2+a/to3 (7) we get again that . . (2 + a)(3iV + a - 4 ) A ~ A* = ^—^ as 7 —> 0 0 . Note the oscillatory behavior of w(P) in (2.6.14) for large P, which means that u(0) is expected to oscillate around the value A* = (2+a)(3^+a"~4) as P —> 00. The diagrams below point to the existence of a sequence {Aj} satisfying Ao = 0, A 2 f c . / A* as fc —> 0 0 ; A i — A* , A2fe_i \ A* as fc —> 00 and such that exactly 2fc + 1 solutions for (S)\ exist when A € (A 2£, A2fc+2), while there are exactly 2fc solutions when A € (A2fc+i, A 2fc_i). Furthermore, (S)A has infinitely multiple solutions at A = A*. The three cases (2.6.13a), (2.6.136) and (2.6.13c) considered here for N and a are illustrated by the diagrams in Figure 2.3, Figure 2.4(a) and Figure 2.4(b), respectively. We now conclude from above that the bifurcation diagrams show four possible regimes -at least if the domain is a ball: A . There is exactly one branch of solution for 0 < A < A*. This regime occurs when N > 8, and if 0 < a < a**(N) := 4 ~ 6 J V + 3 / 5 ( J V ~ 2 ) • The results of this section actually show that in this range, the first branch of solutions "disappears" at A* which happens to be equal t o A . ( a , W ) = ( 2 + a > < V + " ~ 4 ) - B . There exists an infinite number of branches of solutions. This regime occurs when • AT = 1 and a > a* := - \ + ^ 2 7 / 2 . • 2 < N < 7 and a > 0; . N > 8 and a > a**(N) := * - ™ + * f { » - i ) . In this case, A»(a, N) < A* and the multiplicity becomes arbitrarily large as A approaches -from either side- A*(a, A'') at which there is a touchdown solution u (i.e., || u ||oo= 1)- C. There exists a finite number of branches of solutions. In this case, we have again that Xt{a,N) < A*, but now the branch approaches the value 1 monotonically, and the number of solutions increase but remains finite as A approaches A»(a, N). This regime occurs when JV = 1 and 1 < a < a* := - \ + \yj27/2. D. There exist exactly two branches of solutions for 0 < A < A* and one solution for A = A*. The bifurcation diagram vanishes when it returns to A = 0. This regime occurs when N = 1 and 0 < a < 1. Some of these questions will be considered in Chapter 3. A detailed and involved analysis of compactness along the unstable branches wil l be discussed there, as well as some information about the second bifurcation point. 46 Chapter 3 Compactness along Lower Branches 3.1 Introduction In this Chapter we continue the analysis of the problem A/fx) . n -Au = , ' in ft, (l — uy 0 < u < 1 in ft, u = 0 on 9ft, where A > 0 is a parameter, ft C RN is a bounded smooth domain and / satisfies (2.1.1). Following the notations and terminology of Chapter 2, the solutions of (S)\ are considered to be in the classical sense, and the minimal solution u\ of (S)\ is the classical solution of (S)\ satisfying u\(x) < u(x) in ft for any solution u of (S)\. There already exist in the literature many interesting results concerning the properties of the branch of semi-stable solutions for Dirichlet boundary value problems of the form —Au = \h(u) where h is a regular nonlinearity (for example of the form eu or (1 + u)p for p > 1). See for example the seminal papers [20, 43, 44] and also [15] for a survey on the subject and an exhaustive list of related references. The singular situation was considered in a very general context in [48], and this analysis is completed in Chapter 2 to allow for a general continuous permittivity profile / (x ) > 0. Fine properties of steady states -such as regularity, stability, uniqueness, multiplicity, energy estimates and comparison results- are shown there to depend on the dimension of the ambient space and on the permittivity profile. Now for any solution u of (S)\, one can introduce the linearized operator at u defined by: A 2A/(x) and its corresponding eigenvalues {nk,\{u)\ k = 1,2,...}. Note that the first eigenvalue is simple and is given by: HiiX(u) = inf | ( L U | A 0 , 4 > ) H i { n ) ; <P e Co°(n), jT |<£(x)| 2dx = 1 with the infimum being attained at a first eigenfunction <j>i, while the second eigenvalue is given by the formula: / i 2 , A (u) = inf | (£u ,A0!0)#i ( f}) ; <P S Cg°(fi), j f |^(x) | 2 dx = 1, jT 4>{x)<j>i(x)dx = 0 This construction can then be iterated to obtain the fc-th eigenvalue Hkt\{u) with the convention that eigenvalues are repeated according to their multiplicities. 47 Chapter 3. Compactness along Lower Branches The usual analysis of the minimal branch (composed of semi-stable solutions) is extended in Chapter 2 to cover the singular situation (S)\ above - best illustrated by the following bifurcation diagram- is obtained. Figure 3.1: Top figure: plots of u(0) versus A for the case where f(x) = 1 is defined in the unit ball Bi(0) C RN with different ranges of dimension N, where we have A* = (6yV — 8)/9 for dimension N > 8. Bottom figure: plots of u(0) versus A for the case where f(x) = 1 is defined in the unit ball B\(Q) C RN with dimension 2 < N < 7, where A* (resp. X2) is the first (resp. second) turning point. One can recognize from Chapter 2 a clear distinction - i n techniques and in the available results- between the case where the permittivity profile / is bounded away from zero, and where it is allowed to vanish somewhere. A test case for the latter situation -that has generated much interest among both mathematicians and engineers- is when we have a power-law permittivity profile f(x) = |a;|Q (a > 0) on a ball. Our first goal of this Chapter is the study of the effect of power-like permittivity profiles f(x) ~ \x\a for the problem (S)x on the unit ball B = B i (0) . We extend Theorem 2.1.2 to higher dimensions: T h e o r e m 3.1.1. Assume N > 8 and a > aN = 3N~™~£^ • Let f G C(B) be such that: f(x) m i with different r a n g e s of N f{x) = \x\ag(x), g(x) >C>0inB. (3.1.1) 48 Chapter 3. Compactness along Lower Branches Let (Xn)n be such that Xn —• A € [0, A*] andun be a solution of(S)\n so that fi\in := /ii,A n(wn) > 0. Then, sup || un ||oo< 1. In particular, the extremal solution u* = l im u\ is a solution of {S)\* satisfying u.\t\* (u*) = 0. As to non-minimal solutions, it is also shown in Chapter 2 -following ideas of Crandall- Rabinowitz [20]- that, for 1 < N < 7, and for A close enough to A*, there exists a unique second branch U\ of solutions for (S)\, bifurcating from u*, such that HiAUx) < 0 while ii2,x{Ux) > 0. (3.1.2) For N > 8 and a > a^, the same remains true for problem (S)\ on the unit ball with f{x) as in (3.3.1) and U\ is a radial function. In the sequel, we try to provide a rigorous analysis for other features of the bifurcation diagram, in particular the second branch of unstable solutions, as well as the second bifurcation point. But first, and for the sake of completeness, we shall give a variational characterization for the unstable solution U\ in the following sense: T h e o r e m 3.1.2. Assume f is a non-negative function in C(Cl) where Q. is a bounded domain in R N . If 1 < N < 7, then there exists 6 > 0 such that for any X 6 (A* — 5, A*), the second solution U\ is a Mountain Pass solution for some regularized energy functional Je\ on the space HQ(£1). Moreover, the same result is still true for N > 8 provided fl is a ball, and f(x) is as in (3.3.1) with a > aw. We are now interested in continuing the second branch t i l l the second bifurcation point, by means of the implicit function theorem. For that, we have the following compactness result: T h e o r e m 3.1.3. Assume 2 < N < 7. Let f £ C{Cl) be such that: k fix) = (J[\x-pi\ai)g{x), g(x)>C>0inn, (3.1.3) i=i for some points pi € Q and exponents ai > 0. Let (Xn)n be a sequence such that Xn —-> A S [0, A*] and let un be an associated solution such that ^ 2 , n : = ( U 2 , A n ( « n ) > 0. (3.1.4) Then, sup || un lloo*^ 1. Moreover, if in addition fJ>\tn '•— Mi,A n(w«) ^ 0» then necessarily A > 0. Let us remark that the case ct\ = • • • = ak = 0 in (3.1.3) corresponds to a function f(x) bounded away from zero.We also mention that Theorem 3.1.3 yields another proof -based on a blow-up argument- of the compactness result for minimal solutions established in Chapter 2 by means of some energy estimates, though under the more stringent assumption (3.1.3) on f(x). We expect that the same result should be true for radial solutions on the unit ball for N > 8, a > a N , and / € C(Cl) as in (3.3.1). 49 Chapter 3. Compactness along Lower Branches As far as we know, there are no compactness results of this type in the case of regular nonlinearities, marking a substantial difference with the singular situation. Theorem 3.1.3 is based on a blow up argument and the knowledge of linear instability for solutions of a limit problem on RN, a result which is interesting in itself (see for example [16]) and which somehow explains the special role of dimension 7 and a — for this problem. Theorem 3.1.4. Assume that either 1 < N < 7 and a > 0 or that N > 8 and a > a^. Let U be a solution of AU = ! g £ in R " , U{y) > C > 0 inRN. Then, U is linearly unstable in the following sense: m(U) = inf | j T^ ( | V 0 | 2 - ^<P2)dx; 4> € C?(RN), 4> 2 = 1 j < 0. (3.1.6) Moreover, if N > 8 and 0 < a < a^, then there exists at least a solution U of (3.1.5) such that m(U) > 0, given by the limit as X —• A* of suitable rescaling of the minimal solution u\ of (S)\ on the unit ball with f(x) = \x\a. Theorem 3.1.4 is the main tool to control the blow up behavior of a possible non compact sequence of solutions. The usual asymptotic analysis for equations with Sobolev critical non- 2N linearity, based on some energy bounds (usually LN~2 (Q)-bounds), does not work in our con- 3/v* text. In view of Chapter 2, a possible loss of compactness can be related to the I/"2~(ft)-norm along the sequence. Essentially, the blow up associated to a sequence un (in the sense of the blowing up of (1 — un)~l) corresponds exactly to the blow up of the L~ (Q)-norm. We replace these energy bounds by some spectral information and, based on Theorem 3.1.4, we provide an estimate of the number of blow up points (counted with their "multiplicities") in terms of the Morse index along the sequence. We now define the second bifurcation point in the following way for (S)\: X*2 = inf{/? > 0 : 3 a curve Vx £ C([/3, A*]; C 2 (Q) ) of solutions for (5) A s-t. H2,\(VX) >0,VX = C/AVA e (A* - 6,X*)}. We then have the following multiplicity result. Theorem 3.1.5. Assume f G C(Q) to be of the form (3.1.3). Then, for 2 < N < 7 we have that X2 G (0, A*) and for any X G (A2, A*) there exist at least two solutions u\ and Vx for {S)x, so that l * i A v > ) < 0 W H I L E M2,A(VA) > 0. In particular, for X = X2, there exists a second solution, namely V* := l im Vx so that M i , A 5 ( 0 < P and ^ ( V * ) = 0 . One can compare Theorem 3.1.5 with the multiplicity result of [1] for nonlinearities of the form Xuq + up (0 < q < 1 < p), where the authors show that for p subcritical, there exists a second 50 Chapter 3. Compactness along Lower Branches -Mountain Pass- solution for any A G [0, A*). On the other hand, when p is critical, the second branch blows up as A —> 0 (see also [4] for a related problem). We note that in our situation, the second branch cannot approach the value A = 0 as illustrated by the bifurcation diagram above. Now let V\, A G A*) be one of the curves appearing in the definition of A^. By (3.1.2), we have that Lyx,x i s invertible for A G (A* — S, A*) and, as long as it remains invertible, we can use the implicit function theorem to find V\ as the unique smooth extension of the curve U\ (in principle U\ exists only for A close to A*). We now define A** in the following way A** = i n f {/3 > 0 : VA G (/?, A*) 3 V A solution of ( S ) A so that M2,A(VA) > 0, VX = Ux for A e (A* - 6,\*)}. Then, Aj < A** and there exists a smooth curve V\ for A G (A**, A*) so that Vx is the unique maximal extension of the curve U\. This is what the second branch is supposed to be. If now Aj < A**, then for A G (A2, A**) there is no longer uniqueness for the extension and the "second branch" is defined only as one of potentially many continuous extensions of U\. It remains open the problem whether A?! is the second turning point for the solution diagram of [S)\ or if the "second branch" simply disappears at A = Aj . Note that if the "second branch" does not disappear, then it can continue for A less than A2 but only along solutions whose first two eigenvalues are negative. In dimension 1, we have a stronger but somewhat different compactness result. Recall that Hk,xn{un) i s the k—th eigenvalue of LUnt\n counted with their multiplicity. Theorem 3.1.6. Let I be a bounded interval in R and f G Cl(I) be such that f > C > 0 in I. Let (un)n be a solution sequence for (S)\n on I, where Xn —* A G [0, A*]. Assume that for any n G N and k large enough, we have: Vk,n •'= Vk,\n(un) > 0. (3.1.7) If A > 0, then again sup || un ||oo< 1 and compactness holds. raeN Even in dimension 1, we can still define A2 but we don't know when \\ = 0 (this is indeed the case when f{x) = 1, see [56]) or when A2 > 0. In the latter situation, there would exist a solution V * for [S)\* which could be - i n some cases- the second turning point. Let us remark that the multiplicity result of Theorem 3.1.5 holds also in dimension 1 for any A G (A£, A*). This Chapter is organized as follows. In §3.2 we provide the Mountain Pass variational characterization of U\ for A close to A* as stated in Theorem 3.1.2. The compactness result of Theorem 3.1.1 on the unit ball is proved in §3.3. §3.4 is concerned with the compactness of the second branch of {S)\ as stated in Theorem 3.1.3. In §3.5 we give the proof of the multiplicity result in Theorem 3.1.5. §3.6 deals with the dimension 1 of Theorem 3.1.6. 3.2 Mountain Pass solutions This section is devoted to the variational characterization of the second solution U\ of {S)\ for A | A* and in dimension 1 < N < 7. Let us stress that the argument works also for problem (S)\ on the unit ball with f(x) in the form (3.3.1) provided N > 8, a > a^. 51 Chapter 3. Compactness along Lower Branches Since the nonlinearity g(u) = JJZ^I is singular at u = 1, we need to consider a regularized C 1 nonlinearity ge(u), 0 < e < 1, of the following form: u < 1 - £ , * < « > H 1 " 2 ( 1 - * ) 2 , _ (3- 2- 1) p £ J pei{l — e)p 1 where p > 1 if iV = 1,2 and 1 < p < $ ± § if 3 < AT < 7. For A G (0,A*), we study the regularized semilinear elliptic problem: { —Au = Xf(x)gE(u) in ft, u = 0 on 9ft. (3.2.2) From a variational viewpoint, the action functional associated to (3.2.2) is Je,\{u) = \ I \Vu\2dx - A / f(x)Ge(u)dx, u G Hl{9) , (3.2.3) /"" where Ge(u) = / gc(s)ds. J —oo In view of Theorem 2.4.5, we now fix 0 < £ < 1~H^*H°°. For A f A*, the minimal solution u\ of (5) A is still a solution of (3.2.2) so that /zi( — A — \f{x)g's(u\)) > 0. The proof of existence of second solutions for (3.2.2) relies on the standard Mountain Pass Theorem [3]. For selfcontainedness, we include this theorem as follows: M o u n t a i n Pass T h e o r e m : Suppose C 1 functional J£,\{u) defines on a Banach space E satisfying (P.S.) conditions and 1. there exists a neighborhood U of u\ in E and a constant a > 0 such that JElx(vi) ^ ^ E , A ( ^ A ) + o- for all v\ G dU; 2. 3v2 & U such that Je,\(v2) < Je,x{u\)- Define then r = { 7 e C ( [ 0 , l ] , t f ) : 7 (0) = «A, 7(1) = " 2 } c £ ) A = inf max { J ^ f r W ) = * G (0,1) } is a critical value of JEt\. We next briefly sketch the proof of Theorem 3.1.2 as follows. First, we prove that u\ is a local minimum for JE,\{u) for A | A*. Then, by Mountain Pass Theorem, we show the existence of a second solution Ue>\ for (3.2.2). Using subcritical growth: 0 < ge{u) < C e ( l + \u\p) (3.2.4) and applying the inequality: 9Ge{u) < ugE{u) for u > M£, (3.2.5) 52 Chapter 3. Compactness along Lower Branches for some C£, M£ > 0 large and 9 = ^ > 2, we obtain that J£ x satisfies the Palais-Smale condition and, by means of a bootstrap argument, we get the uniform convergence of U£iX. On the other hand, a similar proof as in §2.4.1 shows that the convexity of g£{u) ensures that problem (3.2.2) has the unique solution u* at A = A*, which then allows us to deduce that U£,X —> u* in C(ft) as A t A*, and it implies U£>x < 1 — e. Therefore, U£t\ is a second solution for (S)\ bifurcating from u*. But since £/ £ ) A is a M P solution and since (S)x has exactly two solutions (cf. Lemma 2.5.6) u\, U\ for A | A*, it finally yields that U£t\ = U\. In order to complete the details for the proof of Theorem 3.1.2, we first need to show the following: L e m m a 3.2.1. For A ] A*, the minimal solution u\ of (S)x is a local minimum of J£\ on Proof : First, we show that u\ is a local minimum of J £ ] A m Cl(Cl). Indeed, since Mi,A := AH ( - A -\f{x)g' £(u x)) > 0, we have the following inequality: / |V<£|2dx - 2A / -JW—<fdx > m ,A / <f (3.2.6) i n Ja I 1 - u\) Ja for any <f> € H~l(£l), since u x < l - e . Now, take any </> £ ( f t ) D C 1 (ft) such that \\(f>\\c^ < &x- Since u\ < 1 — | e , if 5X < §, then ux + <j) < 1 — e and we have that: = I / n | vrf*> +1 v« • v* . - A / n / W ( r - i - ^ - j-L-) „ 2 7 ) . / " , 2 _ > /" f / w 1 1 0 <P2 \ - 2 A J n n X ) [ l - u x - < f > 1-UX ( 1 - « A ) 2 ( l - u A ) 3 J ' where we have applied (3.2.6). Since now 1 1 <f> <j>2 <C\4>\ \l-ux-cj> l - u x ( l - u A ) 2 ( l - u A ) 3 l for some C > 0, (3.2.7) gives that Je,x(ux + cj>) - J£<x(ux) > ( ^ - CX || / ||oo Sx) I <t>2 > 0 provided <5A is small enough. This proves that ux is a local minimum of J£tX in the C 1 topology. Since (3.2.4) is satisfied, we can then directly apply Theorem 1 in [12] to get that ux is a local minimum of J £ | A in Hg(ft). • Since now / ^ 0, fix some small ball B2r C ft of radius 2r, r > 0, so that JB f{x)dx > 0. Take a cut-off function \ s o that x = 1 on B r and x = 0 outside B2r. Let we = (1 — e)x € F ^ f t ) . We have that: Je,x(we) < / | V X | 2 d x - A /" / ( z ) _> - o o 2 i n e i s r 53 Chapter 3. Compactness along Lower Branches as e —> 0, and uniformly for A far away from zero. Since JzAux) = \ I \Vux\2dx-X j J £ L d x ^ \ j \Vu*\2dx-X* j / ^ d x 2 Jn J n l ~ u x 2 Jn Jn 1 - u as A —* A*, we can find that for e > 0 small, the inequality Je,x(we) < Je,x{uX) (3.2.8) holds for any A close to A*. F i x now e > 0 small enough so that (3.2.8) holds for A close to A*, and define ce,\ = inf max J£,\(u), •yer ue-y where r = { 7 : [0,1] —> HQ(Q);I continuous and 7(0) = u\, 7(1) = wE}. We can then use the Mountain Pass Theorem to get a solution U£tx of (3.2.2) for A close to A*, provided the Palais-Smale condition holds at level c. We next prove this (PS)-condition in the following form: L e m m a 3.2.2. Assume that {wn} C HQ(£Y) satisfies JE,xn(wn)<C, J's,Xn(wn)-^0 in H ~ L (3.2.9) for Xn —> A > 0. Then the sequence (wn)n is uniformly bounded in HQ(Q) and therefore admits a convergent subsequence in HQ(Q). Proo f : By (3.2.9) we have that: / \Vwn\2dx - A„ / f(x)g£(wn)wndx = o(|| wn \\Hi) Jn Jn as n —» + 0 0 and then, C> \ ( \Vwn\2dx -Xn [ f(x)Ge{wn)dx 2 Jn Jn = - i ) J \Vwn\2dx + Xn J^f{x)(^wng£(wn) - G£(wn))dx + o(|| wn \\Hi) > [\ - \) j \Vwn\2dx + o(|| wn \\Hh) - C£ +A„ / f{x)(^wng£(wn)-G£(wn))dx J{wn>Mc} y >{\-\)J^wn\2dx + o{\\wn\\Hl)-Ce in view of (3.2.5). Hence, sup || wn \\Hi< + 0 0 . neN 0 Since p is subcritical, the compactness of the embedding HQ(Q.) LP+1(Q) provides that, up to a subsequence, wn —> w weakly in HQ(£1) and strongly in L P + 1 ( Q ) , for some w G HQ(Q). B y (3.2.9) we get that Jn \\7w\2 = X Jnf(x)g£(w)w, and then, by (3.2.4), we deduce that [\V(wn-w)\2 = / \Vwn\2- f | V ™ | 2 + o ( l ) Jn Jet Jo = Xn f{x)g£(wn)wn -XI f{x)g£(w)w + o ( l ) -> 0 Jn Jo 54 Chapter 3. Compactness along Lower Branches as n —> + 0 0 . • C o m p l e t i o n of T h e o r e m 3.1.2: Consider for any A G (A*-S, A*) the Mountain Pass solution U£i\ of (3.2.2) at energy level c£t\, where 8 > 0 is small enough. Since cEt\ < C£|A*-<5 for any A G (A* — 5, A*), and applying again Lemma 3.2.2, we get that || U£t\ < C , for any A close to A*. Then, by (3.2.4) and elliptic regularity theory, we get that U£>\ is uniformly bounded in C2,a(Cl) for A t A*, for a G (0,1). Hence, we can extract a subsequence U£t\n, A n | A*, converging in C2(Cl) to some function U*, where U* is a solution for problem (3.2.2) at A = A*. Also u* is a solution for (3.2.2) at A = A* so that A-X*f(x)g'£(u*)) = 0. B y convexity of gE(u), similar to §2.4.1 it is classical to show that u* is the unique solution of this equation and therefore U* = u*. Since along any convergent sequence of UE>\ as A | A* the limit is always u*, we get that l im^A* U£>\ = u* in C 2 ( f j ) . Therefore, since u* < 1 - 2e, there exists 5 > 0 so that for any A G (A* - 5, A*) UEt\ <u*+e<l-e and hence, UEi\ is a solution of (S)\. Since the Mountain Pass energy level C £ ] A satisfies C E ] A > Je,\(u\), we have that UEi\ ^ u\ and then Ue>\ = U\ for any A G (A* — 5, A*). Note that by [20], we know that u\, U\ are the only solutions of (5)A as A | A*. • Applying the compactness of Theorem 3.3.1 proved in next section, one can note that the argument of Theorem 3.1.2 works also for problem (S)\ on the unit ball with f(x) in the form (3.3.1) provided N > 8, a > a^. This leads to the following proposition for higher dimensional case. P r o p o s i t i o n 3.2.3. Theorem 3.1.2 is still true for N > 8 provided Cl is a ball, and f(x) is as in (3.3.1) with a > a^. 3.3 Minimal branch for power-law profiles Our goal of this section is to study the effect of power-like permittivity profiles f(x) ~ ( a ; o n the problem (S)A denned in the unit ball B = B\(Q). The following main results of this section extend Theorem 2.1.2 to higher dimensions N > 8, which give Theorem 3.1.1 concerning the compactness of minimal branch. T h e o r e m 3.3.1. Assume N > 8 and a > aN = 3 J V ~ + 1 4 ^ | A Let f G C{B) be such that: f{x) = \x\ag(x), g(x) > C > 0 in B. (3.3.1) Let (A n )„ be such that A n —> A £ [0, A*] andun be a solution of(S)\n so that pL\tTl := Hit\n(un) > 0. Then, S l i p || XLn I j 00 < 1. In particular, the extremal solution u* = l im u\ is a solution of (S)\* such that p,\ A * ( U * ) = 0. P roo f : Let B be the unit ball, and let (A„) n be such that Xn —> A G [0,A*] and un be a solution of (5)A„ on B so that Mi.n := M i , A n K 0 > 0. (3.3.2) B y Proposition 2.5.2 un coincides with the minimal solution u\n and, by some symmetrization arguments, it is shown in Proposition 2.6.1 that the minimal solution un is radial and achieves its absolute maximum only at zero. 55 Chapter 3. Compactness along Lower Branches Given a permittivity profile f(x) as in (3.3.1), in order to get Theorem 3.3.1, we want to show: sup || un ||oo< 1, (3.3.3) provided N > 8 and a > = 3 J V ~ ^ ^ | ' y / ^ . In particular, since u\ is non decreasing in A and S U p || UX ||oo< 1. Ae[o,v) the extremal solution u* = l im ux would be a solution of (S)\» so that nit\*(u*) > 0. Prop- erty fxi^'iu*) = 0 must hold because otherwise, by implicit function theorem, we could find solutions of (S)x for A > A*, which contradicts the definition of A*. In order to prove (3.3.3), let us argue by contradiction. Up to a subsequence, assume that un{0) = m a x u n —» 1 as n —> +oo. Since A = 0 implies un —> 0 in C2(B), we can assume B that A n —> A > 0. Let en := 1 — un(0) —+ 0 as n —> +oo and introduce the following rescaled function: 3 1_ Un{y) = n l " V ) , y £ B n : = B s i (0). (3.3.4) The function Un satisfies: ' A T T \y\a9{ei^\n^y) . _ A [ / » = —{j2 " i n B « . (3.3.5) I Onfe) > C/n(0) = 1, and Bn —> R w as n —» +oo. This would reduce to a contradiction between (3.3.2) and the following Proposition 3.3.2. • Proposition 3.3.2. There exists a subsequence {Un}n defined in (3.3.4) s u c h that Un —* U in Cjoc(RN), where U is a solution of the problem AU = 9 { 0 ) ^ in*», ( 3 3 6 ) U(y) > U(0) = 1 in RN . Moreover, there exists <f)n S C Q ° ( B ) such that: I. ( j v w 2 _ 2 ^ M , a < 0 . IB The rest of this section is devoted to the proof of Proposition 3.3.2. First, we establish the following theorem, which characterizes the instability for solutions of a limit problem (3.3.7) on RN. Theorem 3.3.3. Assume either l<N<7orN>8 and a > a^. Let U be a solution of the problem A U J S ™RN> (3.3.7) U(y) >C>0 in RN. 56 Chapter 3. Compactness along Lower Branches Then, / i l(CA) = i n f | j f J V ( | V ^ | 2 - ^ 0 2 ) ; 0 - G C O O O ( R J V ) and j ^ 2 = l j < 0 . (3.3.8) Moreover, if N > 8 and 0 < a < a^, then there exists at least one solution U of (3.3.7) satisfying u-i{U) > 0. P roo f : B y contradiction, assume that K{U) = inf y ( | V 0 | 2 - <j>2); 4> e C?(RN) and <f>2 dx = l | > 0. By the density of C0X(RN) in D1'2(RN), we have J|V</>|2 > 2 y î 2<£2 , V 0 G D 1 , 2 ( R W ) . (3.3.9) In particular, the test function <6 = 1N_i s £ D 1 ' 2 ( R i V ) applied in (3.3.9) gives that ( i +M 2 ) - * - + 2 / ^ t — < C / L - ^ < + o o J ii + W)V+»u* J (i + IDI*)?+' for any <5 > 0. Therefore, we have /• i / (i + M2)^ , / (i + l^l2)" J (1 + | U|2) i^+<5[/3 7 B L (1 + |y|2)^2+*^3 ./ Bc (1 + |y|2) V + * [ / 3 i C f e M C h - ( 3 ' 3 1 0 ) < c + c i»r (1 + 1 ^ 2 ) ^ + ^ 3 \y\a (i + | y | 2 ) ^ + 4 c / 3 ' which gives / l-2-a , , <C + C [ L _ _ < + 0 o . (3.3.11) J (i + \y\2)^-^+sU3 J ( l + |y | 2 ) f+* Step 1. We want to show that (3.3.9) allows us to perform the following Moser-type iteration scheme: for any 0 < q < 4 + 2\/6 and (3 there holds / (1 + | y | 2 ) ^ - f U0+3 - C ^ + J (1 + | y | 2 ) / W ( 3 - 3 ' 1 2 ) (provided the second integral is finite). Indeed, let R > 0 and consider a smooth radial cut-off function n so that: 0 < n < 1, •n2 77 = 1 in BR(0), r, = 0 in RN \ B2R(0). Multiplying (3.3.7) by + ^ | 2 ^ _ l y g + 1 , 9 > 0, and 57 Chapter 3. Compactness along Lower Branches integrating by parts we get: \y\W I [ v f 2 ^ a _ * ( g + i ) M v f 2 ) (1 + . | j , |2) /J- l t f«+3 4(g + 1) 02 9 + 2 02 4(9 + 1) (1 + | J / | 2 ) ^ + 9 •/ 1 V(l + M2) * £/ 2(9 + 2) /• 1 / J _ 2 A ( V- ) (i + \y\2)^ where the relation A(ip)2 = 2|V'0|2 + 2ipAtp is used in the second equality. Then, by (3.3.9) we deduce that (8? + 8 - 9 2 ) J \y\W (l + |y|2)^-1^9+3 71 . . o ' + -(i + M 2 ) ^ ' , 1 2 ^ (1 + M2) Assuming |V?7| < ^ and |A?y| < - ^ j , it is straightforward to see that: (1 + | 2 / | 2 ) ^ |v ( < c V (l + l i / l 2 ) ^ ' (i + M2) * .(1 + lyl2)? + R2{1 + |y|2)/3-l*B2*(0)\B*(0) for some constant C independent of R. Then, (89 + 8 - 9 (1 + |j , |2)/3-ltf«+3 - ^ _/ (1 + |y|2)/9^g- Let 9 + = 4 + 2\/6. For any 0 < 9 < 9+, we have 89 + 8 - 9 2 > 0 and therefore: |y |V / (1 + |f/|! (1 + |y| 2)/3-l[/9+3 (1 + |i/|2)^l79 ' where Cq does not depend on R > 0. Taking the limit as i? —> + 0 0 , we get that: y \y\a < c y 1 7 (1 + |j/|2)/3-l[/</+3 - ° » _/ (1 + |y | 2)0£/9 ' and then, the validity of (3.3.12) easily follows from the same argument of (3.3.10). Step 2. Let either l < A ' ' < 7 o r A ' ' > 8 and a > a « . We want to show that / ( i + ls y | 2 ) ^ < + 0 0 (3.3.13) 58 Chapter 3. Compactness along Lower Branches for some 0 < g < g + = 4 + 2y/E. Indeed, set p0 = +6,5>0, and g 0 = 3. B y (3.3.11) we get that / ( i + M 2 )*c /«> < +oo. Let pi = PQ - i(l + f ) and g, = go + 3i, i € N . Since g 0 < gi < q+ = 4 + 2\/6 < g 2 , we can iterate (3.3.12) exactly two times to get that: / (1 + | j / | 2 ) f t £ / « < +oo (3.3.14) where p2 = ^ " l " 3 " + 6, q2 = 9. Let 0 < g < g + = 4 + 2\/6 < 9. B y (3.3.14) and Holder inequality we get that: / f 1 ^ /* 1 \ 9 — q - ( / ( i + i y i 2 ) ^ t / « ) 9 ( y ( 1 + M 2 ) ^ ( ^ + i « ) + ^ ) 9 < + ° ° ( l + |y|2)C/9 ( i + I ^ K ^ - ' + i - ) U1 (1 + | j , | 2 ) f ( ^ - i + l a J + l ( l | y | 2 ) ^ provided — ^ ^ P 2 + > N or equivalently To assure (3.3.15) for some 5 > 0 small and q < q+ at the same time, it requires < q+ or equivalently K i V < 7 or N>8, q > q N = 3 N ~ 1 4 ~ * ^ . ~ ~ 4 + 2 ^ Our assumptions then provide the existence of some 0 < g < g + = 4 + 2A/6 such that (3.3.13) holds. S t e p 3. We are ready to obtain a contradiction. Let 0 < q < 4 + 2\/6 be such that (3.3.13) holds, and suppose 77 is the cut-off function of Step 1. Using equation (3.3.7) we compute: 4 ( 9 + 1 ) J '•[/«+•' y ui + 4 8g + 8 - g 2 f \y\V jf IVT?! 2 g + 2 f A T ? 2 4(g + 1 ) 7 t /«+ 3 7 Ui 4(g + 1) y U" 59 Chapter 3. Compactness along Lower Branches Since 0 < q < 4 + 2\/6, we have 89 + 8 - q2 > 0 and 8q + 8-q2 f \ v £ r ? , 0 ( ± [ J _ \ - 4(g + l ) y B l ( 0 ) ^ + 3 + U 2 y B 2 f i(o)\B R (o) 17'/ 8q + 8-g2 f \yT]f,n([ 1 \ - 4(g + l ) y B l ( 0 ) C / 9 + 3 + W M > f l ( l + M 2 ) C / W - Since (3.3.13) implies: l i m f t _ + 0 o / 77:; | 1 | os r r „ = 0, w e S e t t n a t for R l a r S e 7|y|>fi ( i + \yr)uq [ | V ( - i U | 2 - / ^ ( - ^ - ) 2 y - i v ^ i / f l / 2 ^ y c / 3 ^ 9 / 2 ^ < _ 8 g + 8 - ^ 2 / w _ + 0 ( [ - )<o. 4(9 + 1) JBI(0) A contradiction to (3.3.9). Hence, (3.3.8) holds and the proof of the first part of Theorem 3.3.3 is complete. We now deal with the second part of Theorem 3.3.3. Consider the minimal solution un of (5)A„ as A„ -> A* on the unit ball with f(x) = \x\a. Using the density of Cg°(ft) in H^(Q), Theorem 2.5.1 gives / ( i v ^ l 2 - , f n | a : | " ^ ) ^ > o v^ecg°(n). In view of the rescaled function (3.3.4), we now define 4>n(x) = ( e ^ X n ^ Y ^ ^ e n ^ ^ x ) . Then we have J ( | V ^ - 2 | 3 - ^ 2 ) d y = l i m ™ | ( | v ^ | 2 - ^ 2 ) d y = l i n w , J ( | V 0 „ | 2 - 0^-34>2n)dx > 0, since <j> has compact support and Un —> U in Cj 1 ( R w ) . This completes the proof of Theorem 3.3.3. • Proof of Proposition 3.3.2: Let R > 0. For n large, decompose Un = U\ + U2, where U2 satisfies: J AU2 = AUn in B f i ( 0 ) , \ U2 = 0 on 0B*(O). B y (3.3.5) we get that on BR(0): 0 < AUn < Ra II 9 ||oo. 60 Chapter 3. Compactness along Lower Branches and standard elliptic regularity theory gives that U2 is uniformly bounded in C1'^(BR(Q)) for some j3 6 (0,1). Up to a subsequence, we get that U2 —> U2 in C 1 ( B f i ( 0 ) ) . Since U\ = UN > 1 on 8BR(Q), by harmonicity U\ > 1 in BR(0) and then the Harnack inequality gives sup U\ < C R inf UN < CRU^O) = C R ( 1 - U2(0)) < C R ( l + s u p \ U 2 ( 0 ) \ ) < oo. BR/2(0) BR/2{0) nen Hence, UN is uniformly bounded in C1'/3(BR/I(Q)) for some (3 G (0,1). Up to a further subse- quence, we get that U„ -> U1 in C1{BR/4(0)) and then, f/„ -» UL + U2 in C 1 (-8/1/4(0)) for any R > 0. B y a diagonal process and up to a subsequence, we find that UN —> U in Cj 1 (U^ ) , where E/ is a solution of the equation (3.3.6). If either 1 < N < 7 O X N > % and a > ajv, since 5(0) > 0 Theorem 3.3.3 shows that Hi(U) < 0 and then, we find <f> G C^(RN) so that: J ( | V ^ | 2 - 2 f l ( 0 ) ^ 2 ) < 0 . Defining now then we have - J ( | V 0 | 2 - 2 f l ( O ) ^ 2 ) < O asn -> + 0 0 , since <f> has compact support and UN —> f7 in (IR^). The proof of Proposition 3.3.2 is now complete. • 3.4 Compactness along the second branch In this section, we are interested in continuing the second branch ti l l the second bifurcation point, by means of the implicit function theorem. Our main result of this section is the compactness of Theorem 3.1.3 for 2 < N < 7. In order to prove Theorem 3.1.3, we now assume that / G C(Q) is in the form (3.1.3), and let (un)n be a solution sequence for (S)\n where A n —> A G [0, A*]. 3.4.1 Blow-up analysis Assume that the sequence (un)n is not compact, which means that up to passing to a subse- quence, we may assume that m a x u n —> 1 as n —> 00. Let xn be a maximum point of un in ft (i.e., un(xn) = m a x u n ) and set en = 1 — un(xn). Let us assume that xn —> p as n —* + 0 0 . We have three different situations depending on the location of p and the rate of \xn — p\: 1) blow up outside the zero set {pi,... ,Pk} of f(x), i.e. p $ {pi,... ,Pk}; 2) "slow" blow up at some Pi in the zero set of f(x), i.e. xn —> Pi and e^3Xn\xn — Pi\a+2 —> + 0 0 a s n - > +00 ; 61 Chapter 3. Compactness along Lower Branches 3) "fast" blow at some pi in the zero set of f{x), i.e. xn —» p% and l im„_> + 0 0 sup(en3\n\xn — Pi\a+2) < + 0 0 . Accordingly, for 2 < iV < 7 we next discuss each one of these situations. 1 s t Case Assume that p £ {pi,... ,pk}- In general, we are not able to prove that a blow up point p is always far away from dft, even though we suspect it to be true. However, the following weaker estimate is available and -as explained later- wi l l be sufficient for our purposes. Lemma 3.4.1. Let hn be a function on a smooth bounded domain An in RN. Let Wn be a solution of the problem Wn(y)>C>0 inAn, ( 3 A 1 ) Wn(0) = 1, for some C > 0. Assume that sup || hn \\oo< + ° ° and An —> as n —> +oo for some n S N H e (0,+oo), where is a hyperspace so that 0 € and dist (0, dT^) = fi. Then for sufficiently large n, either inf Wn<C (3.4.2) dA„nB2LL(0) or inf d„Wn < 0, (3.4.3) dAnt\B2TL{0) where v is the unit outward normal of An. Proof: Assume that dvWn > 0 on dAn n ^2^(0). Let G(x) = { _ J _ l o g M if TV = 2 2?r B2n be the Green function of the operator —A in B2^(0) with homogeneous Dirichlet boundary condition, where CN = (jv-2)|dBi(o)| a n c ^ I' I s t a n d s for the Lebesgue measure. Here and in the sequel, when there is no ambiguity on the domain, v and dS will denote the unit outward normal and the boundary integration element of the corresponding domain. B y the representation formula we have that: W n (0) = - f AWn{x)G(x)dx - I Wn{x)dpG{x)dS JAnnB2ti(o) JdA„nB2ll(o) ^ 4 4^ + f duWn{x)G{x)dS - f Wn{x)dvG{x)dS. JdAnnB2n(0) JdB2LL(0)r\An Note that on dT^ we have f ^ r a ? - ^ > ° if iV = 2 ; , 62 Chapter 3. Compactness along Lower Branches Since dAn —> dT^ as n —+ oo, it yields that for sufficiently large n, duG{x) < 0 on dAn n £ 2 / i ( 0 ) . (3.4.6) Hence, by (3.4.4), (3.4.6) and the assumptions on Wn, we then get for sufficiently large n, I M r \ G i X ) d x - { i n f Wn) I dvG{x)dS, JAnr\B2^)Wn\x) KdAnnB2LI(0) JdAnnB2LI(0) since G(x) > 0 in B2^(0) and dvG(x) < 0 on d i ? 2 M ( 0 ) . On the other hand, we have and (3.4.5) also implies that for sufficiently large n, - / d„G(x)da(x) -> - / dvG{x)dS > 0. JdAnnB2LI(0) JdTllr\B2li(p) Then for sufficiently large n, 1 > - C + C - 1 ( inf W„) for some C > 0 large enough. va4„nB 2 M(o) Therefore, we conclude that for sufficiently large n, inf Wn is bounded and the proof is aAnnB2f.(0) complete. • We are now ready to completely discuss this first case. Introduce the following rescaled function: i TT i \ 1 — un(en^n 2y + xn) _ CI — xn , « Un(y) = - - , y G ft„ = 3 _ i . ( 3 A 7 ) £ " - 2 \ 2 then J7n satisfies 2 _ i f{el\n2y + xn) . A C / » = - I J72 i n f i » > (3.4.8) C/„(0) = 1 " in ftn. In addition, we have that Un > Un(0) = 1 as long as xn is the maximum point of un in ft. We would like to prove the following: Proposition 3.4.2. Let xn G ft and £n:—l— un(xn), and assume xn ->P <£ {Pi,---,Pk} , SnK1 0 a s n - > + c o . (3.4.9) £e£ [/„ and ftn 6e defined as in (3.4-7) satisfying Un > C> 0 m ftn n B f l n ( 0 ) (3.4.10) for some Rn —> +oo asn —> +oo. T/ien, i/iere exists a subsequence of (Un)n such that Un —> U in Cjoc(RN), where U is a solution of the problem * U = ' - W (3.4.U) U{y) > C > 0 inRN. 63 Chapter 3. Compactness along Lower Branches Moreover, there exists a function (f>n £ C Q ° ( O ) such that and Supp (f>n C B 3 _ 1 (xn) for some M > 0. P roo f : We first claim that Lemma 3.4.1 provides us with a stronger estimate: e^A-^dis t (xn,dQ.))~2 -> 0 as n -> + 0 0 . (3.4.13) Indeed, by contradiction and up to a subsequence, assume that enA"1^2 —> 5 > 0 as n —> + 0 0 , where d„ := dist ( x „ , 9 n ) . We get from (3.4.9) that d„ —> 0 as n —» + 0 0 . We introduce the following rescaling W„: , x 1 -un{dny + xn) Sl-Xn Wn{y) = , y £ An = — . Since dn —> 0, we get that An -» T M as n —» + 0 0 , where T M is a hyperspace containing 0 so that dist (0,(97^) = y.. The function W„ solves problem (3.4.1) with hn(y) = ^f(dny + xn) and C = Wn(0) = 1. We have that: || ||oo< II / I II / H°° and Wn = j • + 0 0 on dAn as n —> 00. B y Lemma 3.4.1 we get that (3.4.3) must hold, a contradiction to Hopf Lemma applied to un. This gives the validity of (3.4.13). (3.4.13) now implies that Cln —» RN as n —> + 0 0 . Arguing as in the proof of Proposition 3.3.2, we get that Un -> U in C^1 ( R N ) , where £/ is a solution of (3.4.11) by means of (3.4.8)- (3.4.10). ° C If 2 < N < 7, since f(p) > 0 by Theorem 3.3.3 we get that ni(U) < 0 and then, we find 4> £ CQ°(RN) SO that: / (I W l 2 - 2J^4>2) < 0. 3 _1 N-2 _ 3 1 Defining now 4>n(x) = ( e ^ A n 2 ) 2 (f>(£n2Xn(x — xn)), then we have I ( I W n ' 2 " = / ( I W ' 2 " 2 / ( £ " A " ^ + :C"^2) -> / ( i v ^ l 2 - ^ < A 2 ) < 0 as n —> + 0 0 , since ^ has compact support and Un —> U in C j 0 C ( R ) . The proof of Proposition 3.4.2 is now complete. • 2 n d Case Assume that xn —> Pi and £ ~ 3 A „ | x n — Pi\a'+2 —> + 0 0 as n —* + 0 0 . For conve- nience, in the following we denote k a : = a i , / , • ( * ) : = ( J J \x - Pjp)g(x), (3.4.14) 64 Chapter 3. Compactness along Lower Branches and we rescale the function un in a different way: Un(y) = , y e ft„ = a _ i . (3.4.15) 71 £n^n2\Xn~Pi\ 2 In this situation, Un satisfies: Aun = \ e h n k \ x n - P i \ - ^ y + ^ P i - \ a f i ^ X n 2 l g " - f i ~ f y + x " > i n fi,,, F n Pi I t-'n C/„(0) = 1 in ftn, (3.4.16) and we have the following P r o p o s i t i o n 3.4.3. Let xn £ ft and en := 1 — u n (a; n ) , and assume xn^Pi, £^ 3 A„|x r a - P i | a + 2 —> +oo as n —> + 0 0 . (3.4.17) Le i C/ n and ft„ be defined as in (3.4-15) satisfying (3-4-10). Then, up to a subsequence, Un —> U in CjQC(B.N), where U is a solution of the equation: ^ U - TJ2 ' (3.4.18) U{y) > C > 0 inRN. Moreover, there holds (3-4-12) for some 4>n £ Co°(ft) such that Supp <(>n c B 3 1 _ a (x„) /or some M > 0. Me^A 7 l 2 | x„ -p i | 7 Proo f : Similar to Proposition 3.4.2 we get from (3.4.17) that ftn — > RN as n —* + 0 0 . As before, £/„ -» [/ in (RN) and 17 is a solution of (3.4.18) in view of (3.4.10) and (3.4.16)- (3.4.17). Since 2 < N < 7 and fi(pt) > 0, Theorem 3.3.3 implies (ii(U) < 0 and the existence of some 4> £ C0X{RN) so that: / (| W | 2 - < 0. Defining now <f>n(x) = (e%\J\xn - f t p * ) ™ 2 '<A(e„ 1 A | | x n - p ^ f (x - £ „ ) ) , then we have = / (IV^I 2 - lehn^Xn -Pi\-^y + ^ L ^ l M ^ l X n ~ + / (| W | 2 - ^ < / > 2 ) < 0 a s n - » + 0 0 , which completes the proof of Proposition 3.4.3. • 65 Chapter 3. Compactness along Lower Branches 3rd Case Assume that xn —> pi as n —» + 0 0 and e„ 3 A„|a ; n - p j | Q i + 2 < C. In the following we denote a := ai, and we rescale the function un in a still different way: 3 1 (7n(j/) = , = — 3 — Z ~ T - • (3.4.19) - 2 + Q \ 2 + Q Then £/ n satisfies 3 l _ AC/„ = |y + £n + Xn(xn-pj)I — ^ i n n™> (3.4.20) [ t/„(0) = 1 " i n fi„, where /j is defined in (3.4.14). In this situation, the result we have is the following P r o p o s i t i o n 3.4.4. Let xn £ Q and en := 1 — un(xn), and assume 3 1 £nK1 -* 0 . -> Pi - £ « Q + 2 A « + 2 fan - Pi) -* 2/o as t i - » +oo. (3.4.21) Let Un and Q,n be defined as in (3.4-19) satisfying either (3.4-10) or Un>C(e~^\n^\xn-Pi\y%\y + en^XZ^(xn-Pi)\° in nnnBRn(0) (3.4.22) for some Rn —* +oo as n —• +oo and C > 0. T/jen, up to a subsequence, Un —* U in CjQC(RN) and U satisfies: AC/ = \y + yo\a^j0- inRN, ( 3 4 2 3 ) U(y) > C > 0 i n R " . Moreover, we have (3.4-12) for some function (fin £ Co°(n) suc/i that Supp <t>n C B 3 _ i (xn) for some M > 0. P roo f : B y (3.4.21) we get again that Cln —> RN as n —> +oo. If (3.4.10) holds, as before we have Un-^U in C^QC(RN) and, by (3.4.10) and (3.4.20)-(3.4.21), U solves (3.4.23). We need to discuss the non trivial case when we have the validity of (3.4.22). Arguing as in the proof of Proposition 3.3.2, fix R > 2\yo\ and decompose Un = U* + U2, where U2 satisfies: f AU2 = AUn i nBf l (O) , \ U2 = 0 on dBR(0). By (3.4.20) and (3.4.22) we get that on BR(0): 3 1_ \a fi(£n~ Xn + y + Xn) 0 < AUn = \y + £n2+a X£+a (xn ~ Pi)\C rj2 _ _ 3 _ _ J _ 2a, 3_ - i - , l <C{£na+2Xn+2\Xn-Pi\) 3 \y + en2+a\n+a(xn-Pi)\- 66 Chapter 3. Compactness along Lower Branches 3 1 Since en a+2Xn+2 (xn - p%) is bounded, we get that 0 < AUn < Cn on BR(0) for n large, and then, standard elliptic regularity theory gives that U2 is uniformly bounded in C1')3(BR(0)) for some P G (0,1). Up to a subsequence, we get that U2 -» U2 in C1{BR(Q)). Since by (3.4.22) U^ = Un> C(R - 2\y0\)t > 0 on dBR{0), by harmonicity > CR in BR(0) and hence the Harnack inequality gives s u p B f i / 2 ( 0 ) ^ < C f i i n f B H / 2 ( 0 ) Etf < CflC^(O) = CR(l - t/ 2(0)) < C f i ( l + s u P n 6 N | t / 2 ( 0 ) | ) < o o . Therefore, C/^ i s uniformly bounded in Cl>P(BR/${$)), /? G (0,1). Up to a further subsequence, we get that U\ -> U1 in C 1 (B f l / 4 (0 ) ) and then, Un -> f/1 + t/ 2 in C ^ B ^ O ) ) for any > 0. By a diagonal process and up to a subsequence, by (3.4.22) we find that Un —> U in (RN), where U eC1(RN)C\ C2(RN \ {-j/o}) is a solution of the equation AU=\y + y 0 \ a ^ in R " \ {-y 0 } , U(y)>C\y + y0\% mRN, for some C > 0. In order to prove that t/ is a solution of (3.4.23), we still need to prove that U(—yo) > 0. Let B be some ball so that — yo G dB and assume by contradiction that U{-y0) = 0. Since -AU + c{y)U = 0 in B , £/ G C2{B) n C ( B ) , E % ) > l / ( - y 0 ) in B , and c(y) = fi(Pi) \y+ffl > 0 is a bounded function, Hopf Lemma shows that dvU{—yo) < 0, where v is the unit outward normal of B at —yo- Hence, U becomes negative in a neighborhood of —yo, in contradiction with the positivity of U. Hence, U(—yo) > 0 and U satisfies (3.4.23). Since 2 < N < 7 and fi{pi) > 0, Theorem 3.3.3 implies fi\{U) < 0 and the existence of some cf> G C^(RN) so that: / ( | V ^ | 2 - | 2 / + 2 / 0 r ^ M ^ ) < 0 . 3 1 /V_2 3 1 Let <j>n(x) = (e£+a Xn 2 + a ) ~ <f>(en 2 + a Xn+a (x - xn)), then it reduces to 3 1 = / (1 V 0 | 2 - \y + e l ^ xt* (xn - Pi) r y W + X n ) 4>2) - / ( | V ^ | 2 - | 2 / + y o r ^ ^ 2 ) < 0 a s m +oo, and Proposition 3.4.4 is established. • 67 Chapter 3. Compactness along Lower Branches 3 . 4 . 2 S p e c t r a l c o n f i n e m e n t Let us now assume the validity of (3.1.4), namely p,2,n •— l^2,xn(un) > 0 f ° r any n e N . This information wil l play a crucial role in controlling the number k of "blow up points" (for (1 — Un)-1) in terms of the spectral information on un. Indeed, roughly speaking, we can estimate k with the number of negative eigenvalues of LUnt\n (with multiplicities). In particular, assumption (3.1.4) implies that "blow up" can occur only along the sequence xn of maximum points of un in Q. P r o p o s i t i o n 3 .4 .5. Assume 2 < N < 7, and suppose f G C(Cl) is as in (3.1.3). Let Xn A G fO, A*l and un be an associated solution. Assume that un(xn) = m a x u n —> 1 as n —> +co. a Then, there exist constants C > 0 and No G N such that (1 - un(x)) > C\\d(x)i\x-zn|f , V x G ft, n >-/V 0 , (3.4.24) where d(x)s = min{|x — Pi\~3 : i = l , . . . , f c} is the distance function from the zero set {pi,...,Pk} off(x). Proof : Let en = 1 — un(xn). Then, en —> 0 as n —> +oo and, even more precisely: elK1 -> 0 as n - t +oo. (3.4.25) Indeed, otherwise we would have along some subsequence: 0 ^ 7VZ^2 < ^ II / lloo< C, Xn -> 0 as n -» +oo. But if the right hand side of (5)A n is uniformly bounded, then elliptic regularity theory implies that un is uniformly bounded in Cl'P(Cl) for some (3 G (0,1). Hence, up to a further subse- quence, un —y u in C 1(f2), where u is a harmonic function such that u = 0 on dCl, and hence u = 0 on Q. On the other hand, e„ —> 0 implies that m ^ x - u = 1) a contradiction. B y (3.4.25) we get that e^A" 1 -> 0 as n -» +oo, as needed in (3.4.9) and (3.4.21) for Propositions 3.4.2 and 3.4.4, respectively. Now, depending on the case corresponding to the blow up sequence xn, we can apply one among Propositions 3.4.2 and 3.4.4 to obtaining the existence of a function <f>n G Co°(n) such that (3.4.12) holds, together with a specific control on Supp tf>n. B y contradiction, assume now that (3.4.24) is false: up to a subsequence, then there exists a sequence yn G Cl such that A ^ 3 c % „ ) ~ f \yn -xn\~i(l -un(yn)) = Xn3 m i n x e o (d(x)~%\x - xn\~%(l - un{x))^ —> 0 as n—>+oo. Then, \xn := 1 - Un(j/n) —» 0 as n —> oo and (3.4.26) can be rewritten as: (3.4.26) 3 _ I 11 2 \ 2 H - - + 0 as +oo. (3.4.27) | - 2/n| ^(j/n) 2 68 Chapter 3. Compactness along Lower Branches We now want to explain the meaning of the crucial choice (3.4.26). Let pn be a sequence of positive numbers so that - i l l Rn := pn 2 m i n { d ( y n ) 2 , \xn - yn\2} -» +co as n -> +oo. (3.4.28) Let us introduce the following rescaled function: - 1 - un(Pny + yn) - 0 - yn Un(y) = , 2/ G ft„ = — 5 • Mn Pn Formula (3.4.26) implies: =d(yn)3\yn -xn\% m i n i e n (d(x)~3 \x - xn\~i ( l - u „ ( a r ) ) ) < Hnd{yn)* \yn - xn\3d{Pny + yn)~s\Pny + yn Xn Since d(Pny + yn) . r\Vn-Pi . Pn I . - . 1 Pn L , —r—'- = mm{ + — — r y : i = 1, . . . , A;} > 1 - T—r\y\ d{yn) 1 d{yn) d{yn) 1 d(yn) in view of \yn - pi\ > d(yn), by (3.4.28) we get that: v d(yn) K \xn-yny v 2 y for any y £ fin f~)BRn(0). Hence, whenever (3.4.28) holds, we get the validity of (3.4.10) for the rescaled function Un at yn with respect to pn- We need to discuss all the possible types of blow up at yn. 1 s t Case Assume that yn -> q $ {pi,...,Pk}- B y (3.4.27) we get that u.n\~l —> 0 as n -> +oo. Since d(yn) > C > 0, let pn = M I A ~ 2 and, by (3.4.27) we get that (3.4.28) holds. Associated to yn, /J„, define Un, Cln as in (3.4.7). We have from above that (3.4.10) holds by the validity of (3.4.28) for our choice of pn. Hence, Proposition 3.4.2 applied to Un gives the existence of ipn G C^(9.) such that (3.4.12) holds and Supp tpn C B a _ i (yn) for some M > 0. In the worst case xn —> q, given Un be as in (3.4.7) associated to xn, en, we get by scaling 3 _ 1 that for x = e£A„ 2 y + x„ , A „ 3 (d(x)~3\x - xn\~i ( l -Un(x ) ) ) > C A ^ ( | x _ Xn\-I (1 - u„(x) ) ) = C\y\-2Wn{y) >CR>0 uniformly in n and y G Bfl(0) for any R > 0. Then, 3 Ajj _ 1 2 F n 2/n| 0 as i n +co. Hence, in this situation <j>n and tpn have disjoint compact supports and obviously, it remains true when xn —> p / q. Hence, H2,n < 0 in contradiction with (3.1.4). 69 Chapter 3. Compactness along Lower Branches 2 n c * Case Assume that yn —> pi in a "slow" way: ^ ~ 3 A n | y „ - P i \ a + 2 + 0 0 as n —> + 0 0 . 3 _ i _ a Let now f3n = \inXn 2 \yn — pj| 2 . Since d(y n ) = | y n — Pi\ in this situation, we get that: - J 3 — = A ^ | y n - p i \ 2 - » + 0 0 , and (3.4.27) exactly gives \Xji Vn\ \Xn J/n| 3 1 ^™ P-nXn2\yn-Pi\ 2 + 0 0 (3.4.29) as n —* + 0 0 . Hence, (3.4.28) holds. Associated to p,n, yn, define now Un, Cln according to (3.4.15). Since (3.4.10) follows by (3.4.28), Proposition 3.4.3 for Un gives some ipn € C§°(Q) such that (3.4.12) holds and Supp ipn C B 3 _ i _ a (y„) for some M > 0. If x„ —» p ̂ Pi , then clearly ipn have disjoint compact supports leading to p,2,n < 0 in contradiction with (3.1.4). If also xn —> pi, we can easily show by scaling that: 1) if e^3Xn\xn -pi\a+2 —> + 0 0 as n —> + 0 0 , given Un be as in (3.4.15) associated to xn, sn, 3 _ i _ s we get that for x = enXn 2 | x n — p»| 2 y + £„, A ^ 3 ( d ( x ) _ t \x - (1 - Un{x))) = \v\-*Un(v)\en'\n'*\xn-pi\-s%iy + ^ L ? ± | - f > CR > 0 l^n Pi I uniformly in n and y G BR(0) for any i? > 0. Then, £ n A " l X n _ V A -> 0 as n -> + 0 0 , and hence, by (3.4.29) (j>n and ipn have disjoint compact supports leading to p,2,n < 0, which contradicts (3.1.4). 2) if e^ 3A„|a;„ - Pi\a+2 < C as n —> +oo, given Un be as in (3.4.19) associated to xn, £„, 3 1_ we get that for x = en+a Xn 2+ay + xn, Xn~3(d{x)-i\x-xn\—*(l-un(x))) = \y\—*Un(y)\y + s n 2 + a \ n + a {xn -Pi)\ 3 >DR\y\-lun(y)>CR>Q uniformly in n and y € BR(0) for any R > 0. Then, 3 1 2+a \ 2+a —•> 0 as n - » +oo, and hence, by (3.4.29) <t>n and Vn have disjoint compact supports leading to a contradiction. 70 Chapter 3. Compactness along Lower Branches 3 r < ^ Case Assume that yn —> pi in a "fast" way: u,-3\n\yn-Pi\a+2 <C. Since d(yn) = \yn - Pi\, by (3.4.27) we get that 3 1 \V2L_JPl = t*±il ^Xn\yn-Pir^ -> 0 as n -> +oo, (3.4.30) \xn-yn\ \xn-yn\\yn-Pi\2 and then for n large \xn - P i | > \xn - y„\ _ 2 > ! t l*n ~ P i | > t _ \Vn ~ P i | > 1_ ( 3 A 3 1 ) |j/n - Pi | |3/n - Pi | F n ~ 3/n| F n ~ 2/n| 2 Since £„ < /n„, (3.4.27) and (3.4.31) give that ^n^nl^-n Pi I 3 _ l , 2 \ 2 , M«A n 2 \ - 2 / F " — P* I \ot+2 > (, n W> \ 1 ^ (3.4.32) \Xn ~ VnWVn ~ Pi\2 \xn - yn\a+2 \Vn ~ Pi\a+2 2 _ 1 ^ / Mn A n 2 \ — 2 , . > C ( a-J —*+oo as n —»+oo. |x„ - yn\ d(yn)2 The meaning of (3.4.32) is the following: once yn provides a fast blowing up sequence at pi, then no other fast blow up at pi can occur as (3.4.32) states for xn. 3 1 Let pn = Hn+a A „ 2 + a . B y (3.4.27) and (3.4.30) we get that R _ 3 _ 1_ t-'n -,2+Q -v 2+a | „ „ , 1 - 1 , , 2 + a \ 2+a _ ^n l^n Jm| \X-n Vn] 2 _ i (3.4.33) / MnA„ 2 , 2 a = ( 5-) + (i y ) 2 + a - + 0 as n —» +co. However, since u„ blows up fast at Pi along y n , we have P~1d(yn) < C and then, (3.4.28) does not hold. Letting as before - 1 - un{pny + yn) A ft - y„ we need to refine the analysis before in order to get some estimate for Un even when only (3.4.33) does hold. Formula (3.4.26) gives that: Un(y) > \yn ~ Pi\~^\yn ~ xn\~i\Pny + yn - pi\%\Pny + yn - xn\* F n yn\ F n 2/n| (3.4.34) •\y + t i n ^ ( y n -Pi)\^ > C(u~n^ A 2 ^ \yn - pi\)_f \y + u7n &X2^ (yn - Pi)|1 71 Chapter 3. Compactness along Lower Branches for \y\ < Rn = ( l x " f e y n l ) 5 , and Rn -> + 0 0 a s n - > + 0 0 by (3.4.33). Since (3.4.34) implies that (3.4.22) holds for fJ-n, yn, Un, Proposition 3.4.4 provides some ipn £ C°° (0 ) such that (3.4.12) holds and Supp ijjn C B 3 1 (yn) for some M > 0. Since yn cannot lie in any ball centered at xn and radius of order of the scale parameter - - 1 - - 1 _a (£n An 2 Or An 2 | x „ — pi I 2 ) , we get from (3.4.33) that <j)n and ipn have disjoint compact supports leading to ^2,n < 0, a contradiction to (3.1.4). This completes the proof of Proposition 3.4.5. • 3.4.3 C o m p a c t n e s s issues We are now in position to give the proof of Theorem 3.1.3. Assume 2 < N < 7, and let / € C(Cl) be as in (3.1.3). Let (A„)„ be a sequence such that A„ —> A £ [0,A*] and let un be an associated solution such that (3.1.4) holds, namely The essential ingredient will be the estimate of Proposition 3.4.5 combined with the uniqueness result of Proposition 2.5.2. P r o o f o f T h e o r e m 3.1.3: Let xn be the maximum point of un in Cl and, up to a subsequence, assume by contradiction that un(xn) = maxu n (x ) —> 1 as n —> oo. Then Proposition 3.4.5 gives that for some C > 0 and J V o E N large, - 2 . 2 Un{x) < 1 — CXnd(x) 3 \x — Xn\3 for any x £ Q. and n > No, where d(x) 3 = min{ |a ; -p i | 3 : i = l,...,k} stands for the distance function from the zero set of f(x). Thus, we have that: 0 < ^ r 2 < C f f i % i A | | 4 (3.4.35) (i—Un) d(x) 3 |x — X „ | 3 for any x £ Q and n > A ô- Since by (3.1.3) i m [d(x) la | — 3 < | x - P i | » | | / i | | o o < C for x close to pi, fi as in (3.4.14), we get that ^ x \ a is a bounded function on Cl and then, (3.4.35) gives that Xnf(x)/(1 — un)2 is uniformly bounded in Ls(Ci), for any 1 < s < ™. Standard elliptic regularity theory now implies that un is uniformly bounded in W2'3(Cl). B y Sobolev's imbedding theorem, un is uniformly bounded in C0,^(Cl) for any 0 < /? < 2/3. Up to a subsequence, we get that un —* uo weakly in Hq(CI) and strongly in C°'P(Cl), 0 < P < 2/3, where UQ is a Holderian function solving weakly in HQ(CI) the equation: -Au0 = J K \ 2 mCl, J ? - U o ? . 0 (3.4.36) uo = 0 on 72 Chapter 3. Compactness along Lower Branches Moreover, by uniform convergence maxuo = l im maxw„ = 1 n n—>+oo £2 and, in particular uo > 0 in Cl. Clearly, A > 0 since any weak harmonic function in HQ(CI) is identically zero. To reach a contradiction, we shall first show that /xi^(uo) > 0 and then deduce from the uniqueness, stated in Proposition 2.5.2, of the semi-stable solution u\ that u0 = u\. But max.u\ < 1 for any A € [0,A*], contradicting maxuo = 1- Hence, the claimed compactness must hold. In addition to (3.1.4), assume now that p,\tn < 0, then A > 0. Indeed, if A n —> 0, then by compactness and standard regularity theory, we get that un —» u$ in C2(Cl), where UQ is a harmonic function so that UQ = 0 on dCl. Then, UQ = 0 and un —> 0 in C2(Cl). But the only branch of solutions for (S)\ bifurcating from 0 for A small is the branch of minimal solutions u\ and then, un = u\n for n large contradicting fj,\in < 0. In order to complete the proof, we need only to show that /x l i A(uo) = inf ( / (|V<£|2 - M 2 A / ( 3 ; U 2 ) ; <S> € C?(Cl) and / 4>2 = l ) > 0. (3.4.37) Indeed, first Propositions 3.4.2 ~ 3.4.4 imply the existence of a function fa € CQ*(CI) SO that / n ( | V * » | 2 - ^ f i « < 0 . (3.4.38) Moreover, Supp fa C BTn(xn) and r n —> 0 as n —> +oo. Up to a subsequence, assume that xn —> p € Cl as n —> +oo. B y contradiction, if (3.4.37) were false, then there exist fa £ C^(Cl) such that / n ( | v r f - r a « < a ( 3 ' 4 ' 3 9 ) We wil l replace fa with a truncated function fa- with 5 > 0 small enough, so that (3.4.39) is still true while fa = 0 in Bp(p) n O. In this way, 0n and <fo would have disjoint compact supports in contradiction to p,2,n > 0. Let 6 > 0 and set ^ = xsfa: where \s is a cut-off function defined as: 0 \x-p\<52, X s ( x ) = { 2 - l ^ t X ^ - 52<\x-P\<5, ' logo 1 \x — p\ > 5. By Lebesgue's theorem, we have: For the gradient term, we have the expansion: I | V ^ | 2 = [ <Pl\VX6\2 + [ xl|V<Ao|2 + 2 / XsfaVxsVfa • Jn Jn Jn Jn 73 Chapter 3. Compactness along Lower Branches The following estimates hold: and o < / ^ | v x * | 2 < Ho\\l I -. ^ 7 ^ r ~ r Jn Js2<\x-P\<6 \x-p\* log 5 log j , y v W k 2 | |0O11 O O | |V^Q| | O O f 1 2 / Xi'PoVxiV^o < : j / T - r , Jn l og^ JB!(O) Ft which provide / | V ^ | 2 -> / | V 0 O | 2 as 6 -> 0. (3.4.41) ./n i n Combining (3.4.39)-(3.4.41), we get that for <5 > 0 sufficiently small. This completes the proof of (3.4.37) and therefore, Theorem 3.1.3 is completely established. • 3.5 The second bifurcation point In this section, we discuss the second bifurcation point for (S)x in the sense A 2 = inf{ 0 > 0 : 3 a curve Vx G C([/3, A*]; C 2 (f t )) of solutions for (S)x such that u.2,x(Vx) > 0, Vx = Ux VA G (A* - 6, A*)} , where E/\ and 5 are as in Theorem 3.1.2, and we prove the multiplicity result of Theorem 3.1.5. Proof of Theorem 3.1.5: For any A G (A 2 , A*), the definition of A 2 gives that there exists a solution Vx such that: M , A : = / * I , A ( V A ) < 0 V A G ( A ^ , A * ) . (3.5.1) In particular, Vx ^ ux provides a second solution different from the minimal one. Clearly (3.5.1) is true because first fj,itX < 0 for A close to A*. Moreover, if u.ijX = 0 for some A G (A 2 , A*), then by Proposition 2.5.2 Vx — ux contradicting the fact that u-iiX(ux) > 0 for any 0 < A < A*. Since the definition of A 2 gives fi2,x{Vx) > 0 for any A G (A 2 ,A*) , we can take a sequence A n I AS and apply Theorem 3.1.3 that A 2 = l im A„ > 0, sup || VXn | | 0 0 < 1. B y elliptic n-+oo _ „ e N regularity theory, up to a subsequence VXn —> V* in C 2 ( Q ) , where V* is a solution for {S)x*. As before, Hi,x*{V*) < 0 and by continuity fi2,x*(V*) > 0. Suppose ^^{Y*) > 0, let us fix some e > 0 so small that 0 < V* < 1 — 2e and consider the truncated nonlinearity gE{u) as in (3.2.1). Clearly, V* is a solution of (3.2.2) at A = A 2 so that —A — A 2 / ( x ) a £ ( V * ) has no zero eigenvalues, since ^ I , A * ( V * ) < 0 and / i 2 , A 2 ( V * ) > 0. Namely, V* solves N(\*2, V*) = 0, where N is a map from R x C2>Q(ft) into C 2 ' a ( f i ) , a G (0,1), defined as: N:(X,V) —» V + A-^XfixfaiV)). 74 Chapter 3. Compactness along Lower Branches Moreover, dvN(\*2,V*) = U + A - 1 ( ^ M ^ ) is an invertible map since —A — X2f(x)g'e(V*) has no zero eigenvalues. The implicit function theorem gives the existence of a curve W\, A G (X2 — 6,X2 + S), of solution for (3.2.2) so that l im A - ,Aj W\ = V * in C 2 , a ( Q ) . Up to take 8 smaller, this convergence implies that /J.2,\(W\) > 0 and W\ < 1—£ for any A £ (X2—8, X2+6). Hence, W\ is a solution of (S)\ so that u.2t\{W\) > 0, contradicting the definition of X2. Therefore, y2t\*{V*) = 0, which completes the proof of Theorem 3.1.5. ' • 3.6 The one dimensional problem In this section, we discuss the compactness of solutions for (S)\ in one dimensional case. Recall that u.k:xn{un) is the fc—th eigenvalue of LUn^\n counted with their multiplicity. P r o o f of T h e o r e m 3.1.6: Let I = (a, 6) be a bounded interval in R. Assume / E C ^ / ) so that / > C > 0 in I. We study solutions un of {S)\n in the form A„/ (x) . T -""= U-u )2 i n 7 ' 0 < u n < l i n / , [ 6 - ° A ) { un{a) = Un(b) = 0. Assume that un satisfy (3.1.7) and A n —» X G (0, A*]. Let xn G / be a maximum point: un(xn) = m a x u „ . If (un)n is not compact, then up to a subsequence, we may assume that un(xn) —> 1 with xn —> xo G / as n —> +oo. Away from xo, un is uniformly far away from 1. Otherwise, by the maximum principle we would have un; —> 1 on an interval of positive measure, and then yk,xn iun) < 0 f ° r any k and n large, a contradiction. Assume, for example, that a < XQ < b. B y elliptic regularity theory, un(x) is uniformly bounded for x far away from XQ. Letting e > 0, we multiply (3.6.1) by un and integrate on (xn,x0 + e): = 2 A n / ( x 0 + £) _ 2 A „ / ( x n ) _ p + £ 2 A n / Q ) ^ Then, for n large: u „ m + i ? — \ ^ u n ( a ; o + e) + 2A„- ; r - 2A„ / j^r ™v n ' l-un(xn) ™v l-un(x0 + e) JXn l-un{s) < C £ + 4 A H/l loo ds e) " A n l - « n W XQ + £ - XN 1 ^ n ( ^ n ) since un(xn) is the maximum value of un in / . Choosing e > 0 sufficiently small, we get that for any n large: 1 _ u ^ X n ) < C £ , contradicting un(xn) - > l a s n - » +oo. • 75 Chapter 4 Dynamic Deflection 4.1 Introduction The rest of this thesis is devoted to the dynamic deflection of the elastic membrane satisfying (1.2.30). Throughout this Chapter and unless mentioned otherwise, for convenience we study dynamic solutions of (1.2.30) in the form ^ - A U = 7M% for xeQ, (4.1.1a) at (1 — uy u(x,t) = 0 for x £ dn, u(x,0) = 0 for z £ ft, (4.1.1b) where nonnegative / £ Ca(Cl) for some a € (0,1] describes the permittivity profile of the elastic membrane shown in Figure 1.1, while A > 0 characterizes the applied voltage, see §1.3.2. In this Chapter we deal with issues of global convergence, finite and infinite time "touch- down" , and touchdown profiles as well as pull-in distance. Recall that a point XQ £ Q is said to be a touchdown point for a solution u(x,t) of (4.1.1), if for some T £ (0, +oo], we have lim u(xo,tn) — 1. T is then said to be a -finite or infinite- touchdown time. For each such solution, we define its corresponding -possibly infinite- "first touchdown time": T A ( 0 , / , u ) = i n f it £ (0,+oo]; supu{x,t) = l ) . xen ' We first analyze the relationship between the applied voltage A, the permittivity profile / , and the dynamic deflection of the elastic membrane. It is already known that solutions correspond- ing to large voltages A necessarily touchdown in finite time (see [32]). The following theorem proved in §4.2 completes the picture. T h e o r e m 4.1.1. Suppose A* := A*(Q, / ) is the pull-in voltage defined in Theorem 2.1.1, then the following hold: 1. If A < A*, then there exists a unique solution u(x,t) for (4.1.1) which globally converges as t —> +oo, monotonically and pointwise to its unique minimal steady-state. 2. If A > A* and inff}/ > 0, then the unique solution u(x,t) of (4.1.1) must touchdown at a finite time. This "touchdown" phenomenon is referred to sometimes as quenching. Note that in the case where the unique minimal steady-state of (4.1.1) at A — A* is non-regular - which can happen if N > 8 - the above result means that the corresponding dynamic solution must touchdown but that quenching occurs here in infinite time. In §4.3 we shall establish that -an isolated- touchdown cannot occur at a point in Q where the permittivity profile is zero, a fact that was observed numerically and conjectured to hold in [32]. More precisely, we prove the following. 76 Chapter 4. Dynamic Deflection T h e o r e m 4.1.2. Suppose u(x,t) is a touchdown solution of (4.1.1) at a finite time T, then ut > 0 for allO <t <T. Furthermore, 1. The permittivity profile f cannot vanish on an isolated set of touchdown points in ft. 2. On the other hand, zeroes of the permittivity profile can be locations of touchdown in infinite time. In §4.4 we shall provide upper and lower estimates for finite touchdown times. Uniqueness considerations lead to a first touchdown time T\(ft, f) that only depends on the domain ft and on the profile / . These touchdown times translate into useful information concerning the speed of the operation for many M E M S devices, such as Radio Frequency (RF) switches and microvalves. Estimates (4.1.4) and (4.1.5) below were already established in [32] for large A. Considering that A* < min{Ai,A2}, the estimate (4.1.3) below gives an upper bound on the first touchdown time as soon as we exceed the pull-in voltage A*. T h e o r e m 4.1.3. Suppose f is a non-negative continuous function on a bounded domain ft, and let T\(ft, / ) be the first -possibly infinite- touchdown time corresponding to a voltage A. 1. The following lower estimate then holds for any A > 0: r r 1—Ff^ < TX(Q, / ) . (4.1.2) 3Asup x e S 7 / ( a ; ) 2. If mixen f(x) > 0, then the following upper estimate holds for any A > A*: ua, n < w;)3i„tim/(^;_A;).;(A+3A.) v + , / 2 i . w 3. Ifmixenf{x) > 0, and A > Ai := 2imi^S(x)' t h e n Un,f) < T M ( f t , / ) := jf1 [ ^ ^ m - ^ d s . (AAA) T A ( f t , / ) < T 2 , A (ft, / ) : = - — log / f<t>ndx)-\ (4.1.5) Here ^n and </>n are the first eigenpair of —A on HQ(CI) with normalized fa <pndx = 1. Note that the upper bounds TO,A and T\:\ are relevant only when / is bounded away from 0, while the upper bound T2j\ is valid for all permittivity profiles provided of course that A > A 2 . In §4.5 we discuss touchdown profiles by the method of asymptotic analysis, and our purpose is to provide some information on the refined touchdown rate discussed in next Chapter. §4.6 is devoted to the pull-in distance of M E M S devices, referred to as the maximum stable deflection of the elastic membrane before touchdown occurs. We provide numerical results for pull-in distance with some explicit examples, from which one can observe that both larger pull-in distance and pull-in voltage can be achieved by properly tailoring the permittivity profile. 77 Chapter 4. Dynamic Deflection 4.2 Global convergence or touchdown In this section, we analyze the relationship between the applied voltage A, the permittivity profile / , and the dynamic deflection u of (4.1.1). We first prove in §4.2.1 global convergence in the case A < A*. In §4.2.2 we study finite-time touchdown for the case A > A*. Finally we discuss the case A = A* in §4.2.3. First, we note the following uniqueness result. Lemma 4.2.1. Suppose u\ and u2 are solutions of (4.1.1) on the interval [0,T] such that ll uillL~(nx[o,r]) < 1 fori = 1,2, thenui = u2. Proof: Indeed, the difference U = u\ — u2 then satisfies Ut-AU = aU in Q (4.2.1) with initial data U(x, 0) = 0 and zero boundary condition. Here A(2 - m - u2)f(x) a(x,t) = ( 1 - U l ) 2 ( l - u 2 ) 2 ' The assumption on ui,u2 implies that a(x,t) e L°°(f2 x [0,T]). We now fix T i £ [0,T] and consider the solution <fi of the problem ' <t>t + A<t> + a<t> = 0 x e ft, 0 < t < Ti, <t>{x,Ti) = 6(x)£C0(Q), (4.2.2) <f>(x,t) = 0 xedCl, The standard linear theory (cf. Theorem 8.1 of [47]) gives that the solution of (4.2.2) is unique and bounded. Now multiplying (4.2.1) by <j>, and integrating it on Q x [0,Ti], together with (4.2.2), yield that / U(x,T1)6{x)dx = 0 for arbitrary T\ and 0(x), which implies that U = 0, and we are done. • 4.2.1 G l o b a l c o n v e r g e n c e w h e n A < A* Theorem 4.2.2. Suppose A* := A*(fi, / ) is the pull-in voltage defined in Theorem 2.1.1, then for A < A* there exists a unique global solution u(x, t) for (4.1.1) which monotonically converges as t —> +co to the unique minimal solution ux(x) of (S)\. Proof:: This is standard and follows from the maximum principle combined with the existence of regular minimal steady-state solutions at this range of A. Indeed, fix 0 < A < A*, and use Theorem 2.1.2 to obtain the existence of a unique minimal solution ux(x) of (S)\. It is clear that the pair u = 0 and u = ux(x) are sub- and super-solutions of (4.1.1) for all t > 0. This implies that the unique global solution u(x,t) of (4.1.1) satisfies 1 > ux(x) > u(x,i) > 0 in D. x (0, oo). B y differentiating in time and setting v = ut, we get for any fixed to > 0 vt = Av+ JX^X\v i € f l , 0 < t < t o , (4.2.3a) (1 — u)6 78 Chapter 4. Dynamic Deflection v(x,t) = 0 x G d f t , « ( i , 0 ) > 0 (4.2.3b) Here l s a locally bounded non-negative function, and by the strong maximum principle, (_! U) we get that ut — v > 0 for (x, t) G ft x (0, to) or ut = 0. The second case is impossible because otherwise u(x,t) = u\(x) for any t > 0. It follows that ut > 0 holds for all {x,t) G . f t x (0,oo), and since u(x, t) is bounded, this monotonicity property implies that the unique global solution u(x,t) converges to some function us(x) as t —> oo. Hence, 1 > u\(x) > us(x) > 0 in ft. Next we claim that the limit us[x) is a solution of (S)\. Indeed, consider a solution u\ of the linear stationary boundary problem - A m = , X^X\0 x G f t , u i = 0 x G d f t . (4.2.4) Let w(x,t) = u(x,t) — u\(x), then w satisfies wt-Aw = Xf(x) [ 1 - 1 ] , ( i , < ) € f i x (0, T ) ; (4.2.5a) w(x,t) = 0 x e 3 ( ] x ( 0 , T ) ; iu(x, 0) = -ui(x) x G f t . (4.2.5b) Since the right side of (4.2.5a) converges to zero in L 2 (f t ) as t —» oo, a standard eigenfunction expansion implies that the solution w of (4.2.5) also converges to zero in L 2 ( Q ) as t —> oo. This shows that u(x,t) —> u i ( x ) in L 2 ( f t ) as t —> oo. But since u(x,t) —> w s ( x ) pointwise in ft as t —> oo, we deduce that u\(x) = us(x) in L 2 ( f t ) , which implies that u s ( x ) is also a solution for (S)x- The minimal property of ux(x) then yields that ux(x) = us(x) on O, which follows that for every x G ft, we have u(x,£) ] ux(x) as t ^> oo. • 4.2.2 Touchdown at finite time when A > A* Recall from Theorem 2.1.1 that there is no solution for (S)\ as soon as A > A*. Since the solution u(x,t) of (4.1.1) -whenever it exists- is strictly increasing in time t ((see preceding theorem)), then there must be T < oo such that u(x, t) reaches 1 at some point of ft as t —» T~. Otherwise, a proof similar to Theorem 4.2.2 would imply that u(x,t) would converge to its steady-state which is then the unique minimal solution u\ of (S)\, contrary to the hypothesis that A > A*. Therefore for this case, it only remains to know whether the touchdown time is finite or infinite. This is exactly what we prove in the following. T h e o r e m 4.2.3. Suppose A* := A*(ft , /) is the pull-in voltage defined in Theorem 2.1.1. If i n f x e n f(x) > 0, then for A > A* there exists a finite time T\(ft, / ) at which the unique solution u(x,t) of (4.1.1) must touchdown. Moreover, we have the bound T t Q f X T 8(A + A*) 2 r . A + 3A-N1 /2- , T. ( f t , / ) < T 0 , A . - 3 f { x ) { x _ A , ) 2 ( A + m [1 + ( ^ X ~ T ^ ) J- (4.2.6) We start by transforming the problem from a touchdown situation (i.e. quenching) into a blow-up problem where a concavity method can be used. For that, we set V = 1/(1 — u) which 79 Chapter 4. Dynamic Deflection reduces (1.1) to the following parabolic problem Vt = AV- 2 I ^ I 2 + \f(x)V4 for xGQ, V for x £ dCl, for x Gil. (4.2.7a) (4.2.7b) (4.2.7c) V{x,t) = 1 V{x,0) = 1 This transformation implies that when A > A*, the solution of (4.2.7) must blow up (in finite or infinite time) and that there is no solution for the corresponding stationary equation: 2 | V V | 2 A V - V + A / ( x ) V 4 = 0, x e f t ; V = l , xedQ. (4.2.8) Therefore, proving finite touchdown time of u for (1.1) is equivalent to showing finite blow-up time of the solution V for (4.2.7). For the proof, we shall first analyze the following auxiliary parabolic equation vt = Av - 1^1- + \G2t2f{x)vi for x e f t , (4.2.9a) v v = l for x e dfl, (4.2.9b) v(x,0) = l for i £ f i , (4.2.9c) where a > 0 is a given constant. L e m m a 4.2.4. Suppose v is a solution of (4.2.9) up to a finite time T, then ( ^ i ) t > 0 for all t < f. Proof : Dividing (4.2.9a) by u 4 , we obtain Av 2 |Vv | : v* vH v° Setting w = v~3, then direct calculations show that 2\\7w\2 + \a2t2f(x) wt — Aw + + 3 A a 2 i 2 / ( x ) = 0. 3w (4.2.10) Differentiate (4.2.10) twice with respect to t, we obtain f\\7w\2\ _ {2\7wVwt \Ww\2wt\ V w TVwWwtt 2\S7wt\ 4Vw\7wtwt \Vw\2wtt 2\S/w\2wf w which means that the function satisfies w z = wtt + w° 4Vw L(z) : = zt - Az + ——Vz 2\Vw\2 (4.2.11) 3w 3w2 = - 6 A a 2 / ( x ) - < - 6 A a 2 / ( x ) , 2 | V w t | 2 2\Ww\2w2 4WwVwtwt + wJ 80 Chapter 4. Dynamic Deflection after an application of Cauchy-Schwarz inequality. Hence we have L{z) < - 6 A a 2 / ( x ) < 0. (4.2.12) Now from (4.2.9) and the definition of z, we have z(x,0) = 0 and z — 0 on 9ft. Since the coefficients of L remain bounded as long as v is bounded, we conclude that z(x,t) < 0 holds for all t < T. This completes the proof of Lemma 4.2.4. • P r o o f of T h e o r e m 4.2.3: Let A > A*, and set A' = A - A* > 0, 5 = i n f x € n f(x) > 0, and 4 A * + A ' \ i / 2 - i 3<5A'(4A* + A') ao — 4(2A* + A') I1 {2(2\* + \<)J J ' and T0,x = 1 8(A + A*) 2 p. . f A + 3A* \ i / 2 a 0 3 6 ( A - A*) 2(A + 3A*) i + ( s w n < - - ^ .2A + 2A*. Consider now a solution v of (4.2.9) corresponding to A = A* + A' and ao as defined in (4.2.13a). We first establish the following C l a i m : There exists XQ £ ft such that v(xo,t) —> oo as t / T0t\. Indeed, let t0 = ^ [ 2 ( 2 A * * ~ + Y ) ] M S U C N A W A Y T N A T A' A' t0<T0tX and ogtg(A* + - ) = A* + - . We claim that there exists XQ £ ft such that Av(x0,t0) ~ 2 | V ! ( 3 : 0 ; t ; ) | 2 + (A* + y ) / ( s 0 ) M z 0 ) t o ) | 4 > °" ^ 2 ' 1 4 ) u(xo,to) 4 Essentially, otherwise we get that for all x £ ft Av(x,t0) - 2 | V y ( 3 : ' f ° ) | 2 + (A* + %)f(x0)\v(x,t0)\4 < 0. (4.2.15) v[x,t0) 4 Since v(x,to) > 1 on ft and hence on ft, this means that the function v(x) = v(x,to) is a supersolution for the equation A y _ 2 | W | 2 + A ^ y 4 = 0 > V = l, x£8Q. (4.2.16) Since t> = 1 is obviously a subsolution of (4.2.16), it follows that the latter has a solution which contradicts the fact that A = A* + ^ > A*(/,f t) . Hence, assertion (4.2.14) is verified. On the other hand, we do get from (4.2.9) that for t = to and every x £ ft, V t = Av- + (A* + ^)f(x)v* + ^altlf(x)v4 . (4:2.17) V 4 z We then deduce from (4.2.17) and (4.2.14) that at the point (xo,£o), we have £ > y<#g/(*o) > 0. 81 Chapter 4. Dynamic Deflection Applying Lemma 4.2.4, we then get for all {xo,t), to < t < To,\ that: $ > %4tlf(x0) > 0. (4.2.18) Integrating (4.2.18) with respect to t in (toi^o^), we obtain since f(xo) > 5 that: ^(1 - v-3(x0,To,x)) > jalt2of(xo)(T0iX - t0) > ja2t26(T0<x - t0) = | . It follows that V(XQ, t) —> oo as t f Tot\, and the claim is proved. To complete the proof of Theorem 4.2.3, we note that since a^t2 < 1 for all t < T0,\, we get from (4.2.9) that vt<Av- - ! — - J - + Xf(x)v4 , ( i , f ) 6 ( l x ( 0 , T 0 , A ) . Setting w = V — v, where V is the solution of (4.2.7), then w satisfies . 2 V ( V + v ) _ r . , „ , . . . . , . . 2 |Vur wt — Aw — vw + Here the coefficients of Vw and w are bounded functions as long as V and v are both bounded. It is also clear that w = 0 on dSl and w(a;,0) = 0. Applying the maximum principle, we reduce that w > 0 and thus V > v. Consequently, V must also blow up at some finite time T < Tot\, which means that u must touchdown at some finite time prior to To,A- ' Remark 4.2.1. A slightly revised proof of Theorem 4.2.3 can be essentially adopted to prove finite-time touchdown for the case where A > A* and f(x) > 0 is almost everywhere on Cl. The extension to more general nonnegative profile f(x) is now in progress. 4 . 2 . 3 G l o b a l c o n v e r g e n c e o r t o u c h d o w n i n i n f i n i t e t i m e f o r A = A* In order to complete the proof of Theorem 4.1.1, the rest is to discuss the dynamic behavior of (4.1.1) at A = A*. For this critical case, there exists a unique steady-state w* of (4.1.1) obtained as a pointwise limit of the minimal solution u\ as A | A*. If w* is regular (i.e, if it is a classical solution such as in the case when N < 7) a similar proof as in the case where A < A*, yields the existence of a unique solution u*(x, t) which globally converges to the unique steady-state w* as t —» oo. On the other hand, if w* is a non-regular steady-state, i.e. if ||u;*||oo = 1> the situation is complicated as we shall still prove global convergence to the extremal solution, which then amounts to a touchdown in infinite time. Throughout this subsection, we shall consider the unique solution 0 < u* = u*(x,t) < 1 for the problem u*t - Au* = **^X\„ for (x, t ) £ ( l x [0, **), (4.2.19a) (l — u*y u*{x,t)=0 for i e 9 Q x [ 0 , O , (4.2.19b) u*{x,0) = 0 for xeCl, (4.2.19c) where t* is the maximal time for existence. We shall use techniques developed in [10] to establish the following X(V2 +v2)(V + v)f(x) + -y^-]™ > 0, (x,t) € Cl x (0,T0,x). 82 Chapter 4. Dynamic Deflection Theorem 4.2.5. If w* is a non-regular minimal steady-state of (4.2.19), then there exists a unique global solution u* of (4.2.19) such that u*(x,t) < w*(x) for all t < oo, while u*(x,t) —> w*(x) as t —> oo. In particular, l im ||u*(x,t)lloo = 1- t—>+oo The proof of Theorem 4.2.5 needs to use the following lemma. Lemma 4.2.6. Consider the function 6(x) := dist(:r, dCl), then for any 0 < T < oo, there exists e\ = Ei{T) such that for 0 < e < E\ the solution Z£ of the problem Zt-AZ = -ef(x) in Q x (0, oo), Z(x,t) = 0 on S O x ( 0 , o o ) , Z(x,0) = 5{x) in 0 satisfies ZE > 0 on [0,T] x Cl. Proof: Let (T(t))t>Q be the heat semigroup with Dirichlet boundary condition, and consider the solution £o of - A £ o = 1 in Cl; Co = 0 on dQ. then we have ^ Co = T(t)Co+ / T(s)lnds Jo for all t > 0. Since T(t)£0 > 0, it follows that / T{s)lQds < Co < C5 for all £ > 0 . (4.2.20) Jo On the other hand, we have Z£{t) = T(t)5-sf fr^lnds, Jo and so we have Z£(t) > T(t)5 — sC5. Consider now Co, Ci > 0 such that co</>i < 5 < c\<f>\, where (f>\ is the first eigenfunction of —A in HQ(CI), associated to the eigenvalue pt,\. We have T(t)5 > c0T(t)4>i = coe-^fa > - e ' ^ d . Cl Therefore, we have Z£(t) > (f^-^ - CE)5. And hence it follows that Ze{t) > 0 on [0,T] provided s < ffceT^• • Proof of Theorem 4.2.5: We proceed in four steps. Claim 1. We have that u*(x,t) < w*(x) for all (x,t) eClx [0,t*). Indeed, fix any T < t* and let £ be the solution of the backward heat equation: £t - A f = h(x,t) in Cl x (0,T), C|aa = 0, C(r) = 0, 83 Chapter 4. Dynamic Deflection where h(x,t) > 0 is in Q. x (0,T). Multiplying (4.2.19) by £ and integrating on Q x (0,T) we find that _ / / u*hdxdt= [ [ Xyf<"Xl dxdt. Jo Jn Jo Jn (1 - u*) 2 On the other hand rT £ J w*it dxdt = J w*£(0)dx and - J w*A£dxdt = J - ^ ^ ^ dxdt. Therefore, we have rT dxdt f1 [ (u* -w*)hdxdt< [ w*£(Q)dx+ f f {u*-w*)hdxdt Jo Jn Jn Jo Jn <C [ f {u* -w*)+£dxdt, Jo Jn since ||w*||oo < 1 for £ e [0,T). Therefore, we have £ J (n* -w*)hdxdt<c(J* J \{u* - w*)+\2 dxdt}11*J dxdt)1'2. On the other hand, £{x,t) = T(s — t)h(x, s)ds, where T(t) is the heat semigroup with Dirichlet boundary condition, and hence t)fL2 < ( jT \\h(x, s)\\L2ds)2 <(T-t)£ J h2 dxdt. Therefore, / / £2 dxdt < ^ / / h 2 d x d t ' Jo Jn 2 J0 Jn and so, £ J {u* - w*)hdxdt < ^~ ( jT j \{u* - w*)+}2 dxdt) V 2 ( £ J h2 dxdt) Letting h converge to (u* — w*)+ in L2, and since u* — w* S LX(Q) we have fT f {{u* - w*)+}2 dxdt < ^ F [ \{u* - w*)+)2 dxdt, Jo Jn v 2 Jo Jn which gives that u* < w* provided C2T2 < 2, and our first claim follows. 1 / 2 84 Chapter 4. Dynamic Deflection Claim 2. There exist 0 < T\ < t*, and Co, CQ > 0 such that for all x € Q U"{X,TI) < mm{C0S{x); w*{x) - CQ6(X)} . (4.2.21) F i x 0 < T < t* sufficiently small, and let v be the solution of vt - Av = / n 1 \> for (x, i) e fi x [0, f ) , (4.2.22a) ( 1 - f ) 2 v(x,t)=0 for xedflx[0,T), (4.2.22b) v(x,0) = v0 =U*(X,T) for xeCl, (4.2.22c) where [0,T) is the maximal interval of existence for v. Similarly to Claim 1, we can show that 0 < v < w*. Choose now K > 1 sufficiently large such that the path z(x,t) := u*(x,t) + T(T{t)vQ satisfies ||z(a;,<)||oo < 1 for 0 < i < T . We then have z(x,t) = 0 on 9 Q x ( 0 , T ) , z(x,0) = ^ M in n , and the maximum principle gives that z < v. Consider now a function 7 : [0,00) —> R such that 7(t) > 0 and T(t)v0 > K-y{t)5 on Q. (4.2.23) We then get u* < v - ^T{t)v0 <w*- ^T{t)v0 < w* - j{t)6 for 0 < t < f . (4.2.24) On the other hand, for any 0 < t < T < t*, u* is bounded by some constant M < 1 on Q x [0, T] such that u* < MT{t)\u + ( 1 _ C M ) 2 J T(s)lQds. Consider now a function C : [0,00) —> R such that T(t)ln, < C(t)5 for t > 0, which means that u* < MC(t)5 + C{M)CS for any 0 < t < T, where (4.2.20) is applied. This combined with (4.2.24) conclude the proof of Claim (4.2.21). Claim 3. For 0 < e < 1 there exists we satisfying ||we||oo < 1 and / Vw£Vtp> f ( 1 - e ) A V / 0 ) (4-2.25) for all <p 6 ^ o ( ^ ) w ^ n <p > 0 on Q. Moreover, there exists 0 < E\ < 1 such that for 0 < e < £i , we also have 0 < w£(x) - ^d(x) for i t f i (4.2.26) 85 Chapter 4. Dynamic Deflection Co being as in (4.2.21). To prove (4.2.25), we set For any e e (0,1) we also set 1 ~ fw" ds 9(w*) = T . ^ ~ e , h(w*)= — , 0<w*<l, (4.2.28) (i - w*V Jo 9{s) • and tj>e{w*) := h~l (h(w*)). It is easy to check that <f>£(0) = 0 and 0 < <f>£{s) < s for s > 0, and <j>e is increasing and concave with Setting w£ = 4>£(w*), we have for any <p € HQ(Q) with <p > 0 on Q, f Vw£V<p= f <p'£(w*)Vw*\7<p= [ V w * V (<f>'E(w*)<p) - [ $(w*)<p\Vw*\2 Jn Jn Jn Jn which gives (4.2.25) for any e € (0,£o)- In order to prove (4.2.26), we set rj{x) =mm{w*(x),(C0 + co)S(x)} and rj£ = <f>£ori, where (j>£(-) is denned above, and Co and Co are as in (4.2.21). Since rj < w* and (f>£ is increasing, we have r/e < <f>£(w*) = w£. Applying (4.2.21) we get that 0 < rj{x) - c05{x) on n. (4.2.29) We also note that rj£ = <j>£(n) < r] < M with M = (Co + CQ)5(X), and (j>'£(s) —> 1 as e —> 0 uniformly in [0,1]. Therefore, for some 9 £ (0,1) we have V-Ve=V- (Mv) - 0S(O)) = r?(l - <fi'£(6v)) < V sup (1 - {0<s<l} <(Co + c 0)5 sup ( l {0<s<l> 1 provided e small enough, which gives rj<rj£ + ^S. (4.2.30) We now conclude from (4.2.29) and (4.2.30) that 0 < r? - c06 < rj£ - — 5 < w£ - — <5 86 Chapter 4. Dynamic Deflection for small e > 0, and (4.2.26) is therefore proved. To complete the proof of Theorem 4.2.5, we assume that t* < oo and we shall work towards a contradiction. In view of Claim 3), we let e > 0 be small enough so that 0 < w£ — ̂ -5. Use Lemma 4.2.6 and choose K > 2 large enough such that the solution Z of the problem Zt-AZ = -e\*f(x) in fix (0, t*), Z{x,t)=0 on dSlx(Q,t*), Z(x,0) = ^6 in SI satisfies 0 < Z < 1 - u* on Cl x (0,£*). Let v be the solution of vt- Av= ( ^ J ^ a ~£)x*f(x) i n fix(0,s*), v{x,t)=0 on d Q x ( 0 , s * ) , f(a;, 0) = w£ in , where [0, s*) is the maximal interval of existence for v. Setting z(x,t) = Z(x,t) +u*(x,t) for 0 < t < t*, we then have 0 < u* < z < 1 and z t - A z = ( 1 - e ) A V ( a : ) < - e ) A V W in fix ( 0 , 0 , 2(a:,t)=0 on 9 J 2 x ( 0 , i * ) , z(x, 0) = ~j£$(x) — wz{x) in SI. Now the maximum principle gives that z < v on SI x (0, min{s*, £*})> and in particular we have 0 < v on SI x (0, min{s*,i*}). Furthermore, the maximum principle and (4.2.25) also yield that v < w£. Since || ^ellcx) ^ f we necessarily have t* < s* — oo. Therefore, u* ^ z ^ v ^ i f e on [0,£*)> which implies that ||«*||oo < 1 at t = t*, which contradicts to our initial assumption that u* is not a regular solution. • 4.3 Location of touchdown points In this section, we first present a couple of numerical simulations for different domains, different permittivity profiles, and various values of A, by applying an implicit Crank-Nicholson scheme (see [32] for details) on (4.1.1). For the connection with the involved figures below, we discuss (4.1.1) in the form of u(x,t) = 0 for xedSl; u(x,0) = 0 for xeSl, (4.3.1b) with the following two choices for the domain SI SI: [-1/2,1/2] (slab); Sl:x2+y2<l (unit disk). (4.3.2) 87 Chapter 4. Dynamic Deflection Figure 4.1: Left Figure: u versus x for A = 4.38. Right Figure: u versus x for A = 4.50. Here we consider (4.3.1) with f(x) = \2x\ in the slab domain. S i m u l a t i o n 1: We consider f(x) = \2x\ for a permittivity profile in the slab domain —1/2 < x < 1/2. Here the number of the meshpoints is chosen as N — 2000 for the plots u versus x at different times. Figure 4.1(a) shows, for A = 4.38, a typical sequence of solutions u for (4.3.1) approaching to the maximal negative steady-state. In Figure 4.1(b) we take A = 4.50 and plot u versus x at different times t = 0, 0.1880, 0.3760, 0.5639, 0.7519, 0.9399, 1.1279, 1.3159, 1.5039, 1.6918, 1.879818, and a touchdown behavior is observed at two different nonzero points x = ±0.14132. These numerical results and Remark 4.2.1 point to a pull-in voltage 4.38 < A* < 4.50. <a). - i arm X - 1.70 <b). HO - i «nd i. - i .00 Figure 4.2: Left Figure: u versus r for A = 1.70. Right Figure: u versus r for A = 1.80. Here we consider (4.3.1) with f(r) = r in the unit disk domain. S i m u l a t i o n 2: Here we consider / ( r ) = r for a permittivity profile in the unit disk domain. The number of meshpoints is again chosen to be N = 2000 for the plots u versus r at different times. Figure 4.2(a) shows how for A = 1.70, a typical sequence of solutions u for (4.3.1) approach to the maximal negative steady-state. In Figure 4.2(b) we take A = 1.80 and plot u versus r at different times t = 0, 0.4475, 0.8950, 1.3426, 1.7901, 2.2376, 2.6851, 3.1326, 3.5802, 4.0277, 4.4751942, and a touchdown behavior is observed at the nonzero points r = 0.21361. Again these numerical results point to a pull-in voltage 1.70 < A* < 1.80. 88 Chapter 4. Dynamic Deflection One can observe from above that touchdown points at finite time are not the zero points of the varying permittivity profile / , a fact firstly observed and conjectured in [32]. The main purpose of this section is to analyze this phenomena. T h e o r e m 4.3.1. Suppose u(x,t) is a touchdown solution of (4.1.1) at a finite time T, then we have 1. The permittivity profile f cannot vanish on an isolated set of touchdown points in ft. 2. On the other hand, zeroes of the permittivity profile can be locations of touchdown in infinite time. Note that Theorem 4.3.1 holds for any bounded domain. The proof of Theorem 4.3.1 is based on the following Harnack-type estimate. L e m m a 4.3.2. For any compact subset K of ft and any m > 0, there exists a constant C = C(K,m) > 0 such that supxeK \u(x)\ < C < 1 whenever u satisfies 771 A u > - x e f t ; 0 < u < l z e f t . (4.3.3) (1 — u)z Proo f : Setting v = 1/(1 — u), then (4.3.3) gives that v satisfies Av 2\Wv\2 2 . 5 — > mv in ft, which means that v is a subsolution of the "linear" equation Av = 0 in ft. In order to apply the Harnack inequality on v, we need to show that for balls Br C ft, we have that v G L3(Br) with an L 3 -norm that only depends on m and the radius r. Without loss of generality, we may assume 0 G K C ft. Let Br = Br(Q) C K be the ball centered at x = 0 and radius r. For 0 < n < r 2 < 4r\, let rj(x) G C o ° ( 5 r 2 ) be such that n = 1 in Bri, 0 < 77 < 1 in BT2 \BT1 and |Vr7| < 2/(r2-rl). Multiplying (4.3.3) by (j)2/(l-u), where A = r)a and a > 1 is to be determined later, and integrating by parts we have f mcf f fAu f <f>2\\7u\2 _ f 2<t>W<j> • Wu JBr2 (1 - „)3 - 1 - „ JBr2(l-u)2 JBr2 ' From the fact, / , ! W + 4 / ^ + 4 / J» 1 - u JBrn Y JBn (1 - u)2 JB (1 - u)2 JB (1 - u JT1 (4.3.4) gives that ) 2 m(f>2 ^ A f W „ ( i - « ) 3 - 4 7 , ( 1 - l i ) Jr2 v ' " " r 2 Now choose (f> = rj213 with /3 = | . Then Holder's inequality implies that „4/3 / iVryl 4^' V 2 ( i - U ) 3 — L ; ^ 1 " " J uBr2(i-u) 20 V A0 2 g - l 20 89 Chapter 4. Dynamic Deflection This shows that By virtue of the one-sided Harnack inequality, we have II Y ~ \\L°°(B^=11 v | |L<X. ( b )< C ( n ) || v | U s ( B r i ) < C(n,m). The rest follows from a standard compactness argument. Proof of Theorem 4.3.1: Set v = ut, then we have for any t\ < T that vt = Av+ JXfi-X},v ( x , i ) G f i x ( 0 , i i ) ; (4.3.6a) (1 — u)° v{x,t) = Q (x,t) 6 dCl x (0 , i i ) ; v ( x , 0 ) > 0 x G Q. (4.3.6b) Note that the term is locally bounded in Q x (0,t i) , so that by the strong maximum principle, we may conclude ut = v > 0 for (x, t) G fi x (0 , i i ) (4.3.7) and therefore, ut > 0 holds for all (x, i) G x (0, T ) . Since K is an isolated set of touchdown points, there exists an open set U such that K C U C U C with no touchdown points in C/ \ K. Consider now 0 < to < T such that inixeQ ut(x,to) = C\ > 0. We claim that there exists e > 0 such that J e ( x , t)=ut- , ^ . 2 > 0 for all (x, t) G C x (t 0, T ) , (4.3.8) (1 tt) Indeed, there exists C2 > 0 such that u t (x, T) > C2 > 0 on U, and since dt/ has no touchdown points, there exists e > 0 such that J e > 0 on the parabolic boundary of U x (to,T). Also, direct calculations imply that Since is locally bounded on U x (to, T ) , we can apply the maximum principle to obtaining (4.3.8). " If now i n f - t gx / ( x ) = 0, then we may combine (4.3.8) and (4.1.1), to deduce that for a small neighborhood B c U of some point xo G K where f(x) < e/2, we have A x / > ^ . , 1 f o r ( x , t ) G 5 x ( t 0 , T ) . 2(1— u j z In view of Lemma 4.3.2, this contradicts the assumption that xo is a touchdown point. For the second part, recall from Theorem 2.1.2 that the unique extremal solution for the stationary problem on the ball in the case N > 8 and for a permittivity profile f(x) = | x | Q , is u*(x) = 1 — |x| 3 ° as long as a is small enough. Theorem 4.1.1 then implies that the origin 0 is a touchdown point of the solution even though it is also a root for the permittivity profile 90 Chapter 4. Dynamic Deflection (i.e., /(O) = 0). This complements the statement of Theorem 4.3.1 above. In other words, zero points of / in ft cannot be on the isolated set of touchdown points in finite time (which occur when A > A*) but can very well be touchdown points in infinite time of (4.1.1), which can only happen when A = A*. The proof of Theorem 4.3.1 fails for touchdowns in infinite time, simply because the maximum principle cannot be applied in the infinite cylinder ft x (0, oo). • 4.4 Estimates for finite touchdown times In this section we give comparison results and explicit estimates on finite touchdown times of dynamic deflections u = u(x,t). This often translates into useful information concerning the speed of the operation for many M E M S devices such as R F switches or micro-valves. 4.4.1 Comparison results for finite touchdown time We start by comparing the effect on finite touchdown time of two different but comparable permittivity profiles f(x), at a given voltage A. T h e o r e m 4.4.1. Suppose u\ = u\(x,t) (resp., u2 = u2(x,t)) is a touchdown solution for (4.1.1) associated to a fixed voltage X and permittivity profiles f\ (resp., f2) with a corresponding finite touchdown time T \ ( f t , / i ) (resp., Tx(Q,f2)). If f\(x) > f2(x) on ft and if f\{x) > f2(x) on a set of positive measure, then necessarily T\(ft, fi) < T\(ft, f2). Proo f : B y making a change of variable v — 1 — u, we can assume to be working with solutions of the following equation: < ^ „ A v = _hiW f o r i e f i i (4.4.1a) at vl v(x,t) = l for x£dQ, (4.4.1b) v(x,0) = l for x e f t , (4.4.1c) where / is either f\ or f2. Suppose now that T \ ( f t , / i ) > T\(Q,f2) and let fto C ft be the set of touchdown points of u2 at finite time T\(ft, f2). Setting w — u2 — u\, we get that W t _ A w _ X ^ u \ + / ^ w = A ^ ~ ^ > 0 ( x , £ ) e f t x ( 0 , 2 M f t , / 2 ) ) . (4.4.2) u\u^ U\U2 Since w = 0 at t = 0 as well as on 9 f t x (0, T\(Q, f2)), we get from the maximum principle that w cannot attain a negative minimum in ftx (0, T\(ft, f2)), and therefore w > 0 in ftx (0, T\(ft, f2)). Since u2 —> 0 in fto as t —> T\(ft ,/2), and since our assumption is that T\(ft, f\) > T\(Q,,f2), we then have u i > 0 in fto as t —* T\(Q.,f2). Therefore, w < 0 in fto as t —> T\(Q,f2), which is a contradiction and therefore T\(ft, / i ) < T\(ft ,/2). To prove the strict inequality, we note that the above proof shows that w > 0 in ft x (0,T\(ft,/2)), which once combined with (4.4.2) gives that wt-Aw>0, in ft x ( i 1 , T x ( f t , / 2 ) ) ) where t\ > 0 is chosen so that w{x,t\) ^ 0 in ft. Now we compare w with the solution z of zt-Az = Q in ft x ( £ i , T A ( f t , / 2 ) ) 91 Chapter 4. Dynamic Deflection subject to z(x,t\) = w(x,t\) and z(x,t) = 0 on dCl x (t\,T\(Q,$2))- Clearly, w > z in Cl x (ti,Tx(Cl, f2))- On the other hand, for any to > t\ we have z > 0 in Cl x ( £ 0 , T x ( C l , / 2 ) ) . Consequently, w > 0 which means that u 2 > u i in Cl x (£ 0 , T ^ f i , /2)) and therefore Tx(Cl, fx) < Tx(n,h). m The second comparison result deals with different applied voltages but identical permittivity profiles. Theorem 4.4.2. Supposeux = u\(x,t) (resp., u2 = U2(x,t)) is a solution for (4.1.1) associated to a voltage X\ (resp., A 2 / ) and which has a finite touchdown time Tx1(Cl,f) (resp., T\2(Cl,f)). If Ai > A 2 then necessarily T ^ f i , / ) < T\2(Cl, f). Proof: It is similar to the proof of Theorem 4.4.1, except that for w — u 2 — u\, (4.4.2) is replaced by wt - Aw - X l i u \ + 2 U 2 ) f W = ( A l ~ 2 A 2 ) / > 0 (x,t)€Qx(0,T). u1u2 u2 The details are left for the interested reader. • Remark 4.4.1. A reasoning similar to the one found in Proposition 2.5 of [29], gives some information on the dependence on the shape of the domain. Indeed, for any bounded domain r in RN and any non-negative continuous function / on T, we have A*(r,/) > \*(BR,f*) andT A ( r , / ) >Tx(BR,f*), where BR = BR(0) is the Euclidean ball in RN with radius R > 0 and with volume \BR\ = |T|, where / * is the Schwarz symmetrization of / . We now present numerical results comparing finite touchdown times in a slab domain. Figure 4.3: Left Figure: plots ofu versus x for different f(x) at A = 8 and t = 0.185736. Right Figure: plots ofu versus x for different A with f(x) = |2x| and t = 0.1254864. Figure 4.3(a): Dependence on the dielectric permittivity profiles / We consider (4.3.1) for the cases where { \2x\ if \x\ < - ~ 8 ' (4.4.3) l / 4 + 2 s i n ( | a ; | - l / 8 ) otherwise. 92 Chapter 4. Dynamic Deflection Using N = 1000 meshpoints, we plot u versus x with A = 8 at the time t = 0.185736 in Figure 4.3(a). The numerical results show that the finite touchdown time T\ ( f i , / i ) for the case fi(x) and T A ( f i , / 2 ) for the case f2{x) are 0.185736 and 0.186688, respectively. Figure 4.3(b): Dependence on the applied voltage A Using N = 1000 meshpoints and the profile f(x) = \2x\, we plot u of (4.3.1) versus x with different values of A at the time t = 0.1254864. The numerical results show that finite touch- down time Tx1(Q.,f) for applied voltage A i = 10 and T\2(Cl,f) for applied voltage \ 2 = 8 are 0.1254864 and 0.185736, respectively. 4.4.2 Explicit bounds on touchdown times We now establish claims 1), 3) and 4) in Theorem 1.3 of the introduction. Note that here Ai > A* and X2 > A* are as in Theorem 2.1.1. Proposition 4.4.3. Suppose / is a non-negative continuous function on a bounded domain Q, and let u be a solution of (4.1.1) corresponding to a voltage A. Then, 1. For any A > 0, we have T A (Q, / ) > T. := aAsup^/(*) • 2. If infn / > 0, and if A > Ai := 2 7 i J ^ f ( x ) , then Tx(nj) < T M := £ i X [ ^ e _ n s y X ) ~ ̂ r l d s . (AAA) 3. If / > 0 on a set of positive measure, and if A > X2 := 3 y d x , then T A ( Q , / ) < T 2 , A : = - — log [ 1 - ^ S . ( f ffadx)-1. (4.4.5) Pn a* Jn Here fin and <j>n are the first eigenpair of —A on HQ(Q) with normalized J Q (f>ndx = 1. Proof: 1) Consider the initial value problem: dr)(t) _ A M dt ~ (1 - rj(t))2 ' (4.4.6) r ? ( 0 ) - 0 , where M — sup x 6 p . / (x ) . From (4.4.6) one has ̂ J0v^\l - s)2ds — t. If T» is the time where lim 4_,T. n(t) = 1, then we have T, = / ^ ( l - s)2ds = Obviously, n(t) is now a super-function of u(x, t) near touchdown, and thus we have T > T* — 1 - •-— 3 A M 3 A s u p I g n / ( a : ) ' which completes the proof of 1). 93 Chapter 4. Dynamic Deflection The following analytic upper bounds of finite touchdown time T were established in The- orem 3.1 and 3.2 of [32]. 2) Without loss of generality we assume that <f>n > 0 in Cl. Multiplying (4.1.1a) by (j>n, and integrating over the domain, we obtain | / 4>Budx= f <t>nAudx + [ XfJ{x)2dx. (4.4.7) "{ Jn Jn Jn U - u ) Using Green's theorem, together with the lower bound Co of / , we get f (j)nudx> -fin [ 4>nudx + XC0 [ ^" .9 dx. (4.4.8) d t Jn Jn Jn (1 - u ) 2 Next, we define an energy-like variable E(t) by E(t) = Jn(j)nudx so that E(t) = / 4>nudx < supu / <pndx = supu . (4.4.9) Jn n Jn n Moreover, E(0) = 0 since u = 0 at t = 0. Then, using Jensen's inequality on the second term on the right-hand side of (4.4.8), we obtain ^ + ^ E - ( T ^ ' E ( ° ) = ° - ( 4 A 1 ° ) We then compare E(t) with the solution F(t) of f + m = ° - <" • "> Standard comparison principles yield that E(t) > F(t) on their domains of existence. There- fore, supu > E(t) > F(t). (4.4.12) n Next, we separate variables in (4.4.11) to determine t in terms of F. The touchdown time T\ for F is obtained by setting F = 1 in the resulting formula. In this way, we get f i sjf [ ( i ^ - ^ r 1 * - (4-4-13) The touchdown time T\ is finite when the integral in (4.4.13) converges. A simple calculation shows that this occurs when A > Ai = 27c%- Hence if T\ is finite, then (4.4.12) implies that the touchdown time T of (4.1.1) must also be finite. Therefore, when A > Ai = we have that T satisfies T ^ = [ [(7̂ )2 - M _ 1 ds . (4.4.14) (3) Mult iply now (4.1.1a) by </>n(l — u ) 2 , and integrate the resulting equation over Cl to get d_ dt f % ( l - u ) 3 d x = - / fa{l-u)2Audx- [ Xffadx. (4.4.15) Jn 3 Jn Jn 94 Chapter 4. Dynamic Deflection We calculate the first term on the right-hand side of (4.4.15) to get V u - V -/ Jn Jn < A n ( i - u ) 2 dx + [ (1 - u)2<pn\7u -ndS- / A/</>n dx Jan Jn 1 - u)4>n\\7u\2dx • Jn dx < - \ f Vcj>n-udS-^ [ {\-uf<t>ndx- j \f<j>ndx, o Jan 6 Jn Jn (4.4.16a) (4.4.16b) (4.4.16c) (4.4.16d) where v is the unit outward normal to dQ. Since Jda M(j)n • vdS — —/z n, we further estimate from (4.4.16d) that d £ + HnE<R, R=!±-xJ f<l>ndx, where E(t) is defined by (4.4.17) E{t)=l-Jju{\-ufdx, E{ti) = \ . Next, we compare E(t) with the solution F(t) of F(0) Again, comparison principles and the definition of E yield ^ i n f ( l - w ) 3 <E(t)<F(t). (4.4.18) (4.4.19) (4.4.20) For A > A 2 we have that R < 0 in (4.4.17) and (4.4.19). For R < 0, we have that F = 0 at some finite time t = f2. From (4.4.20), this implies that E = 0 at finite time. Thus, u has touchdown at some finite-time T < %. B y calculating f 2 explicitly, and by using (4.4.20), the touchdown time T for (4.1.1) is found to satisfy r < f 2 S - - i o g [ i - § ( f f^dxy1}. Mn ^ A Jn (4.4.21) Remark 4.4.2. It follows from the above that if A > max { A j , A 2 } , then r < m i n { T o i A , T i , A , T 2 , A } . (4.4.22) where T0>\ is given by Theorem 4.2.3. We note that the three estimates on the touchdown times are not comparable. Indeed, it is clear that T0i\ is the better estimate when A* < A < min { A i , A 2 } since T 1 ) A and T2t\ are not finite. On the other hand, our numerical simulations show that T0tx can be much worse than the others, for A > max { A i , A 2 } . 95 Chapter 4. Dynamic Deflection Here are now some numerical estimates of touchdown times for several choices of the domain fi given by (4.3.2) and the exponential profile f(x) satisfying (slab): / ( x ) = e Q ( x 2 " 1 / 4 ) (exponential), (4.4.23a) (unit disk) : f{x) = ea{^2-l) (exponential), (4.4.23b) where a > 0. [htb Q a T* T T0,x Ti,\ slab 0 1/60 0.01668 0.2555 0.0175 0.01825 slab 1.0 1/60 0.02096 < 0.3383 0.0229 0.02275 slab 3.0 1/60 0.03239 < 0.6121 0.0395 0.03588 slab 6.0 1/60 0.06312 < 1.7033 0.0973 0.07544 unit disk 0 1/60 0.01667 0.2420 0.0172 0.01745 unit disk 0.5 1/60 0.02241 < 0.4103 0.0289 0.02507 unit disk 1.0 1/60 0.02927 < 0.7123 0.0492 0.03579 unit disk 3.0 1/60 0.09563 < 8.9847 1.1614 0.15544 Table 4.1: Computations for finite touchdown time T with the bounds T», To:\, T\iX and T 2 , A given in Proposition 4-4-3- Here the applied voltage A = 20 and the profile is chosen as (4-4-23). [htb] T{\ = 5) T(A = 10) T(A = 15) (A = 20) slab 0.07495 0.03403 0.02239 0.01668 unit disk 0.06699 0.03342 0.02235 0.01667 Table 4.2: Numerical values for finite touchdown time T at different applied voltages A = 5, 10, 15 and 20, respectively. Here the constant permittivity profile f(x) = 1 is chosen. In Table 2.1 of §2.2 we give numerical results for the saddle-node value A* with the bounds A, Ai and A 2 given in Theorem 2.1.1, for the exponential permittivity profile chosen as (4.4.23). Following the numerical results of Table 2.1 of §2.2, here we can compute in Table 4.1 the values of finite touchdown time T at A = 20, with the bounds T*, To^, T\t\ and T2>\ given in Theorem 4.2.3 and Proposition 4.4.3. Using the meshpoints N = 800 we compute finite touchdown time T with error less than 0.00001. The numerical results in Table 4.1 show that the bounds T\t\ and T 2 ] A for T are much better than Tot\. Further the bound T i ^ is better than T 2 ] A for smaller values of a, and however the bound T 2 ^ is better than Tit\ for larger values of a. In fact, for a ^> 1 and A large enough we can deduce from (2.3.23) that JI ,A ~ , i 2 , A ~ • Here d\ = 1/4, d2 = 1/37T 2 for the slab domain, and d\ = 1, d 2 = 4/3^Q for the unit disk, where ZQ is the first zero of JQ(Z) = 0. Therefore, for a ~S> 1 and fixed A large enough, the bound T 2 | A 96 Chapter 4. Dynamic Deflection is better than T\}\. Table 4.1 also shows that for fixed applied voltage A, the touchdown time is seen to increase once a is increased or equivalently the spatial extent where f(x) -C 1 is increased. However, Theorem 4.4.2 tells us that for fixed permittivity profile / , by increasing the applied voltage A within the available power supply, the touchdown time can be decreased and consequently the operating speed of M E M S devices can be improved. In Table 4.2 we give numerical values for finite touchdown time T with error less than 0.00001, at different applied voltages A = 5, 10, 15 and 20, respectively. Here the constant permittivity profile f(x) = 1 is chosen and the meshpoints N = 800 again. 4.5 Asymptotic analysis of touchdown profiles In this section, we discuss touchdown profiles by the method of asymptotic analysis, which provide some information on the refined touchdown rate studied in next Chapter. 4 . 5 . 1 T o u c h d o w n p r o f i l e : f{x) = 1 We first construct a local expansion of the solution near the touchdown time and touchdown location by adapting the method of [45] used for blow-up behavior. In the analysis of this subsection we assume that f(x) = 1 and touchdown occurs at x = 0 and t = T. In the absence of diffusion, the time-dependent behavior of (4.1.1) is given by uj = A ( l — u)~2. Integrating this differential equation and setting u(T) = 1, we get (1 — u ) 3 = —3A(t — T). This solution motivates the introduction of a new variable v(x,t) defined in terms of u(x,t) by v = ± ( l - u ) 3 . (4.5.1) A simple calculation shows that (4.1.1) transforms exactly to the following problem for v. 2 vt = Av - — \\7v\2 - 1, x e Q , (4.5.2a) v = -^, xedn- v = ^ , t = 0. (4.5.2b) Notice that u = 1 maps to v = 0. We wil l find a formal power series solution to (4.5.2a) near v = 0. As in [45] we look for a locally radially symmetric solution to (4.5.2) in the form v{x,t) = v0(t) + 7yV2(t) + ^v4(t) + --- , (4.5.3) where r = \x\. We then substitute (4.5.3) into (4.5.2a) and collect coefficients in r. In this way, we obtain the following coupled ordinary differential equations for VQ and v2: u 0 = - l + iV7j2, v'2 = - 3 ^ 2 + ^ ^ V i . (4.5.4) We are interested in the solution to this system for which VQ(T) = 0, with v'0 < 0 and v2 > 0 for T — t > 0 with T — t <£L 1. The system (4.5.4) has a closure problem in that v2 depends 97 Chapter 4. Dynamic Deflection on V4. However, we wil l assume that V4 -C V^/VQ near the singularity. W i t h this assumption, (4.5.4) reduces to -1 + Nv2, (4.5.5) We now solve the system (4.5.5) asymptotically as t —> T~ in a similar manner as was done in [45]. We first assume that Nv2 < 1 near t = T. This leads to v0 ~ T -1, and the following differential equation for v2: v2 v2, as 3(T -1) B y integrating (4.5.6), we obtain that 3 B0 v2 ~ — + • 4 [ l o g ( T - t ) ] [ l o g ( T - i ) ] t-*T~. H , as t -> T , (4.5.6) (4.5.7) for some unknown constant B0. From (4.5.7), we observe that the consistency condition that Nv2 <C 1 as t —> T~ is indeed satisfied. Substituting (4.5.7) into the equation (4.5.5) for VQ, we obtain for t —> T~ that + Bo + (4.5.8) 4 [ l o g ( r - t ) ] [\og(T-t)f Using the method of dominant balance, we look for a solution to (4.5.8) as t —> T~ in the form Co , C\ vo~(T-t) + (T- t) . [ l o g ( T - t ) ] [ l o g ( T - i ) ] 2 for some Co and C\ to be found. A simple calculation yields that (r A , -WP-t) 1 -N(B0-3/4)(T-t) v0 ~ (T - t) + ——^—— H — 7 7 ^ — — h • + • J 4 | l o g ( T - i ) | \\og(T-t)\> ast-+T~ (4.5.9) (4.5.10) The local form for v near touchdown is v ~ v0 + r2v0/2. Using the leading term in v2 from (4.5.7) and the first two terms in VQ from (4.5.10), we obtain the local form v ~ - tj 1 - 3N + 3r 2 4 | l o g ( T - i ) | 8 ( r - t ) | l o g ( T - t ) | + (4.5.11) for r < 1 and t - T < 1. Finally, using the nonlinear mapping (4.5.1) relating u and v, we conclude that u ~ 1 3A(T -t) [\- 3N + 3rz 4 | l o g ( T - t ) | 8 ( T - i ) | l o g ( T - i ) | + 1/3 (4.5.12) We note, as in [45], that if we use the local behavior v~(T-t) + 3r2/[8\ log(T - t)\], we get that IV^I 2 \ 2 n _ f r r ^ , 1 6 ( T - i ) | l o g ( r - 0 | 2 i - i - | l o g ( T - * ) | + 9 r 2 (4.5.13) 98 Chapter 4. Dynamic Deflection Hence, the term \\7v\2/v in (4.5.2a) is bounded for any r, even as t —* T~. This allows us to use a simple finite-difference scheme to compute numerical solutions to (4.5.2). W i t h this observation, we now perform a few numerical experiments on the transformed problem (4.5.2). For the slab domain, we define v™ for j = 1, . . . , N + 2 to be the discrete approximation to v(mAt, —l/2 + (j —l)/i) , where h = 1/{N + 1) and At are the spatial and temporal mesh sizes, respectively. A second order accurate in space, and first order accurate in time, discretization of (4.5.2) is , r + A t ( ^ - ^ + ^ - l - ^ - ^ ) , ; = 2 , . . . , t f + l , (4.5,4) <+1 with = v^+2 = 1 for m > 0. The initial condition is = 3̂A) 1 for j = 1,. . . , N+2. The time-step A i is chosen to satisfy A i < h2/4 for the stability of the discrete scheme. Using this argument, one can compute numerical results of dynamic deflection u, see Figures 4.1-4.3 of this Chapter. 4.5.2 Touchdown profile: variable permittivity In this subsection we obtain some formal asymptotic results for touchdown behavior associated with a spatially variable permittivity profile in a slab domain. Suppose u is a touchdown solution of (4.1.1) at finite time T, and let x = XQ be a touchdown point of u. W i t h the transformation v = ± ( l - u ) \ (4.5.15) the problem (4.1.1) for u in the slab domain transforms exactly to vt = vxx - ^-v\ - / ( x ) , - 1 / 2 < X < 1 / 2 , (4.5.16a) v = j ^ , a: = ± 1 / 2 ; v = ^ t = 0> (4.5.16b) where / (x ) is the permittivity profile. In order to discuss the touchdown profile of u near (xo,T), we use the formal power series method of §4.5.1 to locally construct a power series solution to (4.5.16) near touchdown point xo and touchdown time T. For this purpose, we look for a touchdown profile for (4.5.16), near x = xo, in the form , ^ (x — Xn)2 , , (x — Xo) 3 , , (x — Xo) 4 , . „ „„. v(x,t) = vo(t) + V 2 , °' v2(t) + K 3 , 0 1 v3(t) + K 4 | 0 J v4(t) + •••. (4.5.17) In order for v to be a touchdown profile, it is clear that we must require that l im v0 = 0, v0 > 0, for i < T ; v2 > 0, for i - T < 1. (4.5.18) t-*T~ We first discuss the case where / (x ) is analytic at x = xo with /(xo) > 0. Therefore, for x — XQ -C 1, / (x ) has the convergent power series expansion / (x ) = /o + f0{x - x 0 ) + / o ( * - * o ) 2 + . . . f (4.5.19) 99 Chapter 4. Dynamic Deflection where / 0 = f{x0), f'0 = f'{x0), and f'0' = f"{x0). Substituting (4.5.17) and (4.5.19) into (4.5.16), we equate powers of x — XQ to obtain V'Q = -fo + v2 , (4.5.20a) (4.5.20b) «s = fo • (4.5.20c) We now assume that v2 < 1 and v4 < 1 as t —> T~. This yields that vo ~ fo{T - t), and 4TJ| „ V2 = - - 5 — + U 4 - Jo , 3v0 w2 4t,2 2 - f o 3 / 0 ( T - t ) • ' 0 ' For i —> T - , we obtain from a simple dominant balance argument that 3/o v2 + • as t-*T~ 4 [ l o g ( T - t ) ] Substituting (4.5.22) into (4.5.20a), and integrating, we obtain that f (rp .\ 1 - 3 / o ( r - 1 ) « o ~ M r - * ) + 4 | i o g ( r _ t ) | + " as * - > r (4.5.21) (4.5.22) (4.5.23) Next, we substitute (4.5.22), (4.5.23) and (4.5.20c) into (4.5.17), to obtain the local touchdown behavior w ~ / 0 ( T - t ) 1 - _ , f'o(x - xo)3 4 | l o g ( T - t ) | ' S(T-t)\\og(T-t)\+ 6f0(T-t) + 3{x - xo)2 + (4.5.24) for (a; - x0) < 1 and t - T < 1. Finally, using the nonlinear mapping (4.5.15) relating u and v, we conclude that u ~ 1 — r 1 1 / 3 / 3 / 0 A ( r - t)\ (1 - + 3 ( i - x0)2 1/3 4 | i o g ( r - t ) | 1 8 ( r - t ) | i o g ( r - t ) | ' 6 / 0 ( r - t ) (4.5.25) Here / 0 = / ( z 0 ) and /Q = f'{x0). In the following, we exclude the possibility of f(xo) = 0 by using a formal power series analysis. We discuss the case where f(x) is analytic at x — XQ, with f(xo) = 0 and / (xo) — 0, so that f(x) = fo{x — XQ)2 + 0((x — xo) 3) as x —> Xo with fo > 0. We then look for a power series solution to (4.5.16) as in (4.5.17). In place of (4.5.20) for va, we get V3 = 0, and v2 = - ^ + ^ 4 - 2 / 0 . v0 = v2, V2 —^+v4-zjo. (4.5.26) Assuming that v4 < 1 as before, we can combine the equations in (4.5.26) to get M 3uo • 2 / 0 . (4.5.27) 100 Chapter 4. Dynamic Deflection By solving (4.5.27) with Vo(T) = 0, we obtain the exact solution U o = - ^ ( T - t ) 2 < 0 , V2=*h(T-t). (4.5.28) Since the criteria (4.5.18) are not satisfied, the form (4.5.28) does not represent a touchdown profile centered at x = XQ. Therefore, the above asymptotical analysis also shows that the point x = XQ satisfying f(xn) = 0 is not a touchdown point of u. 4.6 Pull-in distance One of the primary goals in the design of M E M S devices is to maximize the pull-in distance over a certain allowable voltage range that is set by the power supply. Here pull-in distance refers to as the maximum stable deflection of the elastic membrane before touchdown occurs. In this section, we provide numerical results of pull-in distance with some explicit examples, from which one can observe that both larger pull-in distance and pull-in voltage can be achieved by properly tailoring the permittivity profile. Following from [32], we focus on the dynamic solution u satisfying ^ - A u = - 1 ^ - for xeQ, (4.6.1a) at (i + uy (x,t) = 0 for xedfl; u(x,Q) = 0 for (4.6.1b) u One can apply Theorem 4.1.1 that for A < A*, the dynamic solution u(x,t) of (4.6.1) globally converges to its unique maximal negative steady-state u\{x). On the other hand, Theorem 2.1.2 implies that the unique maximal negative steady-state u\(x) is strictly increasing in A. Therefore, we can deduce that pull-in distance of (4.6.1) is achieved exactly at A = A*. Since the space dimension N of M E M S devices is 1 or 2, Theorems 2.1.2 & 4.1.1 give that the pull-in distance V of M E M S devices exactly satisfies D : = l i m || u*(x,t) | | L =c ( n ) HI u*(x) \\Loo{n)< C(N) < 1, AT = 1,2, (4.6.2) t—>oo where u*(x,i) is the unique global solution of (4.6.1) at A = A*, and while u*(x) is the unique extremal steady-state of (4.6.1). In order to understand the relationship between pull-in distance V and permittivity profile f(x), we first consider the steady-state of (4.6.1) satisfying - 1 < u < 0 in Q, ( 4 - 6 - 3 ) u = 0 on dQ, where the domain is considered to be a slab or an unit disk defined by (4.3.2). Here we still choose the following permittivity profile f(x) as before: slab : f(x) = \2x\a (power-law); f(x) = e a ( x 2 " 1 / 4 ) (exponential), (4.6.4a) unit disk : f(x) = \x\a (power-law); f(x) = ea^2~^ (exponential), (4.6.4b) 101 Chapter 4. Dynamic Deflection (a). Exponential Profiles: ft a A* slab 0 1.401 slab 3 2.637 slab 6 4.848 slab 10 10.40 unit disk 0 0.789 unit disk 3 6.096 unit disk 4.8 15.114 unit disk 5.6 20.942 (b). Power-Law Profiles: ft a A* slab 0 1.401 slab 1 4.388 slab 3 15.189 slab 6 43.087 unit disk 0 0.789 unit disk 1 1.775 unit disk 5 9.676 unit disk 20 95.66 Table 4.3: Numerical values for pull-in voltage A*; Table (a) corresponds to exponential profiles, while Table (b) corresponds to power-law profiles. | « (0) | K 0 ) | 0.0 2.0 4.0 6.0 8.0 10.0 12.0 14.0 16.0 10.0 12.0 14.0 16.0 Figure 4.4: Plots of the pull-in distance |u(0)| = |u*(0)| versus a for the power-law profile (heavy solid curve) and the exponential profile (solid curve). Left figure: the slab domain. Right figure: the unit disk. with a > 0. For above choices of domain ft and profile f(x), since the extremal solution u*(x) of (4.6.3) is unique, Lemma 2.6.1 shows that u*(x) must be radially symmetric. Therefore, the pull-in distance V of (4.6.3) satisfies V = |u*(0)|. As in §2.2, using Newton's method and C O L S Y S [2] to solve the boundary value problem (4.6.3), we first numerically calculate A* of (4.6.3) as the saddle-node point. We give numerical values of A* in Table 4.3(a) for exponential profiles and in Table 4.3(b) for power-law profiles, respectively. For the slab domain, in Figure 4.4(a) we plot V = \u(0)\ = \u*(0)\ versus a for both the power-law and the exponential conductivity profile f(x) in the slab domain, which show that the pull-in distance V can be increased by increasing the value of a (and hence by increasing the range of f(x) <C 1). A similar plot of V = \u(0)\ = |u*(0)| versus a is shown in Figure 4.4(b) for the unit disk. For the power-law profile in the unit disk we observe that \u(0)\ w 0.444 for any a > 0. Therefore, rather curiously, the power-law profile does not increase the pull-in distance for the unit disk. For the exponential profile we observe from Figure 4.4(b) that the pull-in distance is not a monotonic function of a. The maximum value occurs at a « 4.8 where A* w 15.11 (see Figure 2.1(b)) and V = |u(0)| = 0.485. For a = 0, 102 Chapter 4. Dynamic Deflection we have A* « 0.789 and |u(0)| = 0.444. Therefore, since A* is proportional to V2 (cf. §1.1.2) we conclude that the exponential permittivity profile for the unit disk can increase the pull-in distance by roughly 9% if the voltage is increased by roughly a factor of four. O.o ^ ^ ^ ^ ^ - 0 . 5 I 1 1 ' 1 n.O 0.2 0.4 0.0 0.8 1 |x| Figure 4.5: Left figure: plots ofu versus \x\ at A = A* for a = 0, a = 1, a = 3, and a = 10, in the unit disk for the power-law profile. Right figure: plots ofu versus \x\ at A = A* for a = 0, a = 2, a = 4, and a = 10, in the unit disk for the exponential profile. In both figures the solution develops a boundary-layer structure near \x\ = 1 as a is increased. For the unit disk, in Figure 4.5(a) we plot u versus \x\ at A = A* with four values of a for the power-law profile. Notice that u(0) is the same for each of these values of a. A similar plot is shown in Figure 4.5(b) for the exponential permittivity profile. From these figures, we observe that u has a boundary-layer structure when a » l . In this limit, f(x) -C 1 except in a narrow zone near the boundary of the domain. For a > l the pull-in distance T> = |u(0)| also reaches some limiting value (see Figure 4.4 & 4.5). For the slab domain with an exponential permittivity profile, we remark that the limiting asymptotic behavior of |u(0)| for a ^> 1 is beyond the range shown in Figure 4.4(a). 0.4 0.3 7 0.2 0.1 0.0 0.00 0.05 0.10 0.15 0.20 0.25 Ao Figure 4.6: Bifurcation diagram ofw'(0) = —7 versus Xo from the numerical solution of (4-6.6). For a > 1, we now use a boundary-layer analysis to determine a scaling law of A* for both types of permittivity profiles and for either a slab domain or the unit disk. We illustrate the 103 Chapter 4. Dynamic Deflection analysis for a power-law permittivity profile in the unit disk. For a ~S> 1, there is an outer region defined by 0 < r <^ 1 — 0(a~l), and an inner region where r — 1 = 0(\/a). In the outer region, where \ra <€: 1, (4.6.3) reduces asymptotically to Au = 0. Therefore, the leading-order outer solution is a constant u = A. In the inner region, we introduce new variables w and p by w(p) = u (1 — p/a) , p = a(l — r). (4.6.5) Substituting (4.6.5) into (4.6.3) with f(r) = ra, using the limiting behavior (1 — p/a)a —> e~p as a —> oo, and defining A = a 2 Ao, we obtain the leading-order boundary-layer problem w" = X°£ * , 0 < p < c o ; «;(0) = 0, u / ( o o ) = 0 , A = a 2 A 0 . (4.6.6) (l + wy In terms of the solution to (4.6.6), the leading-order outer solution is u — A = w(oo). Figure 4.7: Comparison of numerically computed A* (heavy solid curve) with the asymptotic result (dotted curve) from (4-6.7) for the unit disk. Left figure: the exponential profile. Right figure: the power-law profile. We define 7 by w (0) = —7 for 7 > 0, and we solve (4.6.6) numerically using C O L S Y S [2] to determine Ao = Ao(7). In Figure 4.6 we plot Ao(7) and show that this curve has a saddle-node point at Ao = Ag = 0.1973. A t this value, we compute w(00) « 0.445, which sets the limiting membrane deflection for a » 1. Therefore, (4.6.6) shows that for a 1, the saddle-node value has the scaling law behavior A* ~ 0.1973a 2 for a power-law profile in the unit disk. A similar boundary-layer analysis can be done to determine the scaling law of A* when a ^> 1 for other cases. In each case we can relate A* to the saddle-node value of the boundary-layer problem (4.6.6). In this way, for a ^> 1, we obtain 4 a 2 A* ~ 4(0.1973)a , A 2 ~ —— , (power-law, slab), (exponential, unit disk), (4.6.7a) o a 2 A* ~ (0.1973)a2 , A 2 ~ — , (power-law, unit disk), (exponential, slab), (4.6.7b) Notice that A 2 = 0(a2), with a factor that is about 5/3 times as large as the multiplier of a2 in the asymptotic formula for A*. In Figure 4.7, we compare the computed A* as a saddle-node point with the asymptotic result of A* from (4.6.7). 104 Chapter 4. Dynamic Deflection Next we present a few of numerical results for pull-in distance of dynamic problem (4.3.1) by applying the implicit Crank-Nicholson scheme again. Here we always consider the domain and the profile defined by (4.3.2) and (4.6.4), respectively. We choose the meshpoints JV = 4000 and the applied voltage A = A* given in Table 4.3: Figure 4.8: Case of exponential profiles We consider pull-in distance of (4.3.1) for exponential profiles in the slab or unit disk domain. In Figure 4.8(a) we plot u versus x at the time t = 80 in the slab domain, with a = 0 (solid line), a = 3 (dashed line), a = 6 (dotted line) and a = 10 (dash-dot line), respectively. This figure and Figure 4.4(a) show that pull-in distance is increasing in a. In Figure 4.8(b) we plot u versus |a;| at the time t = 80 in the unit disk domain, with a = 0 (dash-dot line), a = 3 (dashed line), a = 4.8 (dotted line) and a = 5.6 (solid line), respectively. In this figure we observe that the solution develops a boundary-layer structure near the boundary of the domain as a is increased, and pull-in distance is not a monotonic function of a. Actually from Figure 4.4(b) we know that pull-in distance is first increasing and then decreasing in a. The maximum value of pull-in distance occurs at a pa 4.8 and A* s=s 15.114. Figure 4.8: Left figure: plots ofu versus x at A = A* in the slab domain. Right figure: plots ofu versus \x\ at A = A* in the unit disk domain. Figure 4.9: Case of power-law profiles We consider pull-in distance of the membrane for power-law profiles in the slab or unit disk domain. In Figure 4.9(a) we plot u versus x at the time t = 80 in the slab domain, with a = 0 (solid line), a = 1 (dashed line), a = 3 (dash-dot line) and a — 6 (dotted line), respectively. This figure and Figure 4.4(a) show that pull-in distance is increasing in a. In Figure 4.9(b) we plot u versus \x\ at the time t = 80 in the unit disk domain, with a = 0 (dotted line), a = 1 (dash-dot line), a = 5 (dashed line) and a = 20 (solid line), respectively. For the power-law profiles in the unit disk domain, we observe that pull-in distance is a constant for any a > 0. Therefore, with Figure 4.4(b), it is rather curious that power-law profile does not change pull- in distance in the unit disk domain. In both figures, the solution develops a boundary-layer structure near the boundary of the domain as a in increased. Since one of the primary goals of M E M S design is to maximize the pull-in distance over a certain allowable voltage range that is set by the power supply, it would be interesting to 105 Chapter 4. Dynamic Deflection formulate an optimization problem that computes a dielectric permittivity f(x) that maximizes the pull-in distance for a prescribed range of the saddle-node threshold A*. 106 Chapter 5 Refined Touchdown Behavior 5.1 Introduction In this Chapter, we continue the study of dynamic solutions of (1.2.30) in the form ut — A u u(x, t) u(x,0) A/(z ) for (5.1.1a) (5.1.1b) (5.1.1c) 1 1 for for x G dSl where the permittivity profile f(x) is allowed to vanish somewhere, and wil l be assumed to We focus on the case where a unique solution u of (5.1.1) must touchdown at finite time T = T(A, ft, / ) in the sense D e f i n i t i o n 5.1.1. A solution u(x,t) of (5.1.1) is said to touchdown at finite time T = T(X,Cl, /) if the minimum value ofu reaches 0 at the time T < oo. We shall give a refined description of finite-time touchdown behavior for u satisfying (5.1.1), including some touchdown estimates, touchdown rates, as well as some information on the properties of touchdown set -such as compactness, location and shape. This Chapter is organized as follows. The purpose of §5.2 is mainly to derive some a priori estimates of touchdown profiles under the assumption that touchdown set of it is a compact subset of Q. In §5.2.1, we establish the following lower bound estimate of touchdown profiles. T h e o r e m 5.1.1. Assume f satisfies (5.1.2) on a bounded domain Cl, and suppose u is a touchdown solution of (5.1.1) at finite time T. If touchdown set ofu is a compact subset of SI, then 1. any point a G Cl satisfying f(a) = 0 is not a touchdown point for u(x,t); 2. there exists a bounded positive constant M such that Note that whether the compactness of touchdown set holds for any f(x) satisfying (5.1.2) is a quite challenging problem. We shall prove in Proposition 5.2.1 of §5.2 that the compactness of satisfy / G Ca(Sl) for some a G (0,1], 0 < / < 1 and / > 0 on a subset of SI of positive measure. (5.1.2) M(T-t)3 <u{x,t) in flx(Q,T). (5.1.3) 107 Chapter 5. Refined Touchdown Behavior touchdown set holds for the case where the domain ft is convex and f(x) satisfies the additional condition | £ < 0 on f !§ := dist{x, dQ) < 6} for some 5 > 0. (5.1.4) Here v is the outward unit norm vector to dQ. On the other hand, when f(x) does not satisfy (5.1.4), the compactness of touchdown set is numerically observed, see Chapter 4 or §5.4. Therefore, it is our conjecture that under the convexity of ft, the compactness of touchdown set may hold for any f(x) satisfying (5.1.2). In §5.2.2 we estimate the derivatives of touchdown solution u, see Lemma 5.2.4; and as a byproduct, an integral estimate is also given in §5.2.2, see Theorem 5.2.5. Motivated by Theorem 5.1.1, the key point of studying touchdown profiles is a similarity variable transformation of (5.1.1). For the touchdown solution u = u(x,t) of (5.1.1) at finite time T, we use the associated similarity variables y = -^Z=, s = -log(T-t), u(x, t) = (T — t)^wa(y, s), (5.1.5) where o is any interior point of ft. Then wa(y,s) is defined in Wa := {(y, s) : a + ye~sl2 £ ft, s > s' — —logT}, and it solves P{Wa)s - V • {pVwa) - -pwa H 2 = 0 ' <5 where p(y) = e - ' 2 ' ' 2 / 4 . Here wa(y,s) is always strictly positive in Wa. The slice of Wa at a given time s 1 is denoted by fta(sX) := Wa f~l {s = s 1} = es / 2(ft — a). Then for any interior point a of ft, there exists So = So(a) > 0 such that Bs := {y : \y\ < s} C ftQ(s) for s > SQ. We now introduce the frozen energy functional Es[wa}(s)=1- f p\VWa\2dy-\f pw2ady- f ^Mdy. (5.1.6) 1 JBS D JBS JBs wa By estimating the energy Es\wa]{s) in Bs, one can establish the following upper bound estimate. T h e o r e m 5.1.2. Assume f satisfies (5.1.2) on a bounded domain ft in RN, suppose u is a touchdown solution of (5.1.1) at finite time T and wa(y,s) is defined by (5.1.5). Assume touchdown set of u is a compact subset of ft. If wa(y,s) —> oo as s —> oo uniformly for \y\ < C, where C is any positive constant, then a is not a touchdown point for u. Based on a prior estimates of §5.2, we shall establish refined touchdown profiles in §5.3, where self-similar method and center manifold analysis wi l l be applied. Here is the statement of refined touchdown profiles: T h e o r e m 5.1.3. Assume f satisfies (5.1.2) on a bounded domain ft in RN, and suppose u is a touchdown solution of (5.1.1) at finite time T. Assume touchdown set of u is a compact subset o/ft, then, 1. If N = 1 and x = a is a touchdown point ofu, then we have lim_u(x,t){T -t)~^ = ( 3 A / ( a ) )3 (5.1.7) 108 Chapter 5. Refined Touchdown Behavior uniformly on \x — a\ < Cy/T — t for any bounded constant C. Moveover, when t —» T , (5.1.8) 2. Ifd = Bft(0) C RN is a bounded ball with N > 2, and f(r) = f(\x\) is radially symmetric. Suppose r = 0 is a touchdown point of u, then we have l i m « ( r , t ) ( T - t ) - i = (3A/(0))5 (5.1.9) uniformly on r < C\/T — t for any bounded constant C. Moveover, when t - . ~ |3A/(0)(r - t)f» ( i - m ^ 1 T ] + 4 ( r _ « ) £ . ( , • • t ) | + - ) • Note that the uniqueness of solutions for (5.1.1) gives the radial symmetry of u in Theorem 5.1.3(2). When dimension N > 2, it should remark from Theorem 5.1.3(2) that we are only able to discuss the refined touchdown profiles for special touchdown point x = 0 in the radial situation, and it seems unknown for the general case. Adapting various analytical and numerical techniques, §5.4 will be focused on the set of touchdown points. This may provide useful information on the design of M E M S devices. In §5.4.1 we discuss the radially symmetric case of (5.1.1) as follows: T h e o r e m 5.1.4. Assume f(r) = f(\x\) satisfies (5.1.2) and f'{r) < 0 in a bounded ball BR(0) C Rn with N > 1, and suppose u is a touchdown solution of (5.1.1) at finite time T. Then, r = 0 is the unique touchdown point of u. Remark 5.1.1. Assume f(r) = f(\x\) satisfies (5.1.2) and f'(r) < 0 in a bounded ball BR(0) C RN with N > 1. Together with Proposition 5.2.1 below, Theorems 5.1.1 and 5.1.4 show an interesting phenomenon: finite-time touchdown point is not the zero point of f(x), but the maximum value point of f(x). Remark 5.1.2. Numerical simulations in §5.4.1 show that the assumption f'(r) < 0 in Theorem 5.1.4 is sufficient, but not necessary. This gives that Theorem 5.1.3(2) does hold for a larger class of profiles f(r) = f(\x\). For one dimensional case, Theorem 5.1.4 already implies that touchdown points must be unique when permittivity profile f(x) is uniform. In §5.4.2 we further discuss one dimensional case of (5.1.1) for varying profile f{x), where numerical simulations show that touchdown points may be composed of finite points or finite compact subsets of the domain. 5.2 A priori estimates of touchdown behavior Under the assumption that touchdown set of u is a compact subset of Q, in this section we study some a priori estimates of touchdown behavior, and establish the claims in Theorems 5.1.1 and 5.1.2. In §5.2.1 we establish a lower bound estimate, from which we complete the proof of N = 2. (5.1.10) 109 Chapter 5. Refined Touchdown Behavior Theorem 5.1.1. Using the lower bound estimate, in §5.2.2 we shall prove some estimates for the derivatives of touchdown solution u, and an integration estimate wi l l be also obtained as a byproduct. In §5.2.3 we shall study the upper bound estimate by energy methods, which gives Theorem 5.1.2. We first prove the following compactness result for a large class of profiles f(x) satisfying (5.1.2) and §£ < 0 on Clcs := {x G Cl : dist{x, dCl) < 5} for some 5 > 0. (5.2.1) P r o p o s i t i o n 5.2.1. Assume f satisfies (5.1.2) and (5.2.1) on a bounded convex domain Cl, and suppose u is a touchdown solution of (5.1.1) at finite time T. Then, the set of touchdown points for u is a compact subset ofCl. P r o o f : We prove Proposition 5.2.1 by adapting moving plane method from Theorem 3.3 in [27], where it is used to deal with blow-up problems. Take any point yo G dCl, and assume for simplicity that yo = 0 and that the half space {xi > 0} (x = (x i ,x ' ) ) is tangent to Cl at yn. Let ftj = fin{xi > a} where a < 0 and |a | is small, and also define Cl~ = {(xj ,x ' ) : (2a —xi ,x ' ) G QJ} , the reflection of ftj with respect to the plane {xi = a}, where x ' = (x 2 , • • • , X J V ) . Consider the function w(x, t) = u(2a — x\,x',t) — u(x\,x',t) for x G Cl~, then w satisfies w - Aw — X(u(Xl'x''t) + M(2a ~ x^x'^))f(x)w W t W u2(x\,x',t)u2(2a — xi,x',t) It is clear that w = 0 on {x\ = a}. Since u(x, t) = 1 along dCl and since the maximum principle gives ut < 0 for 0 < t < T, we may choose a small to > 0 such that du{x,t0) > Q ^ S J 2 ) ( 5 2 2 ) where v is the outward unit norm vector to dCl. Then for sufficiently small |a | , (5.2.2) implies that w(x,tn) > 0 in Cl~ and also w — \-u{x\,x',t) > 0 on [dCX^rxfxx < a})x(to,T). Applying the maximal principle we now conclude that w > 0 in Cl~ x (to,T) and J-j^- = — 2 ^ - < 0 on {x i = a} . Since a is arbitrary, it follows by varying a that — > 0 , (x,t) x (t0,T) (5.2.3) provided |ao| = |ao(£o)| > 0 is sufficiently small. F ix 0 < |ao| < 5, where 5 is as in (5.2.1), we now consider the function J = u X l - £ i (x i - a0) in x (t0, T), where e\ = £ i (ao , io) > 0 is a constant to be determined later. The direct calculations show that ^ - W . ^ . - ^ . ^ , - * ^ ^ in n + * < t 0 , D (5.2.4) 110 Chapter 5. Refined Touchdown Behavior due to (5.2.1). Therefore, J can not attain negative minimum in fi+0 x (to,T). Next, J > 0 on {xi = a 0 } by (5.2.3). Since (5.2.2) gives > C > 0 along (9fi+ n dQ) for some C > 0, we have J > 0 on {t — to} provided £\ = £i(ao,£o) > 0 is sufficiently small. We now claim that for small E\ > 0, J > 0 on (0fi+ n dQ) x (t 0, T ) . (5.2.5) To prove (5.2.5), we compare the solution U := 1 — u satisfying Ut-AU = j ^ & p (x,t)eQx(t0,T), U{x, t0) = l- u{x, t0); U(x, t) = 0 x € dQ with the solution v of the heat equation vt = Av, (x,t) e Q x (t0,T), where 0 < v(x,t0) = U(x,t0) < 1 and u = 0 o n dQ. Then we have U > v in Q x (to.T1). Consequently, ^ < ^ < - C 0 < 0 on ( 0 f i + n 0 f i ) x ( i o , T ) , du u and hence ^ > Co > 0 on (<9ft+n<9fi) x ( i 0 , T ) . It then follows that J > C 0 ^ - e i ( n - a 0 ) > 0 provided £i = £ i ( a o ^ o ) is small enough, which gives (5.2.5). The maximum principle now yields that there exists e\ = £I(OJOI ^o) > 0 so small that J > 0 in Q+0 x (t0,T), i.e., u •Xx >ei{xx-ao), (5.2.6) if x' = 0 and ao < x\ < 0. Integrating (5.2.6) with respect to x\ on [ao,yi], where ao < y\ < 0, yields that u{yi,0,t) - u(a0,0,t) > y | y i - a 0 | 2 . It follows that l i m f _ T - M ( 0 , t ) — \imt_T- l im u(y\,0,t) > E\a\j2 > 0, yi-'O- which shows that yo = 0 can not be a touchdown point of u(x, t). The proof of (5.2.3) can be slightly modified to show that | ^ > 0 in Q+Q x (to,T) for any direction v close enough to the zi-direction. Together with (5.2.1), this enables us to deduce that any point in {x' = 0, ao < x\ < 0} can not be a touchdown point. Since above proof shows that ao can be chosen independently of initial point yo on dQ, by varying yo along dQ we deduce that there is an Q—Neighborhood Q' of dQ such that each point x € Q' can not be a touchdown point. This completes the proof of Proposition 5.2.1. • Remark 5.2.1. When f(x) does not satisfy (5.2.1), the compactness of touchdown set is nu- merically observed, see numerical simulations in Chapter 4 or in §5.4 of the present paper. Therefore, it is our conjecture that under the convexity of Q, the compactness of touchdown set may hold for any f(x) satisfying (5.1.2). I l l Chapter 5. Refined Touchdown Behavior 5.2.1 Lower bound estimate Define for 77 > 0, Clv := {x G Cl : dist{x, dCl) > 77} , fi£ : = {x G Cl : dist(x, dCl) < 77} . (5.2.7) Since touchdown set of u is assumed to be a compact subset of Cl, in the rest of this section we may choose a small 77 > 0 such that any touchdown point of u must lie in Cln. Our first aim of this subsection is to prove that any point xo G Cl^ satisfying /(xo) = 0 can not be a touchdown point of u at finite time T, which then leads to the following proposition. P r o p o s i t i o n 5.2.2. Assume f satisfies (5.1.2) on a bounded domain Cl, and suppose u(x,t) is a touchdown solution of (5.1.1) at finite time T. If touchdown set of u is a compact subset ofCl, then any point x o G Cl satisfying f(xn) = 0 cannot be a touchdown point ofu(x,t). Proo f : Since touchdown set of u is assumed to be a compact subset of fi, it now suffices to discuss the point xo lying in the interior domain Cl„ for some small 77 > 0, such that there is no touchdown point on Cl^. For any ti < T, we first recall that the maximum principle gives ut < 0 for all (x,t) G Cl x (0,ti). Further, the boundary point lemma shows that the outward normal derivative of v = Ut on dCl is positive for t > 0. This implies that for taking small 0 < to < T, there exists a positive constant C = C(to,n) such that ut(x,to) < —C < 0 for all x G Cl^. For any 0 < to < t\ < T, we next claim that there exists e = e(to, t\, 77) > 0 such that Jc(x, t) = ut + A; < 0 for all (x, t) £ fl„ x (t0, t{). (5.2.8) u Indeed, it is now clear that there exists C„ = C„(to,ti,ri) > 0 such that ut(x,t) < —C„ on the parabolic boundary of Cln x (*o,*i)• And further, we can choose e = e(to,ti,r]) > 0 so small that Jc < 0 on the parabolic boundary of fl^ x (io,^i), due to the local boundedness of 4? on dCln x (to,t\). Also, direct calculations imply that UA ti4 w5 Now (5.2.8) follows again from the maximum principle. Combining (5.2.8) and (5.1.1) we deduce that for a small neighborhood B of xo where A/ (x ) < e/2 is in B C Cln, we have for v := 1 — u, A ^ - | ( l - 7 j ) 2 ' in**) G B x (^h) • Now Proposition 5.2.2 is a direct result of Lemma 4.3.2, since t\ < T is arbitrary. • P r o o f of T h e o r e m 5.1.1: In view of Proposition 5.2.2, it now needs only to prove the lower bound estimate (5.1.3). Given any small 77 > 0, applying the same argument used for (5.2.8) yields that for any 0 < to < t\ < T, there exists e = £(to,ti,-n) > 0 such that ut < —% in £2„ x (to,ti). uz 112 Chapter 5. Refined Touchdown Behavior This inequality shows that ut —> —oo as u touchdown, and there exists M > 0 such that M i ( T - £ ) 5 < u{x,t) in fi, x (0,T) (5.2.9) due to the arbitrary of to and ti, where M i depends only on A, / and ry. Furthermore, one can obtain (5.1.3) because of the boundedness of u on Q^., and the theorem is proved. • 5.2.2 Gradient estimates As a preliminary of next section, it is now important to know a priori estimates for the derivatives of touchdown solution u, which are the contents of this subsection. Following the analysis in [27], our first lemma is about the derivatives of first order without the compactness assumption of touchdown set. L e m m a 5.2.3. Assume f satisfies (5.1.2) on a bounded convex domain Ci, and suppose u is a touchdown solution of (5.1.1) at finite time T. Then for any 0 < to < T, there exists a bounded constant C > 0 such that - | V u | 2 < - - - in Qx(Q,t0), (5.2.10) 2 u u where u = u(to) = m i n x e n u(x, to), and C depends only on A, / and Q. Proo f : F ix any 0 < to < T and treat u(to) as a fixed constant. Let w = u — u, then w satisfies A fix) wt-Aw = - , M ; 2 in fix(0,t0), (w + u)z w = l — u in dQ,x(0,to), w(x, 0) = 1 — u in fi. We introduce the function P 1 | V H 2 + - ^ - - - , (5.2.11) 2 w + u u where the bounded constant C > 2 A s u p x 6 n / will be determined later. Then we have P _ A P - C X f W _ AV/(s )V™ , 2(\f(x)-C)\Ww\2 _ ^ 2 n ^ - ( w + u)* (w + u)2 (w + u)* . 4 ^ i j 1,3—1 XCsupxeQf - 2 A l V w | 2 s u p x 6 n / + \\Vw\supx£„ \V/| _ y > ^ 2 2 1 2 ) - (w + u)4 (w + u)3 .4^, i j ' ' X(CsupxeQ f + Ci) _ ^ 2 (w + uf ^ i j ' v —' 1,3 = 1 where C i := ( T " t " | V / J ) 2 > 0 is bounded. Since (5.2.11) gives £ { P i + J^TuT2Wi)2 = ^ { W j W i i f - l V w } 2 £ ^ ' ( 5 ' 2 - 1 3 ) i=l ^ —' i,j=l »1.7=1 113 Chapter 5. Refined Touchdown Behavior we now take n / o \ * AsuP 3 ;6n / + A v / ( s u P x 6 f l / ) 2 + 4 C ' l l N O ^ „ . . „ f C := max < 2A sup / , 5 > > 2A sup / xen 2 J xen so that C 2 > A ( C s u p a . e n / 4- C i ) , where C clearly depends only on A, / and Cl. From the choice of C, a combination of (5.2.12) and (5.2.13) gives that Pt - AP < ~b • V P , where b = — | V w | ~ 2 ( V P + 2^+^i) is a locally bounded when V U J ^ 0. Therefore, P can only attain positive maximum either at the point where Vto = 0, or on the parabolic boundary of Q x (0,t0). But when V w = 0, we have P < 0. On the initial boundary, P — — £ < 0. Let (y,s) be any point on dCl x (0,to), if we can prove that dP -^<0 at (y,s), (5.2.14) it then follows from the maximum principle that P < 0 in Cl x (0,to). And therefore, the assertion (5.2.10) is reduced from (5.2.11) together with w = u — u. To prove (5.2.14), we recall the fact that since w = const, on dQ. (for t = s), we have A u ; = wvv + (N — 1)KU>V at (y, s), where K is the non-negative mean curvature of dCl at y. It then follows that A u ; - (N - \)KWV A / ( X ) dP _ Cwv ov (w + u)2 I (u; + u) 2 J = w„[wt - (N - 1)KW„] = -(N - 1)KWI < 0 at (y, s), and we are done. • The following lemma is dealt with the derivatives of higher order, and the idea of its proof is similar to Proposition 1 of [35]. Lemma 5.2.4. Assume f satisfies (5.1.2) on a bounded domain Cl, and suppose u is a touch- down solution o/(5.1.1) at finite time T. Assume touchdown set of u is a compact subset of Cl, and x = a is any point of Clv for some small n > 0. Then there exists a positive constant M' such that \Vmu(x,t)\(T- t)"3+T < M', m = l,2 (5.2.15) holds for |o; — a| < R. Proof: It suffices to consider the case o — 0 by translation, and we may focus on \R2 < r2 < R2 and denote Qr = BT x (T[l - (^ ) 2 ] ,T) . Our first task is to show that | V u | and | V 2 u | are uniformly bounded on compact subsets of Q R . Indeed, since f(x)/u2 is bounded on any compact subset D of Q R , standard LP estimates for heat equations (cf. [47]) gives I L ( | V 2 u | p + \ut\p)dxdt < C, K p < 0 0 . D 114 Chapter 5. Refined Touchdown Behavior Choosing p to be large enough, we then conclude from Sobolev's inequality that f(x)/u2 is Holder continuous on D. Therefore, Schauder's estimates for heat equations (cf. [47]) show that | V u | and | V 2 u | are uniformly bounded on compact subsets of D. In particular, there exists M i such that |Vw| 4- | V 2 u | < M i for (x,t) € Br x (T[ l - (^) 2 ] ,T[1 - 1(1 - ^ ) 2 ] ) , (5.2.16) where M i depends only on R, N and M given in (5.1.3). We next prove (5.2.15) for |z | < r and T[l - | (1 - £ ) 2 ] <t <T. F i x such a point (x,t), let fi= [y(T — £)]5 and consider V(Z,T) = n~iu{x + nz,T- n2{T - T)) . (5.2.17) For above given point (x,t), we now define O := {z : (x + fiz) € £1} and g(z) := f(x + fiz) > 0 on O. One can verify that V(Z,T) is a solution of A Ao(z) _ ^ - A ^ = ~ — z ^ 0 ' (5.2.18) v(z,0) = vo(z) > 0; V(Z,T) = n 3 z e 80 , 2 where A z denotes the Laplacian operator with respect to z, and Vo(z) = n~3u(x + u.z,T — u.2T) > 0 satisfies Azv0 - < 0 on O. The formula (5.2.17) implies that T is also the finite touchdown time of v, and the domain of v includes QTQ for some rn = ro(R) > 0. Since touchdown set of u is assumed to be a compact subset of Q, one can observe that touchdown set of v is also a compact subset of O. Therefore, the argument of Theorem 5.1.1(2) can be applied to (5.2.18), yielding that there exists a constant M 2 > 0 such that V{Z,T) > M2(T-T)13 where M2 depends only on R, A, / and CI again. The argument used for (5.2.16) then yields that there exists M[ > 0, depending on R, N and M 2 , such that | V ^ | + | V 2 t , | < M[ for (z,T)GBrx ( r [ l - ( ^ ) 2 ] ,T [1 - 1(1 - ^ ) 2 ] ) , (5.2.19) where we assume \TQ < r2 < r2,. Applying (5.2.17) and taking (Z,T) — (0, ^ ) , this estimate reduces to ^ - i + 1 | V u | + / j " t + 2 | V 2 u | < M { . Therefore, (5.2.15) follows since /x = [ f (T -t)]2. • Before concluding this subsection, we now apply gradient estimates to establishing integral estimates. Theorem 5.2.5. Assume f satisfies (5.1.2) on a bounded domain J7, and suppose u is a touchdown solution of (5.1.1) at finite time T. Assume touchdown set ofu is a compact subset ofQ, then for 7 > |AT we have l i m t ^ T - / f(x)u 7(x, t)dx = + 0 0 . Jn 115 Chapter 5. Refined Touchdown Behavior Proof: For any given to £ (0, T) close to T , Lemma 5.2.3 implies that l\Vu\2 < ̂ (u - u) in Clx(0,t0) (5.2.20) 2 uf1 for some bounded constant C > 0, where u = u(xo,to) = min ; r e p. 'u(x,£o)- Considering any t sufficiently close to to, we now introduce polar coordinates (r, 9) about the point XQ- Then in any direction 9, there is a smallest value of ro = ro{9,t) such that u(ro,t) = 2u, Note that ro is very small as t < to sufficiently approach to T. Furthermore, since xo approaches to one of touchdown points of u as t —» T~, Proposition 5.2.2 shows that as t < to sufficiently approach to T, we have f(x) > Co > 0 in {r < ro} for some Co > 0. Since (5.2.20) and the definition of u imply that < ^p-, which is 2y/u - u < ^pr, we attain yj~^u3/2 < r 0 by taking r = ro- Therefore, for 7 > | i V we have / u'^dx >C f f{x)vT*idx > CCo I u'^dx > C f dSe f u^^^dr Jn Jn J{r<r0} Je J{r<ro} >C [dSg [ (2u)-^rN-1dr J$ J{r<r0} >C f dSgu-trg >C f dSeur1+^N = + 0 0 Je Je as t —> T~, which completes the proof of Theorem 5.2.5. • 5.2.3 Upper bound estimate In this subsection, we discuss the upper bound estimate of touchdown solution u by applying energy methods. First, we note the following local upper bound estimate. Proposition 5.2.6. Suppose u is a touchdown solution of (5.1.1) at finite time T. Then, there exists a bounded constant C = C(X,f, Cl) > 0 such that minu(x, t) < C ( T - t ) 3 for 0<t<T. (5.2.21) x£f2 Proof: Set U(t) =minu{x,t), 0<t<T, xeo. and let U(U) = u{xi, U) (i = 1,2) with h = t2 - h > 0. Then, U(t2) - U{ti) < u(xx,t2) - u(xi,t{) = hut(xi,ti)+o{h), U(t2) - U(ti) > u(x2,t2) - u(x2,tx) = hut{x2,t2) + o(h). It follows that U(t) is lipschitz continuous. Hence, for t2 > t\ we have ——r—r^—- ^ Mx2, t2) + 0 ( 1 ) . t2 —1\ 116 Chapter 5. Refined Touchdown Behavior On the other hand, since Au(x2,t2) > 0 we obtain, I *\ ^ Xf(Xz) A / ( Z 2 ) C ut{x2,t2)>—2? 7 T = ~ 7 7 2 7 7 T - _ 7 T 2 7 7 T F O R 0 < * 2 < ^ - U1{X2,t2) UZ{t2) Uz{t2) Consequently, at any point of differentiability of U(t), it deduces from above inequalities that U2Ut > -C a.e. * e (0 ,T ) . (5.2.22) Integrating (5.2.22) from t to T we obtain (5.2.21). • For the touchdown solution u = u{x,t) of (5.1.1) at finite time T, we now introduce the associated similarity variables 3, = - ^ = , s = -log(T-t), u(x,t) = (T-t)-3Wa(y,s), (5.2.23) where a is any point of fi„ for some small 77 > 0. Then u) a(y, s) is defined in W a := {(y, s): a + ye'3'2 £Q,s>s' = -logT) , and it solves 3 % a - AWa + \y • VWa - \ W a + A / ( a T ' 5 ) = 0. (5.2.24) ds 2 3 wi "a Here wa(y,s) is always strictly positive in Wa. Note that the form of wa defined by (5.2.23) is motivated by Theorem 5.1.1 and Proposition 5.2.6. The slice of Wa at a given time s 1 wil l be denoted by fia(s1): fi^s1) := Wa n {s = s1} = e s l / 2 ( f i - a) . Then for any a £ fi,,, there exists so = SO(T], a) > 0 such that -Bs := {j/ : \y\ < s) C fia(s) for s > s 0 . (5.2.25) From now on, we often suppress the subscript a, writing w for wa, etc. In view of (5.2.23), one can combine Theorem 5.1.1 and Lemma 5.2.4 to reaching the following estimates on w = wa: C o r o l l a r y 5.2.7. Assume f satisfies (5.1.2) on a bounded domain fi, and suppose u is a touchdown solution of (5.1.1) at finite time T. Assume touchdown set ofu is a compact subset o / f i , then the rescaled solution w = wa satisfies M < w < ei ,. \\7w\ + \Aw\ < M' in W, where M is a constant as in Theorem 5.1.1 and while M' is a constant as in Lemma 5.2.4- Moreover, it satisfies M < w(y!,s) < w(y2,s)+M'\y2-yi\ for any (yi: s) £ W, i = 1, 2. 117 Chapter 5. Refined Touchdown Behavior We now rewrite (5.2.24) in divergence form: pws-V- (pVw) - \pw + + = q ^ ( 5 2 2 g ) where p(y) — e l ^ l 2 / 4 . We also introduce the frozen energy functional Es[w](s)=l-j p\Vw\2dy-\j pu?dy-\ ^ ^ - d y , (5.2.27) 1 JBs b JBa JBs w which is defined in the compact set Bs of Q,a(s) for s > SQ. L e m m a 5.2.8. Assume f satisfies (5.1.2) on a bounded domain fi, and suppose u is a touch- down solution of (5.1.1) at finite time T. Assume touchdown set of u is a compact subset of fi, then the rescaled solution w = wa satisfies 1 r A - p\ws\2dy<-—Es[w}(s)+9v(s) f°r s > s o , (5.2.28) 2 JBs a s where gv{s) is positive and satisfies gv(s)ds < oo. Proo f : Mult iply (5.2.26) by ws and use integration by parts to get / p\ws\2dy= f ws\7(pVw)dy+^ [ pwwsdy - f XpWs^ a ^ ye—Idy JBB JBS 6 JBs JBS W = - i f ±ww\2pdy+r * a w 2 + ± m ) p d y 2JBsds' JB3ds\6 w J dw f Xpws[f{a) - / ( o + ye _ t ) ] + / pws^-dS+ f JdBs du JE ~Es[w}(s) + [ pws^dS + i / p\Vw\2(y • u)dS as JsBs av Is JdBs Xf(a)\, , / XPws\f(a)-f(a + ye-^)} s JdB, V6 w J JE dy < ds )dB3 d Es[w}(s) + f pws^dS + ^ / p\Vw\2(y • v)dS JdBs ov 2s JdBs Xpws[f{a)- f{a + ye 2 ) ] JBS W2 := -^-E,[w](s) + h+h + h , S (5.2.29) where v is the exterior unit norm vector to dQ and dS is the surface area element. The following formula is applied in the third equality of (5.2.29): if g(y,s) : W >-> R is a smooth 118 Chapter 5. Refined Touchdown Behavior function, then d_ ds [ 9{y,s)dy=^L[ g(sz,s)sNdz JBS ds J B L = N g(sz,s)sN~1dz + / gs(sz,s)sNdz + / (\7yg • z)sNdz JBi JBI JBI = [ gs{y,s)dy + N [ g(y,s)^-+f {^g--)dy JBS JBS S JBS S' = 9s{y,s)dy + - I g(y,s){y • v)dS. J B A S JgBa For s > SQ, we next estimate integration terms I\, I2 and J3 as follows: Considering \y\ < S in Bs, Corollary 5.2.7 gives \wa\ = \&w --yVw + -w- 1 L\ < c ( i + IJ,)) + - u , < Cia + - e 5 , Zt o 11) o o which implies 7i < CaN-1e~^ (da + \e%) < C2sNe-^+i . (5.2.30) It is easy to observe that h < C3sN-1e-'r . (5.2.31) As for I3, since w has a lower bound and since f(x) € Ca(Q) for some a € (0,1], we apply Young's inequality to deduce I p\y\awsdy<Ce-is\e f pw2sdy + C(e) f p\y\2ady JBS 1 JBS JBS where the constant e > 0 is arbitrary. Because e 2 s < 00, one can take sufficiently small e such that h < \ pwldy + C 4 e - f s . (5.2.32) Z JBS Combining (5.2.29) - (5.2.32) then yields -J p\w.\dy< - J s s\2 < ~Et[w](s) + CisNe-^+i + C ^ ' :=-^-Es[w}(s) + gv{s), where gn{s) is positive and satisfies gn(s)ds < 00, and we are done. • Remark 5.2.2. Supposing the convexity of ft, one can establish an energy estimate in the whole domain Qa(s)- [ p\ws\2dy<-^Eaais)[w}{s) + Kn{s) for a > s0, (5.2.33) Jna(s) a s 119 Chapter 5. Refined Touchdown Behavior where K^s) is positive and satisfies K„(s)ds < oo, and EQa^\w](s) is defined by Enais)H(s) = \l P\Vw\2dy - \ f pw2dy - f . ^ ± d y . (5.2.34) However, by estimating the energy functional Es[w](s) in Bs, instead of Cla(s), it is sufficient to obtain the desirable upper bound estimate of w, see Theorem 5.2.10 below. The following lemma is also necessary for establishing the desirable upper bound estimate. L e m m a 5.2.9. Assume f satisfies (5.1.2) on a bounded domain Cl, and suppose u is a touch- down solution of (5.1.1) at finite time T. Assume touchdown set of u is a compact subset of Cl, and a is any point of Cl„ for some r\ > 0. Then there exists a constant e > 0, depending only on X, f and Cl, such that if u{x,t)(T - £ ) - 3 > £ (5.2.35) for all (x,t) € Qs '•= {(x,t) : \x — a\ < 5,T — 5 < t < T}, then a is not a touchdown point for u. Here 5 > 0 is an arbitrary constant. Proo f : Setting v(x,t) = vt — A u = where K := Asup x e f j f(x) > 0. We now apply Theorem 2.1 of [37] to (5.2.36), which gives that there exists a constant j > 0, depending only on A, / and Cl, such that if v{x,t) < ^ ( T - i ) - 5 in Q6, then a is not a blow-up point for v, and hence (5.2.35) follows. • then v(x,t) blows up at finite time T, and v satisfies - ^ ^ + Xf{x)v4 <K(l + v4) in Qs, (5.2.36) T h e o r e m 5.2.10. Assume f satisfies (5.1.2) on a bounded domain Cl, and suppose u is a touchdown solution of (5.1.1) at finite time T. Assume touchdown set ofu is a compact subset of Cl, and a is any point of Cl„ for some r) > 0. Ifwa(y,s) —-> oo as s —> oo uniformly for \y\ < C, where C is any positive constant, then a is not a touchdown point for u. Proo f : We first claim that if wa{y, s) —> oo as s —* oo uniformly for \y\ < C, then Bs\wa\{s) —> — oo as s—>oo. (5.2.37) Indeed, it is obvious from Corollary 5.2.7 that the first term and the third term in Es[wa](s) are uniformly bounded. As for the second term, we can write / pw2dy = / pw2dy + / pw2dy > / pw2dy. JBS JBc JB3\BC JBC Since wa —> oo as s —> oo uniformly on Be, we have JB pw2dy —> oo as s —> oo, which gives — | JB pw2dy —• —oo as s —> oo, and hence (5.2.37) follows. 120 Chapter 5. Refined Touchdown Behavior Let K be a large positive constant to be determined later. Then (5.2.37) implies that there exists an s such that Eg[wa}(s) < —AK. Using the same argument as in [36], it is easy to show that for any fixed s, Es[wa](s) varies smoothly with a G Q. Therefore, there exists an rn > 0 such that Es[wb](s) < -3K for |6 - a\ < r0 . Since touchdown set of u is assumed to be a compact subset of Q, we have dist(a, dQ) > T) for some 77 > 0. Therefore, it now follows from Lemma 5.2.8 that Es[u>b]{s) < -2K for \b - a\ < r 0 , s > s provided K > M\ := gn(s)ds, where gn(s) is as in Lemma 5.2.8. Since the first term and the third term in Es[wb](s) are uniformly bounded, we have JB pw2dy>6K for \b - a\ < r0 , s > s. (5.2.38) Recalling from Corollary 5.2.7, wl(y,s)<2(wl(0,s) + M'2\y\2), we obtain from (5.2.38) that 3K < w2(0, s) f pdy + M'2 f p\y\2dy < ClW2{0,s) + C2 . J BS J BA We now choose K > max{M\, ^C2} so large that / W b { 0 , s ) ~ \l2C~! ~ £ - ( 5 - 2 ' 3 9 ) Setting t:=T - e~s, it reduces from (5.2.39) that u(b,t)(T-t)~* > e for \b - a\ < r0 , t < t < T. Applying Lemma 5.2.9 with a small ro, we finally conclude that a is not a touchdown point for u, and the theorem is proved. • 5.3 Refined touchdown profiles In this section we first establish touchdown rates by applying self-similar method [35]. Then the refined touchdown profiles for N = 1 and N = 2 will be separately derived by using center manifold analysis of a P D E [25], which wil l be discussed for N = 1 in §5.3.1 and for N > 2 in §5.3.2, respectively. It should be pointed out that for N = 1 we may establish the refined touchdown profiles for any touchdown point, see Theorem 5.3.3; while for N > 2, we are only able to deal with the refined touchdown profiles in the radial situation for the special touchdown point r = 0, see Theorem 5.3.5. Throughout this section and unless mentioned otherwise, touchdown set for u is assumed to be a compact subset of Q, and a is always 121 Chapter 5. Refined Touchdown Behavior assumed to be any touchdown point of u. Therefore, all a priori estimates of last section can be adapted here. Our starting point of studying touchdown profiles is a similarity variable transformation of (5.1.1). For the touchdown solution u = u(x, t) of (5.1.1) at finite time T, as before we use the associated similarity variables y = -?LpJL, s = -log(T-t), u(x,t) = (T-t)13w(y,s), (5.3.1) where o is any touchdown point of u. Then w(y, s) is defined inW = {(y, s) : \y\ < Re3/2, s > s' = —logT}, where R = max{|a; — a\ : x £ fi}, and it solves ws - i v ( p V u , ) - \w + A / ( a + f f ) = 0 (5.3.2) p 3 wz with p(y) = e - ' 3 '! 2/ 4 , where /(a) > 0 since a is assumed to be a touchdown point. Therefore, studying touchdown behavior of u is equivalent to studying large time behavior of w. L e m m a 5.3.1. Suppose w is a solution of (5.3.2). Then, w(y, s) —> w^y) as s —> oo uniformly on \y\ < C, where C > 0 is any bounded constant, and u>oo(2/) * s a bounded positive solution of A w - - y W w + l w - ^ - = Q in RN, (5.3.3) 2 3 where f(a) > 0. P roo f : We adapt the arguments from the proofs of Propositions 6 and 7 in [35]: let {SJ} be a sequence such that Sj —> oo and Sj+\ — SJ —+ oo as j —* oo. We define u>j(y, s) = w(y, s + Sj). According to Theorem 5.1.1, Corollary 5.2.7 and Arzela-Ascoli theorem, there is a subsequence of {uij}, still denoted by Wj, such that Wj(y,s) -> Woo(y,s) uniformly on compact subsets of W, and Vwj(y,m) -> Vwoo(2/,ra) for almost all y and for each integer m. We obtain from Corollary 5.2.7 that either Woo = oo or Woo < oo in R w + 1 . Since a is a touchdown point for u, the case Woo = oo is ruled out by Theorem 5.2.10, and hence IUQO < oo in R N + 1 . Therefore, we conclude again from Corollary 5.2.7 that « ; < C i ( l + |y|) (5-3-4) for some constant C i > 0. Define the associated energy of w at time s, ER[w]{s) = l f p\Vw\2dy-\j pw2dy- f M ^ d y . (5.3.5) 2 J B R B JBR JBR W 122 Chapter 5. Refined Touchdown Behavior Taking R(s) = s, the same calculations as in (5.2.29) give -^Es[w}(s)= f p(y)\w3\2dy - K(s) (5.3.6) with K(s) = / Pws^dS + i - / p|\7w\\y • u)dS - i / p ( i ^ 2 + (y • ̂ JdS 7aB s o y 2s 7as s 5 J A B S \ 6 tu / JBS W2 V ' We note that the expression K(s) can be estimated a s s > 1. Essentially, since f(x) G Ca(Q) for some a 6 (0,1], using (5.3.4) and applying the same estimates as in Lemma 5.2.8 one can deduce that K(s) - \ j pw2dy < G(s) := CisNe~^ + C2e'2s for s » 1. (5.3.7) 2 JBS Together with (5.3.7), integrating (5.3.6) in time yields an energy inequality Iff p\w3\2dyds < Ea[w](a) - Eb[w](b) + f G(s)ds, (5.3.8) z Ja JBS Ja whenever a < b. We now use (5.3.8) to prove that u i ^ is independent of s. We set a = Sj+m and b = Sj+i+m in (5.3.8) to obtain I p\wjs\2dyds < ESj+rn[wj](m) - ESj+1+m[wj+i](m) + G(s)ds J B s i + s Jsj+m 2 j-m+Sj+i-Sj : _.. . . ; ; . . is 2 oo. (5.3.9) for any integer m, where we use Wj(y,s) = w(y,s + Sj). Since Vvjj(y,m) is bounded and independent of j, and since we have assumed that \7uij(y,m) —> Vwoo(j/>"i) o,.e. as j —> oo, the dominated convergence theorem shows that J p{y)\\7wj{y,m)\2dy -> J' p(y)\Vwoo(y,m)\2dy as j Arguing similarly for the other terms we can deduce that l im ESi+m[wj](m) = lim Es +m[wi+l}{m) := £[tUoo] • (5.3.10) j—>oo J j—»oo On the other hand, because m + Sj —> oo as j —> oo, (5.3.7) assures that the term involving G in (5.3.9) tends to zero as j —> oo. Therefore, the right side of (5.3.9) tends to zero as j —> oo. It now follows from Sj+i — Sj —> oo that l im / / p\wjs\2dyds = 0 (5.3.11) J^°°Jm JBSj+s 123 Chapter 5. Refined Touchdown Behavior for each pair of integers m < M. Further, since (5.3.4) implies \vjjs(y,s)\ < C ( l + \y\) with C independently of j, one can deduce that WjS converges weakly to W Q O S . Because p decreases exponentially as |y| —> oo, the integral of (5.3.11) is lower semi-continuous, and hence j / p\wooS\2dyds = 0, Jm JRN where m and M are arbitrary, which shows that WOQ is independent of the choice of s. We now notice from (5.3.5) that (5.3.10) defines i5[u>oo] by m = \l PWvv\2dy-\ I P\v\2dy-f ^ ^ d y . 2 JmN oJm N JRV V We claim that i^Woo] is independent of the choice of the sequence {SJ}. If this is not the case, then there is another {SJ} such that S[iOoo] ¥= •̂ ['̂ oo], where Woo = l imj_ O 0 vlj with Wj(y,s) = w(y,s + Sj). Relabeling and passing to a sequence if necessary, we may suppose that -E[t«oo] < E[woo] with Sj < Sj. Now the energy inequality (5.3.8), with a = Sj and 6 = Sj, gives that \ f3 f p\ws\2dyds < ESj [Wj](0) - E-Sj [Wj}(0) + f' G(s)ds. (5.3.12) 2 J SJ JBs J Sj Since ESj[wj}(0) - ESJ[WJ}(0) —» Elw^] - ^^[w^oo] < 0 and G(s)ds -> 0 as j -> oo, the right side of (5.3.12) is negative for sufficiently large j. This leads to a contradiction, because the left side of (5.3.12) is non-negative. Hence ^ [ W Q O ] = ^[fDoo], which implies that ^ [ W Q O ] is independent of the choice of the sequence {SJ}. Therefore, we conclude that w(y, s) —> w00(y) as s —» oo uniformly on \y\ < C, where C is any bounded constant, and w^y) is a bounded positive solution of (5.3.3). • 5.3.1 Refined touchdown profiles for N = 1 In this subsection, we establish refined touchdown profiles for the deflection u = u(x,t) in one dimensional case. We begin with the discussions on the solution w^y) of (5.3.3). For one dimensional case, F i l a and Hulshof proved in Theorem 2.1 of [23] that every non-constant solution w(y) of 1 1 1 n • wyy - T.Vwv + -zw 2 = 0 m ( ~ ° ° ' 0 0 ) & o IV must be strictly increasing for all \y\ sufficiently large, and w(y) tends to oo as |y| —+ oo. So it reduces from Lemma 5.3.1 that it must have Woo(y) = const.. Therefore, by scaling we conclude that lim w(y,s) == (3A/(a ) ) 3 uniformly on \y\ < C for any bounded constant C. This gives the following touchdown rate. L e m m a 5.3.2. Assume f satisfies (5.1.2) on a bounded domain Q C R 1 , and suppose u is a unique touchdown solution of (5.1.1) at finite time T. Assume touchdown set for u is a compact subset ofQ. If x — a is a touchdown point ofu, then we have \im_u(x,t){T -t)~* = (3A/(a))5 124 Chapter 5. Refined Touchdown Behavior uniformly on \x — a\ < Cy/T'— t for any bounded constant C. We next determine the refined touchdown profiles for one dimensional case. Our method is based on the center manifold analysis of a P D E that results from a similarity group trans- formation of (5.1.1). Such an approach was used in [32] for the uniform permittivity profile f(x) = 1. A closely related approach was used in [25] to determine the refined blow-up profile for a semilinear heat equation. We now briefly outline this method and the results that can be extended to the varying permittivity profile f(x): Continuing from (5.3.2) with touchdown point x = a, for s 3> 1 and |y| bounded we have. w ~ Wco + v, where v 1 and = (3A/(a)) 1 ^ 3 > 0. Keeping the quadratic terms in v, we obtain for N = 1 that ^ y wooh / ( a + y e - 3 / 2 ) , 2 [/(a + ye~''2) - f(a)} vs-vyy + - v y - v = —[l m ] + ^ v 3A/(a + y e - * / 2 ) r 2 | ^ (5.3.13) 1 « - ( 3 A / ( a ) ) tv2 + 0(v3 + e-^s) , for s 3>. 1 and bounded |y|, due to the assumption (5.1.2) that f(x) £ Ca(Ci) for some 0 < a < 1. As shown in [25] (see also [32]), the linearized operator in (5.3.13) has a one- dimensional nullspace when N = 1. By projecting the nonlinear term in (5.3.13) against the nullspace of the linearized operator, the following far-field behavior of v for s —> +oo and |y| bounded is obtained (see (1.7) of [25]): v ~ L ( 1 - 2 ) ' N = 1 - ( 5 - 3 - 1 4 ) The refined touchdown profile is then obtained from w ~ Woo + v, (5.3.1) and (5.3.14), which is for t -> T~, u ~ [3Xf(a)(T - 0 | V ( , - j p - ^ j + 8 ( r J ; - a e f r _ t ) | + • • • ) . AT = 1. (5.3.15) Combining Lemma 5.3.2 and (5.3.15) directly gives the following refined touchdown profile. T h e o r e m 5.3.3. Assume f satisfies (5.1.2) on a bounded domain fl in RN, and suppose u is a touchdown solution of (5.1.1) at finite time T. Assume touchdown set of u is a compact subset ofQ, and suppose N = 1 and x = a is a touchdown point ofu. Then we have lim_u{x,t)(T-t)~3 = (3A/(o))5 (5.3.16) uniformly on \x — a\ < CyJT — t for any bounded constant C. Moveover, when t —> T~, u ~ [ 3 V ( a ) ( r - o r ( i - + 8 ( r _ _ ( ) | + • . . ) , (5.3.17) We finally remark that applying formal asymptotic methods, when N = 1 the refined touch- down profile of (5.1.1) is also established in (4.5.12). B y making a binomial approximation, it is easy to compare that (5.3.15) agrees asymptotically with (4.5.12). 125 Chapter 5. Refined Touchdown Behavior 5.3.2 R e f i n e d t o u c h d o w n prof i l es for N > 2 For obtaining refined touchdown profiles in higher dimension, in this subsection we assume that f(r) — f(\x\) is radially symmetric and = BR(0) is a bounded ball in IR-̂ with N > 2. Then the uniqueness of solutions for (5.1.1) implies that the solution u of (5.1.1) must be radially symmetric. We study the refined touchdown profile for the special touchdown point r — 0 of u at finite time T. In this situation, the fact that the solution u of (5.1.1) is radially symmetric implies the radial symmetry of w(y, s) in y, and hence the radial symmetry of Woo(y) (cf. [34]). Note that Woo(y) is a radially symmetric solution of w«/ + ( ^ p ^ - | H + | « ' - ^ = 0 f o r y > 0 > ( 5 - 3 - 1 8 ) where wy(0) = 0 and /(0) > 0. For this case, applying Theorem 1.6 of [39] yields that every non-constant radial solution w(y) of (5.3.18) must be strictly increasing for all y sufficiently large, and w(y) tends to oo as y —> oo. It now reduces again from Lemma 5.3.1 that l im w(y,s) = ( 3 A / ( 0 ) )3 S—'OO ' uniformly on |y| < C for any bounded constant C. This gives the following touchdown rate. L e m m a 5.3.4. Assume f(r) = /(|a;|) satisfies (5.1.2) on a bounded ball BR(0) C Rn with N > 2, and suppose u is a unique touchdown solution of (5.1.1) at finite time T. Assume touchdown set for u is a compact subset of SI. Ifr = 0 is a touchdown point ofu, then we have lim_u{r,t)(T -t)~i = (3A/(0))s uniformly for r < C\/T — t for any bounded constant C. We next derive a refined touchdown profile (5.3.20). Similar to one dimensional case, indeed we can establish the refined touchdown profiles for varying permittivity profile / ( |x | ) defined in higher dimension N > 2. Specially, applying a result from [25], the refined touchdown profile for N = 2 is given by This leads to the following refined touchdown profile for higher dimensional case. T h e o r e m 5.3.5. Assume f satisfies (5.1.2) on a bounded domain Q in R N , and suppose u is a touchdown solution of (5.1.1) at finite time T. Assume touchdown set of u is a compact subset of fl, and suppose Q = BR(0) C M . n is a bounded ball with N > 2 and f(r) = / ( |x | ) is radially symmetric. If r = 0 is a touchdown point ofu, then we have lim_u{r,t)(T-t)-* = (3A/(0))3 (5.3.19) uniformly on r < C\/T — t for any bounded constant C. Moveover, when t u ~ [3 V (o)(r - tt" ( i - ^ L - ^ + 4 ( r _ t ) | ^ e ( r _ t ) | + • • • ) . T-, N = 2. (5.3.20) 126 Chapter 5. Refined Touchdown Behavior Remark 5.3.1. Applying analytical and numerical techniques, next section we shall show that Theorem 5.3.5 does hold for a larger class of profiles f(r) = f(\x\). Before concluding this section, it is interesting to compare the solution of (5.1.1) with that of the ordinary differential equation obtained by omitting A u . For that we focus on one dimensional case, and we compare the solutions of a, a), (5.3.21a) (5.3.21b) a, a), (5.3.22a) (5.3.22b) where / is assumed to satisfy (5.1.2) and (5.2.1). The ordinary differential equation (5.3.22) is explicitly solvable, and the solution touches down at finite time v(x,t) = (1 -3\f(x)t)* , (5.3.23) which shows that touchdown point of v is the maximum value point of f(x). In the partial differential equation (5.3.21), there is a contest between the dissipating effect of the Laplacian uxx and the singularizing effect of the nonlinearity f(x)/v?\ when u touches down at x = xn in finite time T, then the nonlinear term dominates (essentially, for some special cases, touchdown point xo of u is also the maximum value point of f{x), see Theorem 5.1.4 for details). However, we claim that a smoothing effect of the Laplacian can be still observed in the different character of touchdown. Indeed, letting /(yo) = max{/(a:) : x e (—a, a)}, then /'(j/o) = 0 and f"{yo) < 0. And (5.3.23) gives the finite touchdown time To for v satisfying Jo = l/[3A/(j/o)]- Furthermore, we can get from (5.3.23), together with the Taylor series of fix), lxm_{To-t)-U{yo + iTo-t)h,t) = (3A/( t / 0 ) ) f [ l - ^ ^ j M * ] ' ^ (3A / (*o))» • (5-3.24) And our Theorem 5.3.3 says that for such u we have Um ( r - t ) " 5 « ( s o + ( r - t ) 3 y , t ) = ( 3 A / ( i 0 ) ) » . (5.3.25) Comparing (5.3.24) with (5.3.25), we see that the touchdown of the partial differential equation (5.3.21) is "natter" than that of the ordinary differential equation (5.3.22). 5.4 Set of touchdown points This section is focussed on the set of touchdown points for (5.1.1), which may provide useful information on the design of M E M S devices. In §5.4.1, we consider the radially symmetric case where f(r) = fi\x\) with r = \x\ is a radial function and is a ball BR = {\x\ < R} C RN with N > 1. In §5.4.2, numerically we compute some simulations for one dimensional case, from which we discuss the compose of touchdown points for some explicit permittivity profiles fix). and ut - uxx = 2— in (- u(±a,t) = l; u(x,0) = l, A/(x) . , vt = ^ - in (- v(±a,t) = l; v(x,0) = l, 127 Chapter 5. Refined Touchdown Behavior 5.4.1 Radially symmetric case In this subsection, f(r) = f(\x\) is assumed to be a radial function and Q is assumed to be a ball B R = {\x\ < R} C RN with any N >1. For this radially symmetric case, the uniqueness of solutions for (5.1.1) implies that the solution u = u(x,t) of (5.1.1) must be radially symmetric. We begin with the following lemma for proving Theorem 5.1.4: Lemma 5.4.1. Suppose f(r) satisfies (5.1.2) and f'(r) < 0 in BR, and let u = u(r,t) be a touchdown solution of (5.1.1) at finite time T. Then ur > 0 in {0 < r < R] x (tn,T) for some 0 < tQ < T. Proof: Setting w = rN~lur, then (5.1.1) gives ^ - ^ r r ^ = - ^ , 0<t<T. (5.4.1) Differentiating (5.4.1) with respect to r, we obtain wt-wrr + wr fw = — > 0 , 0<t<T, (5.4.2) r u J ui since / ' ( r ) < 0 in B R . Therefore, w can not attain negative minimum in {0 < r < R} x (0,T). Since w(0,t) = w(r,0) = 0 and ut < 0 for all t € (0,T), we have w = rN~lur > 0 on OBR x (0,T). So the maximum principle shows that w > 0 in {0 < r < R] x (0,T). This gives N - 1 wt — wTr H wr> 0 in {0 < r < R] x (t\,T), r where t\ > 0 is chosen so that w(r, ti) ^ 0 in {0 < r < R}. Now compare w with the solution z of N - 1 z t - z r r - \ zr = 0 in {0 < r < R} x (t\,T) r subject to z(r, ti) = w(r, ti)for0<r<R, z(R, i) = w(R, t) > 0 and z(0, t) = 0 for tx < t < T. The comparison principle yields w > z in {0 < r < R} x (t\,T). On the other hand, for any to > £i we have z > 0 in {0 < r < R} x (tn,T). Consequently we conclude that w > 0, i.e ur > 0 in {0 < r < R} x (t0,T). • Proof of Theorem 5.1.4: For w = rN~lur, we set J{r,t) = w — e JQr f(s)ds, where 0 > N and e = e(Q) > 0 are constants to be determined. We calculate from (5.4.1) and (5.4.2) that Jt _ Jrr+^lJr=hJ+wstiv* _ ^1+eer,-,f r u6 uz >bxJ- rN~l (A - 6ere-N) f >bxJ, provided e is sufficiently small, where b\ is a locally bounded function. Here we have applied the assumption f'(r) < 0 and the relations ur = w/rN~l and w = J + e J 0 r f(s)ds. Note that J(0, t) = 0, and hence it follows that J can not obtain negative minimum in B R X (0,T). 128 Chapter 5. Refined Touchdown Behavior We next observe that J can not obtain negative minimum on {r = R} provided e is sufficiently small, which comes from the fact Jr(R,t) = wr-6eRe-1f{R) - 9eR°-lf{R) > RN~1f(R) [X - 9eR9~N} > 0 for sufficiently small e > 0, where (5.4.1) is applied. We now choose some 0 < to < T such that w(r, to) > 0 for 0 < r < R in view of Lemma 5.4.1. This gives ur{r, to) > 0 for 0 < r < R. Since ur(0,to) = 0, there exists some a > 0 such that ,n 4- \ v u r ( r , i o ) w(r,t0) urr(0,to) = l im —- = l im — 7 7 - r > 0. We now choose 9 = max{./V, N + a — 1}, from which one can further deduce that J(r , to) > 0 for 0 < r < R provided e = s(to, 9) > 0 is sufficiently small. (t». HO-l-i'artd X -a Figure 5.1: Left figure: plots of u versus x at different times with f(x) = 1 — x2 in the slab domain, where the unique touchdown point is x = 0. Right figure: plots ofu versus r = \x\ at different times with f(r) = 1 — r2 in the unit disk domain, where the unique touchdown point is r = 0 too. It now concludes from the maximum principle that J > 0 in BR X (to,T) provided e = e(to) > 0 is sufficiently small. This leads to u(r, t) > u{r, t) - u{0, t) > e [ ^° (ff̂ da. Jo s (5.4.3) Given small Co > 0, then the assumption of f(r) implies that there exists 0 < ro = ro(Cb) < R such that f(r) > Co on [0,r 0]. Denote rm = min{ro,r}, and then (5.4.3) gives u(r,t) > £ / Jo Jo <JV-1 1 oiV-l 9-N + 2 eCor9^N+2, where 0 - i V + 2 > 2 , which implies that r = 0 must be the unique touchdown point of u. • Before ending this subsection, we now present a few numerical simulations on Theorem 5.1.4. Here we apply the implicit Crank-Nicholson scheme. In the following simulations 1 ~ 3, 129 Chapter 5. Refined Touchdown Behavior (a). «x) - and * - 0 (*>)• tt.0 - m** >• - » Figure 5.2: Le/t figure: plots of u versus x at different times with f(x) = e~x in the slab domain, where the unique touchdown point-is x = 0. Right figure: plots ofu versus r = \x\ at different times with f(r) = e~r in the unit disk domain, where the unique touchdown point is r = 0 too. Figure 5.3: Left figure: plots of u versus x at different times with f(x) = ex _ 1 in the slab domain, where the unique touchdown point is still at x = 0. Right figure: plots of u versus r = \x\ at different times with f(r) = er _ 1 in the unit disk domain, where the touchdown points satisfy r = 0.51952. 130 Chapter 5. Refined Touchdown Behavior we always take A = 8 and the number of meshpoints N = 1000, and consider (5.1.1) in the following symmetric slab or unit disk domains: fi: [-1/2,1/2] (Slab); Q:x2+y2<l (Unit Disk) . (5.4.4) Simulation 1: / ( |x | ) = 1 — | x | 2 is chosen as a permittivity profile. In Figure 5.1(a), u versus x is plotted at different times for (5.1.1) in the symmetric slab domain. For this touchdown behavior, touchdown time is T = 0.044727 and the unique touchdown point is x = 0. In Figure 5.1(b), u versus r = \x\ is plotted at different times for (5.1.1) in the unit disk domain. For this touchdown behavior, touchdown time is T = 0.0455037 and the unique touchdown point is r = 0. Simulation 2: / ( |x | ) = e~l xl is chosen as a permittivity profile. In Figure 5.2(a), u versus x is plotted at different times for (5.1.1) in the symmetric slab domain. For this touchdown behavior, touchdown time is T = 0.044675 and the unique touchdown point is x = 0. In Figure 5.2(b), u versus r = \x\ is plotted at different times for (5.1.1) in the unit disk domain. For this touchdown behavior, touchdown time is T = 0.0450226 and the unique touchdown point is r = 0 too. Simulation 3: / ( |x | ) = e^ _ 1 is chosen as a permittivity profile. In Figure 5.3(a), u versus x is plotted at different times for (5.1.1) in the symmetric slab domain. For this touchdown behavior, touchdown time is T = 0.147223 and touchdown point is still uniquely at x = 0. In Figure 5.3(b), u versus r = \x\ is plotted at different times for (5.1.1) in the unit disk domain. For this touchdown behavior, touchdown time is T — 0.09065363, but touchdown points are at ro = 0.51952, which compose into the surface of J3 r o(0). This simulation shows that the assumption / ' ( r ) < 0 in Theorem 5.1.4 is just sufficient, not necessary. {a>. «*) - VS-x/2 and X - B <b). tjnj - m 1/a and X - 6 Figure 5.4: Left figure: plots ofu versus x at different times with f(x) — 1/2 — x/2 in the slab domain, where the unique touchdown point is x = —0.10761. Right figure: plots ofu versus r = \x\ at different times with f(x) = x + 1/2 in the slab domain, where the unique touchdown point is x = 0.17467. 5.4.2 One dimensional case For one dimensional case, Theorem 5.1.4 already gives that touchdown points must be unique if the permittivity profile f(x) is uniform. In the following, we choose some explicit varying 131 Chapter 5. Refined Touchdown Behavior permittivity profiles f(x) to perform two numerical simulations. Here we apply the implicit Crank-Nicholson scheme again. S i m u l a t i o n 4: Monotone Function f(x): We take A = 8 and the number of meshpoints N — 1000, and we consider (5.1.1) in the slab domain Q defined in (5.4.4). In Figure 5.4(a), the monotonically decreasing profile f(x) = 1/2 — x/2 is chosen, and u versus x is plotted for (5.1.1) at different times. For this touchdown behavior, the touchdown time is T = 0.09491808 and the unique touchdown point is x — —0.10761. In Figure 5.4(b), the monotonically increasing profile f(x) — x +1/2 is chosen, and u versus x is plotted for (5.1.1) at different times. For this touchdown behavior, the touchdown time is T = 0.0838265 and the unique touchdown point is x = 0.17467. For the general case where f(x) is monotone in a slab domain, it is interesting to look insights into whether the touchdown points must be unique. Figure 5.5: Plots ofu versus x at different times in the slab domain, for different permittivity profiles f[a](x) given by (5.4.5). Top left (a): when a — 0.5, two touchdown points are at x = ±0.12631. Top right (b): when a = 1, the unique touchdown point is at x = 0. Bot- tom Left (c): when a = 0.785, touchdown points are observed to consist of a closed interval [-0.0021255,0.0021255]. Bottom right (d): local amplified plots of(c). S i m u l a t i o n 5: "M"-Form Function f(x): In this simulation, we consider (5.1.1) in the slab domain Q defined in (5.4.4). Here we take A = 8 and the number of the meshpoints N = 2000, and the varying dielectric permittivity 132 Chapter 5. Refined Touchdown Behavior profiles satisfies C 1 - 16(a; + 1/4) 2 , if z < - 1 / 4 ; f[a](x)=< a + (l-a)|sm(27ra)|, if \x\ < 1/4; (5.4.5) { 1 - I6(x - 1/4) 2 , if x> 1/4 with a € [0,1], which has "M"-form. In Figure 5.5, u versus x is plotted at different times for (5.1.1) for different a, i.e for different permittivity profiles f[a](x). In Figure 5.5(a): when a — 0.5, the touchdown time is T = 0.05627054 and two touchdown points are at x — ±0.12631. In Figure 5.5(b): when a = 1, the touchdown time is T = 0.0443323 and the unique touchdown point is at x = 0. In Figure 5.5(c): when a = 0.785, the touchdown time is T = 0.04925421 and touchdown points are observed to compose into a closed interval [—0.0021255,0.0021255]. In Figure 5.5(d): local amplified plots of (c) at touchdown time t = T. This simulation shows for dimension N = 1 that the set of touchdown points may be composed of finite points or finite compact subsets of the domain, if the permittivity profile is ununiform. 133 Chapter 6 Thesis Summary In this thesis, we have used both analytical and numerical methods to analyze the most basic mathematical model describing the dynamics of an elastic membrane in an electrostatic M E M S . We have answered mathematical questions dealing with existence, uniqueness and regularity of solutions. We have also addressed problems of more applicable nature such as stability, as well as estimates on pull-in voltages and touchdown times in terms of the shape of the domain and the permittivity profile of the membrane. The thesis consists of two main parts: 6.1 Stationary Case This reflects the state of the membrane at equilibrium when the voltage is below the critical threshold. We have given a detailed and rigorous analysis of the pull-in voltage and the deflec- tion profile, as described by the solutions of the equation that models Electrostatic M E M S . By applying various numerical and analytic methods, we have given several useful upper and lower bounds for the pull-in voltage A*, by using modern mathematical tools such as Pohozaev-type estimates and Bandle's Schwarz symmetrization techniques. We do believe however that our estimates are not optimal and better ones, depending on the distribution of the permittivity profile and the shape of the domain, can still be obtained. We have studied the branch of stable and semi-stable solutions by using energy estimates and have shown how the problem is dependent on the dimension, the shape of the membrane and the permittivity profile. We have also used sophisticated blow-up analysis to give a rigorous analysis of the unstable solutions. We also established partial results about uniqueness and multiplicity of solutions at various voltage ranges. The case where we have a power law permittivity profile on a round ball is however completely understood. 6.2 Dynamic Case Here we analyze the evolution of the membrane's deflection with time. The system exhibits three types of behavior. We have global convergence to a stable stationary state whenever the voltage is below the critical threshold. We have touchdown in finite time when we are beyond, and we have possible touchdown in infinite time at the critical pull-in voltage. We give several useful estimates for the touchdown time in terms of the domain, the per- mittivity profile and the applied voltage. A detailed analysis of the geometry and "size" of the touchdown set is given, showing in particular how the permittivity profile and the shape of the membrane can be used to affect both the duration and the functioning of the M E M S . 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