Global questions for evolution equations Landau-Lifshitz flow and

by

Meijiao Guan

M.Sc., Huazhong University of Science and Technology, 2003 Ph.D., The University of British Columbia, 2009

A THESIS SUBMITTED IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF

DOCTOR OF PHILOSOPHY

in

The Faculty of Graduate Studies

(Mathematics)

THE UNIVERSITY OF BRITISH COLUMBIA (Vancouver) July 2009 © Meijiao Guan 2009 Abstract

This thesis concerns the stationary solutions and their stability for some evolution equations from physics. For these equations, the basic questions regarding the solutions concern existence, uniqueness, stability and singular ity formation. In this thesis, we consider two different classes of equations: the Landau-Lifshitz equations, and nonlinear Dirac equations. There are two different definitions of stationary solutions. For the Landau-Lifshitz equation, the stationary solution is time-independent, while for the Dirac equation, the stationary solution, also called solitary wave solution or ground state solution, is a solution which propagates without changing its shape. The class of Landau-Lifshitz equations (including harmonic map heat flow and Schrödinger map equations) arises in the study of ferromagnets (and anti-ferromagnets), liquid crystals, and is also very natural from a geometric standpoint. Harmonic maps are the stationary solutions to these equations. My thesis concerns the problems of singularity formation vs. global regu larity and long time asymptotics when the target space is a 2-sphere. We consider maps with some . I show that for m-equivariant maps with energy close to the harmonic map energy, the solutions to Landau Lifshitz equations are global in time and converge to a specific family of harmonic maps for big m, while for m = 1, a finite time blow up solution is constructed for harmonic map heat flow. A model equation for Schrödinger map equations is also studied in my thesis. Global existence and scattering for small solutions and local well-posedness for solutions with finite energy are proved. The existence of standing wave solutions for the is studied in my thesis. I construct a branch of solutions which is a con tinuous curve by a perturbation method. It refines the existing results that infinitely many stationary solutions exist, but with uniqueness and continu ity unknown. The ground state solutions of nonlinear Schrodinger equations yield solutions to nonlinear Dirac equations. We also show that this branch of solutions is unstable. This leads to a rigorous proof of the instability of the ground states, confirming non-rigorous results in the physical literature.

11 Abstract Acknowledgements Table Table Bibliography Statement 1 Bibliography 2 Introduction 2.3 2.2 2.4 1.1 2.1 1.2 Global of Introduction Finite Proof Derived 1.1.2 1.1.1 Objectives Introduction 1.2.3 1.2.2 1.2.4 1.1.3 1.2.1 Contents existence of of time Co-Authorship of Well-posedness flow Model Landau-Lifshitz Nonlinear equations Solitary Schrodinger equations Instability Global nonlinear the and blow main and Contents equation well and main wave up Dirac main of theorem heat posedness blow maps standing solutions results and results equation for flow equations up Schrodinger scattering and for waves . for . blow Landau-Lifshitz . a class for of up maps a the for model of Landau-Lifshitz nonllnear nonlinear equation flow Dirac Dirac for . . 44 48 29 23 23 38 13 10 15 14 16 16 17 iii II’ vi ii v 2 9 1 1 Table of Contents

3 Well-posedness and scattering for a model equation for Schrödinger maps 50 3.1 Introduction and main results 50 3.2 Local weilposedness 56 3.3 Global small solutions and scattering states 62

Bibliography 67

4 Solitary wave solutions for a class of nonlinear Dirac equa tions 69 4.1 Introduction 69 4.2 Preliminary lemmas 73 4.3 Proof of the main theorems 76

Bibliography 88

5 Instability of solitary waves for nonlinear Dirac equations 90 5.1 Introduction 90 5.2 Spectral analysis for the linearized operator 95

Bibliography 107

6 Conclusions 109 6.1 Summary 109 6.2 Future research 111

6.2.1 Blow up for 1-equivariant harmonic map heat flow . 111 6.2.2 Construction of unique ground states for nonlinear Dirac equation when 0 < 8 < 1 112 6.2.3 Asymptotic stability for the model equation for Schrödinger maps 113 6.2.4 Nonlinear instability of the ground states 113

Bibliography 115

iv Acknowledgements

I wish to express my sincere gratitude to my supervisors (in alphabetical order), professor Stephen Gustafson and professor Tai-Peng Tsai for their continued encouragement and invaluable suggestions during my studies at UBC. Without their inspiration and financial support, I could not finish my degree. Also I acknowledge my debt to Dr. Kyungkeun Kang and professor Dmitry Pelinovsky for their useful communications for my research. I would like to thank the department of Mathematics at UBC. Special thanks is devoted to our department secretary Lee Yupitun. Furthermore, I am deeply indebted to my friends at UBC. Throughout my thesis-writing period, they provided good advice to help get my thesis done and shared their experiences in many different ways. Lastly, I express my special thanks to my parents and my husband. Thanks for their encouragement and support during these years. This thesis is particularly devoted to the birth of my daughter.

v Statement of Co-Authorship

The second chapter of my thesis is co-written with my supervisors Stephen Gustafson and Tai-Peng Tsai. Inspired by their study on Schrödinger maps with energy near the harmonic map energy, we want to extend the anal ysis to harmonic map heat flow. Harmonic maps are the stationary solu tions to Landau-Lifshitz equations, including harmonic map heat flow and Schrödinger maps. These map equations should share some common proper ties. For this paper I obtained the key space-time estimates for the nonlinear heat-type equation in section (2.2). In section (2.3), the technical lemmas are proved by my supervisors. The manuscript was finished by me, and my supervisors made the correction. Chapter 5 is also a co-written with my supervisor Stephen Gustafson. The problem arose from the previous chapter on the nonlinear Dirac equa tion. I conjectured that the ground states are unstable. But we needed to verify it through the analysis of the linearized operator. Together with my supervisor Stephen Gustafson, we determined how to relate the eigenvalue to the linearized operator of nonlinear Schrodinger equation at its ground states (see Theorem 5.2.3). Finally I finished the manuscript.

vi Chapter 1 Introduction and main results

1.1 Introduction

Nonlinear evolution equations (partial differential equations with a time vari able) arise throughout the sciences as descriptions of dynamics in various sys tems. The classical examples include nonlinear heat, wave and Schrödinger equations. Recently, evolution equations have emerged as an important tool in geometry. A prime example is the application of the Ricci flow to the Poincaré conjecture. For the evolution equations, once the existence of a local in time solu tion for the Cauchy problem is established, the most basic global questions concern the existence of stationary solutions and their stability. Another important question is whether or not solutions can form singularities, which may prevent the solutions from existing for all times, and may represent a breakdown of the model. This thesis addresses these basic questions for two classes of equations: Landau-Lifshitz equations which arise both in physics and geometry, and nonlinear Dirac equations coming from physics. These equations share a common feature: they are equations not for typically scalar valued functions, but rather for maps into manifolds and vector space respectively. Then the analysis of these equations become more challenging. For Landau-Lifshitz equations, the target space is a manifold, more precisely the 2-sphere. It is the nontrivial geometry of the target which creates the nonlinearity and provides many of the interesting and difficult features of this problem. In the Dirac case, the map is a four-dimensional complex vector .4C Although this is a linear space, the vector map significantly complicates the construction of stationary solutions and the analysis of their stability. In what follows in this chapter, a brief review, including the physical and mathematical backgrounds, as well as the most recent known results related to my thesis are provided in Section 1.1. In Section 1.2, the main objectives

1 1.1. Introduction and methodologies in my thesis are introduced.

1.1.1 Landau-Lifshitz flow

The principle assumption of the macroscopic theory of ferromagnetism is that the state of a magnetic crystal is describable by the magnetization vector m, which is a function of space and time. Magnetization m is the quantity of magnetic moment per unit volume. Suppose in a small region dV C , there is a number N of magnetic moments then the magnetization is defined as

m=

It is known from that the magnetic moment is propor tional to the angular moment of . By the momentum theorem, the rate of change of the angular momentum is equal to the torque exerted on the particle by the magnetic H. Thus one ends up with a model which describes the precession of the magnetic moment j around the field H = — x H, where -y is the absolute value of the gyromagnetic ratio. By taking the volume average of both sides, one has the following continuum gyromagnetic precession model 8m = —‘ymx H.

In 1935 Landau and Lifshitz proposed the Landau-Lifshitz equation [51] as a model for the precessional motion of the magnetization, in which H is replaced by the effective field Heff. They arrived at the Landau-Lifshitz equation

= —‘ymX Heff. (1.1.1) The effective magnetic field Heff is equal to the variational derivative of the magnetic crystal energy with respect to the vector m. In equation (1.1.1), no dissipative terms appear. Nevertheless, dissipative processes take place within dynamic magnetization processes. Landau and Lifshitz proposed to introduce an additional torque term as a dissipation that pushes magneti zation in the direction of the effective field. Then, the Landau-Lifshitz (LL) equation becomes

3m A = —‘ymx Heff — iFmx (m X Heff), (1.1.2)

2 1.1. Introduction where ) > 0 is a phenomenological constant characteristic of the material. The effective magnetic field Heff is equal to the variational derivative of the magnetic crystal energy with respect to the vector H. In 1955, Gilbert [34]proposed to introduce a different damping term for Landau-Lifshitz equation (1.1.1). He derived an equation which is generally referred to as the Landau-Lifshitz-Gilbert (LLG) equation: 3m 3m = —7m x + X ._. (1.1.3)

From a mathematical view point, equation (1.1.2) and (1.1.3) are very sim ilar. The basic property of LL equation and LLG equation is that the magnitude of m is conserved since = 0. This implies that any mag netization motion, at a given location , will occur a sphere, which can be normalized to be the unit sphere. In the simplest case, the energy is just the “exchange energy” fcIVmIdx, , §2 and we can take Heff = —Lm. Let u = in : f C RTh x C 3R with = 1, then LL equation can be considered as a linear combination of heat I and Schrodinger flow for harmonic maps

= —au x (u x /u)+i3u x u, (1.1.4) where denotes the Laplace operator in R’, > 0 is a Gilbert damping constant, /3 IRand “ x “ denotes the usual vector product in .3R At first sight, this equation is a strongly coupled degenerate quasi-linear parabolic system, which makes it hard to analyze mathematically. There are other equivalent forms of LL equations. Suppose there are smooth solutions, by the vector cross product formula

ax (b xc) = (a.c)b— (a.b)c, one can easily verify that equation (1.1.4) is equivalent to ãtu = cu + 2u)IVuI + /3u x LU. (1.1.5) If we let U denote the orthogonal projection from 31R onto the tangent plane 2TS :={RIc.u=0} to g2 at n with 3

3 1.1. Introduction then an equivalent equation, written in a more geometric way, is 8tU = aPUZ.,u + ,BJUPUL\u where JU = ux is a rotation through 7r/2 on the tangent plane 2TS The borderline cases for Landau-Lifshitz equation include harmonic. map heat flow when 3 = 0, a = 1: ãu = iu + 2u,IVuI (1.1.6) and Schrödinger maps if a = 0, j3 = 1: 8u=uxzu. (1.1.7) The Dirichlet energy functional of (1.1.4) given by

E(u) = JIvuI2dx= plays an very important role in the analysis of these flow equations. The energy identity, obtained formally by taking the scalar product with pu/’u = u + 2uIVuI and integrating over 2 x [0,t), E(u(t)) + a f f Iu + 2uIdxdtIVuI = E(u(0)) implies that for a> 0, the energy is nonincreasing, while for a = 0, the en ergy is conserved. Moreover, with respect to scaling, the energy has critical dimension n = 2. Rescaling the spatial variable, we have E(u(.)) = where s > 0. Thus the energy is invariant under the scaling if space di mension n = 2. This suggests that n = 2 is critical for the formation of singularities for these equations. Another important feature of the domain 2JR problem is the relationship between the energy and the topology, as expressed by a lower bound for the energy:

E(u) IVuI 4Ideg(u)I = 2 2R 2dx —> 2• where deg(u) is the topological degree for the map u : 2JR 2S So space dimension 2 is particularly interesting mathematically.

4 1.1. Introduction

These equations have been widely studied by mathematicians and physi cists. One of the most interesting and challenging questions is that of sin gularity formation vs. global regularity: do all solutions with smooth initial data remain smooth for all time, or do they form singularities in finite time for some data? In the following, we describe some important results for the various map equations described above.

Harmonic map heat flow Among the Landau-Lifshitz flow equations (including harmonic map heat flow and Schrödinger maps), harmonic map heat flow is the best understood and studied. Equation (1.1.6) generalizes the linear heat equation to maps into Riemannian manifolds. In geometry, it arises in the construction of harmonic maps of certain homotopy types [61]. In physics it arises in the theory of ferromagnetic materials [24—26,51] and in the theory of liquid crystals [271. A more general setting for equation (1.1.6) is to assume u a differentiable mapping from M, a compact two-dimensional Riemannian manifold (possibly with smooth boundary) to a compact manifold N, which is isometrically embedded in Rk. Eells and Sampson (see [29]) used this equation to construct a harmonic map from M to N. They proved that this equation has a smooth solution defined for all time and converging to a harmonic map under the assumption that the sectional curvature of N was non-positive. This result is not true if no curvature assumptions are made on N. Struwe in [59]proved partial regularity for global weak solutions with finite initial energy (uo H’(M, N)), with at most finitely many singular space-time points where nonconstant harmonic maps “separate”. The small energy solutions are global. Freire [31] showed that the weak solution in [59] is unique if the energy is non-increasing along the flow. Since space dimension 2 is energy critical, much effort has been devoted 2,to the case where the domain is the unit disk in ,2R the target manifold is and for a special class of solutions:

u(., t) : (r, 0) — (cos mOsin (r, t), sin mOsin (r, t), cos (r, t)) e 2S C (1.1.8) for a positive integer m. (r, 0) are polar coordinates. Then the scalar func tion satisfies a nonlinear heat-type equation:

trr+r_m251, OO. (1.1.9) One specifies initial condition (r,O) = o(r), and typical boundary condi tions are (O, t) = 0, and (1, t) = i E Il’. In fact the requirement that

5 1.1. Introduction sin (0, t) = 0 is necessary for solutions to have finite energy + Sm E() = f (r )dr. Singularities can develop only at the origin. If singularity occurs at some space point r = ro 0, then the corresponding solution u(x, t) has infinitely many singular points along the circle IxI= ,r0 which is a contradiction to Struwe’s result. Using the standard notation for Lebesgue norms: we say solutions blow up at time T < oo, if limsup IIVu(.,t)II= 00, or limt-Tsup IIu(,t)IIL2 = 00, while u remains bounded (uI = 1). Thus, for equation (1.1.9), q blows up while remains bounded. The issue is whether all solutions eventually converge to equilibria or singularities form in finite time for some initial data. Intuitively if we choose initial data in a topological class which does not contain any equilibria, the solutions must blow up, at least in infinite time. For m = 1, global regularity is proved by Chang and Ding [17]if (r) qo I ir, 0 r 1. However the global solution in [17] may not subconverge to a harmonic map as t —> oc if i = ir, since there is no harmonic map satisfying both the boundary conditions. It must develop a singularity at t = oo. In 1992 collaborating with Ye [18], they showed (again for m = 1) that, indeed, finite time blow-up does occur for finite energy solutions if > ir. A result I I of [11] tells us that even if m = 1 and < K, finite time blow up is still possible if qo(r) rises above K for some r E (0, 1). As for m 2, the situation may be different. Grotowski and Shatah [38] observed the difference and proved that for boundary data II < 2ir, the solution remains regular for all time, so finite time blow up will not occur. Those results implying the finite-time blow-up do not predict at what rate the gradient should blow up. A direct calculation shows that one pa rameter family of finite energy, static solutions to equation (1.1.9) are given by f(r) = 2arctan-, \ >0. When blow up occurs at t = T, an appropriate rescale will reveal a stationary solution. Let R(t) > 0 be the rescale function, then locally in space lim $(t,rR(t)) = m2arctanr . 6 1.1. Introduction

In [10] the generic blow-up behavior (and blow-up rate) was analyzed via formal asymptotics by Berg, Hulfson and King, where they observed that whether or not singularities occur appears to depend on m, as well as on the initial and boundary data. Moreover, different blow up rates were given explicitly. In [1] Angenent and Hulshof rigorously prove the infinite time blow-up rate in [10] for a special setting, where they assume that the initial data can reach only one time. When blow up occurs, the value of at the origin jumps to another value, the solution changes to another topological class, and the energy jumps by an integer multiple of 4Trm. The harmonic map heat flow splits off “bubbles”, i.e. non constant harmonic maps separate at the singular points. In [57] Qing pointed out the energy loss at a singularity can be recovered as a finite sum of energies of tangent bubbles. After blow-up, the weak solutions can no longer be expected to be unique if the energy is not assumed to be decreasing. In [11] Bertsch, Passo and Van Der Hout constructed explicit examples for non-uniqueness of extensions of solutions after blow-up. These solutions are characterized by “backward bubbling” at some arbitrarily large time and all have uniformly bounded energy. The qualitative descriptions of Struwe’s solutions near their singular points are also given in [65, 66]. In addition to the critical space dimension 2, different space dimensions for harmonic map heat flow are also widely studied. Finite-time blow up was proved by Coron and Ghidaglia in [20] for certain smooth initial data from IR or S’ to §fl, n 3. Later Chen and Ding in [14] extended this result to n 3 without the assumption of symmetries of 5fl and the initial maps. For maps between the 3-dimensional ball and 2, the nonuniqueness of solutions was proved in [12, 13] for some initial data. Grotowski [37] established blow-up and convergence results for certain axially symmetric initial data.

Landau-Lifshitz flow

For Landau-Lifshitz flow equation, with the Schrödinger-type term 3 0, our understanding diminishes considerably. Indeed this equation is still parabolic, but maximum principle arguments are not readily applicable. Due to the extra nonlinear term u x u, more estimates are required in the proof of regularity results compared to those of harmonic map heat flow. The first existence results for weak solutions to LL equation are due to [68], see also [2, 7]. In [2], Alouges and Soyeur established a nonuniqueness result for weak solutions when E .31R Their approach was based on the method introduced in [13] to prove the nonuniqueness of weak solutions to

7 1.1. Introduction the harmonic map heat flow. For a mapping u from a two-dimensional com pact Riemannian manifold M to g2, partial regularity result are analogous extensions of those for Struwe’s solutions in [59]. In the case of OM = 0, Guo and Hong [44] proved the regularity of weak solutions for uo E H’ (M, )2S with the exception of at most finitely many singular space-time points; they are globally regular in the case of small initial energy. The arguments are based on the a priori uniform estimates for 0u and 2Dn. For M with smooth boundary, the similar results were obtained by Chen in [15, 16]. Moreover, the local behavior of the solution near its singularities was investigated in [16]. Instead of using the uniform estimates for and 2Du, L — L and W” estimates for the linear parabolic system were used to show the partial regularity of the weak solutions. The study of the weak solution near the singular points also follows from previous results in the harmonic map heat flow [11, 57]. For bounded domain in ,2R Harpes [48] analyzed the geometric description of the flow at isolated singularities and showed the non-uniqueness of extensions of the flow after blow-up. But the formation of singularities is still open. Since maximum principle arguments (for example, sub-solution construction) do not apply, the blow-up argument for harmonic map heat flow may not provide a useful tool for the Landau-Lifshitz flow equation.

Schrödinger maps In the case of c = 0, equation (1.1.4) becomes the Schrödinger map equation (1.1.7). The analysis of Schrödinger maps becomes more difficult, even the local-in-time theory is not yet well understood. There is a great deal of recent work on the local well-posedness problems in two space dimensions ([4], [5], [23], [49], [53], [63]), see also on [50, 55] for the “modified Schrödinger 52, map”. For maps u : R x R+ local well-p osedness is established for 0Vu e k> n/2 + 1 is an integer, and also the global well-posedness is proved for small data when ii > 2 in [63]. Chang, Shatah and Uhlenbeck in [19] considered the global well-posedness problem for finite energy. For 0U E H’(R’) (1.1.7) has a unique global solution. While for n = 2, small energy implies global existence and uniqueness for radial and equivariant —, maps. For u : 2R C ,3R by an m-equivariant map, we mean u(r,8) = emOv(r) (1.1.10) where m e Z a non-zero integer,(r, 8) are polar coordinates on ,2R and R is the matrix generating rotations around the u3-axis. The argument in [19] is based on a generalized version of the “Hasimoto transformation”. The key

8 1.1. Introduction observation involves the vector field w(x, t) = — !JiJuRu e which lies in the tangent plane to 52 at u for each x, t. For an appropriate choice of an orthonormal frame on the tangent plane, the coordinates of w satisfy a kind of cubic nonlinear Schrödinger equation. Then the standard estimates (Strichartz estimates) for nonlinear Schrodinger equations can be applied to this equation. Gustafson, Kang and Tsai in [45, 46] investigated Schrödinger flow equa tion for energy space initial data, i.e. the energy of the initial data is near the harmonic map energy 4irImI.Their results reveal that if the topological degree m of the map is at least four, blow-up does not occur, and the global in time solution converges (in a dispersive sense) to a fixed harmonic map for large initial data. This is the first general result for Schrödinger maps with non-small energy space initial data. It is still open whether or not finite-time singularities can form for Schrödinger maps from 2R x R to 2, partly because the class (1.1.8) is no longer preserved, as in the harmonic map heat flow. This motivated us to consider a model equation for Schrodinger maps.

1.1.2 Model equation for Schrödinger maps

Let u : 2R x —* .2S For geometric evolution equations such as harmonic map heat flow (1.1.6) and wave maps

PuUtt = Puu a special class of solutions (1.1.8) was preserved, which allows a reduction to a single scalar equation (e.g. equation (1.1.9)). However this class is not preserved by Schrödinger maps which makes the construction of singular solutions much harder. This is our motivation to introduce a model equation.

Let 7(x, t) : x R —* C be a radial scalar function and m > 0 be an integer. By analogy with (1.1.9) for the heat flow, we consider the nonlinear Schrodinger equation () =o(x). (1.1.11) The nonlinearity is designed to be gauge invariant (hence the 2L norm is preserved) and to admit a conserved energy defined by m E(c,b) irJ (IrI2 + —-sin2 hI)rdr. = 2r

9 1.1. Introduction

The nontrivial stationary solutions with finite energy are given by a 2- parameter class of functions := {eQ(r/s)IQ(r) = m),s2arctan(r > O,c e R}. Thus we comes up with two questions: whether we can draw the same conclusion as in [46] (the Schrödinger maps), i.e. harmonic maps are stable under this equation for large m, or can we show finite time blow up when m = 1? Moreover, since zero is a trivial static solution, do small solutions exist for all time? This equation is related to Cross-Pitaveskii equation (Nonlinear Schrodinger equation with nonzero boundary conditions, see [47]), but it is hard in some respects.

1.1.3 Nonlinear Dirac equations In physics, the Dirac equation is a relativistic quantum mechanical wave equation and provides a description of elementary -i particles, such as electrons. In 1928, British physicist derived the linear Dirac equation from the relation of the energy E and the momentum p of a free relativistic particle 2E = c2p + c24m where c is the speed of light, m is the rest, of the . Quantum mechanically , E = ih is the kinetic energy and p = —ihV e 3R is the momentum operator (h is Planck’s constant). For the wave function q5(x,t), a relativistic equation is obtained = m2c2, (V2 (1.1.12) — 2) In order to derive Dirac equation, Dirac proposed to factorize the left hand side of equation (1.1.12) as follows:

= (71 + + + 7°8t)(7’O + + Dz + — 720y 73t), where ’(j‘y°, = 1,2,3) are to be determined. On multiplying out the right 7 yi side, one found out ,y0 must satisfy 773 737 (70)2 + = ,j126 j70 +7 = 0, = I. These conditions could be met if ‘y°,73 are at least 4 x 4 matrices (see [64]) and then the wave functions have four components. The usual representation

10 1.1. Introduction

07O, is f n k /c i 0 (L2x2 I — k_I ‘ 2 — iS\U \ 0 ix) ‘ o ‘ — where are Pauli matrices:

(0 1” — (0 — (‘1 0 a 2 — o)’ o)’ ko —1 Given the factorization and equation (1.1.12), one can obtain the linear Dirac equation which is first order in space and time:

= — Dm = 0, Dm 7O_ichkOk + 27°.mc for ,b : x IR —* .4C Without loss of generality, we always assume c = h = 1. The Dirac operator is symmetric and has a negative continuous spectrum which is not bounded from below, as for —, which makes it harder to analyze mathematically and physically. On one hand, the energy functional is strongly indefinite. On the other hand, although there is no observable electron of negative energy, the negative spectrum plays an important role in the physics. The main interest in this thesis is to present the various results regarding the standing wave solutions for nonlinear Dirac equations. A general form of nonlinear Dirac equation is given by iOt’cb— Dm’b + 70VF(b) = 0. (1.1.13) From experimental data in [58], a Lorentz-invariant interaction term F(b) is chosen in order to find a model of the free localized electron (or on another spin-i particle). So the usual assumption on F is that F e 24C(C,R) and )8F(e = F() for all 0. As pointed out in [58], stationary wave solutions of equation (1.1.13) repre sent the state of a localized particle which can propagate without changing its shape (x,t) = where is a nonzero localized function satisfying Dmq — wq — 70VF() 0. (1.1.14) 11 1.1. Introduction

Different functions F have been used to model various types of self-interaction. In [58], Rafiada gave a very interesting review on the historic background of different models. The existence of standing wave solutions has been extensively studied by different methods. In [32, 33], Finkelstein et al. proposed various models for extended particles corresponding to the fourth order self-couplings like 75 = 70717273 F() := 2a() + 52b)b(y (1.1.15) where ‘z,b = (7°,?) and (.,.), is the Hermitian inner product in .4C This nonlinearity is a sum of a scalar and pseudoscalar terms. In these papers, they gave some numerical results of the structure of the solutions for dif ferent values of the parameters. The special case b = 0, a > 0, called the [60], is proposed by Soler to describe elementary . The advantage of this model is that its solutions can be factorized in spherical coordinates:

(1.1.16) if(r) cos’ sin ’1We Vazquez studied the Soler model in [67]and came up with a necessary condi tion for the existence of localized solutions (see also [52]). In [3]the existence of infinitely many standing waves are obtained. For the generalized Soler model when F(&) = G(),G E C(R,R),G(0) = 0. (1.1.17) the existence of infinity many stationary2 solutions have been obtained in [21] for some function G and w € (0,m). Since the localized solutions are separable in spherical coordinates, the nonlinear Dirac equation can be re duced to a nonautonomous planar differential system. This system can be solved by a shooting method. Later on , this result was extended to a wider class of nonlinearities by Merle [54]. In the case where G has a singularity at the origin like G(s) = —ISIP,0

m, there exists a solution of (1.1.14) such that has a compact support. But there are other models of self couplings for which the ansatz (1.1.16) is no longer valid, for instance (1.1.15) and

F() = iIc1 + byS2

12 1.2. Objectives with nonzero b and c, c2 > 0. Esteban and Séré in [28] studied this more general nonlinearity. They proved by a variational method, there exists an infinity of solutions under the assumption G’(x).xOG(x), 6>1, xEIR for 1 < al,a2 < None of the approaches mentioned above yield a curve of solutions: the continuity of with respect to w, even the uniqueness of was unknown. These issues are important to study the stability of the standing waves. To our knowledge, Ounaies [56]was the first one to consider the regularity of the stationary solutions. He related the solutions to (1.1.14) to those of nonlinear Schrödinger equations. The ground states of Schrödinger equations generate a branch of solutions with small parameter s = m — w for nonlinear Dirac equations. He claimed that for F(s) = sla,1 < < 2, is continuous w.r.t. w when w e (m — eo,m) for some sç > 0. For a thorough review on the linear and nonlinear Dirac equation, we refer to the work by Esteban, Lewin and Séré [30]. A basic question about standing waves is their stability, which has been studied for nonlinear Klein-Gordon equations and nonlinear Schrödinger equations. Grillakis, Shatah and Strauss [35, 36] proved a general orbital stability and instability condition in a very general setting, which can be applied to traveling waves of nonlinear PDEs such as Klein-Gordon, and Schrödinger and wave equations. Their assumptions allow the second vari ation operator to have only one simple negative eigenvalue, a kernel of di mension one and the rest of the spectrum to be positive and bounded away from zero. But this method cannot be applied to the Dirac operator di rectly. Contrary to —, the Dirac operator Dm = —i)’° y8 + 0m is not bounded from below. However there are some partial resultsj about the application of this method to the Dirac equation. Bogolubsky in [6]requires the positivity of the second variation of the energy functional as a necessary condition for stability. Werle [69], Strauss and Vázquez in [62] claim that the solitary waves are unstable, if the energy functional does not have a local minimum at the solitary waves.

1.2 Objectives

In the following I describe the results and the methods used in my thesis for the above equations.

13 1.2. Objectives

1.2.1 Global well posedness and blow up for Landau-Lifshitz flow

,. §2, For the Landau-Lifshitz flow equation (1.1.4) where u : 21R x the well posedness vs. blowup is studied in my thesis [39, 40]. A good starting point to analyze the flow equation is to assume some symmetry. For maps u with equivariant symmetry u = emRv(r), the energy E(u) has a minimal energy 4irImI,which is attainable 8by a two-parameter family of harmonic maps: = e(mOh(r/s), ’5H E IR, s> 0 / hi(r) \ / 2 ‘ \ I r+r h(r)=( 0 1=1 0 \ h3(r) J \ The harmonic maps are static solutions of the evolution equation. The natural question is to consider the stability of the harmonic maps under the Landau-Lifshitz flow. Our first result concerns m-equivariant maps with energy near the min imal energy 47r1m1, E(uo) = 47r1m1+ , 0 < öo << 1. We have shown that there is no finite time blowup for ml 4. Further more the solutions converge to a specific family of harmonic maps in the space-time norm sense. Hence we say that the harmonic maps are asymp totically stable under the Landau-Lifshitz flow. This result is a rigorous verification of [10] where the authors showed no singularity formation in finite time by formal asymptotic analysis. Our main ingredients involved in the proof are the usage of two different coordinate systems. In an ap propriate orthonormal frame on the tangent plane, the coordinates of the tangent vector field u,. — JuRu satisfy a nonlinear heat-Schrödinger type equation. It leaves us with an equation with small 2L initial data. This equation is also coupled to a 2-dimensional dynamical system describing the dynamics of the scaling parameter s(t) and rotation parametero(t) of a nearby harmonic map H(s(t),(t)). A careful choice of these parameters must be made at each time to allow estimates. The key to prove convergence of the solutions is the space-time estimates for the linear operator of the nonlinear heat-Schrödinger type equation. This can be done because of the energy inequality, the positivity of the energy and the assumption of radial functions.

14 1.2. Objectives

For harmonic map heat flow, i.e. /3 = 0, in the subclass of m-equivariant maps (see (1.1.8)), we proved that for m = 1, finite time singularities do occur for some initial data close to the energy of harmonic maps. This result is an adaptation of the blow up result in [18] for a disk domain 2D in .2R 1.2.2 Well-posedness and scattering of a model equation for Schrödinger maps Recall the model equation (1.1.11) sin2I4 2m 2I (0,r)=o(r) where q(x, t) 1l2 x R —> C is a radial scalar function and m> 0 is an integer. We are interested in finite energy solutions which leads to sin Io(x)I = 0 both at IxI= 0 and lxI= oo. Therefore this yields the following boundary conditions = {o: [0,oc) — C, 0E(

15 1.2. Objectives

1.2.3 Solitary wave solutions for a class of nonlinear Dirac equations

We consider a class of nonlinear Dirac equations in [41]

i8 + i7’Oj — m + ii° = 0. (1.2.2)

Under the spherical coordinates ansatz (1.1.16), the equation for solitary waves can be reduced to a nonautonomous planar differential system for (f,g). A rescaling argument reveals that the solutions to this system is generated by the ground states of nonlinear Schrödinger equations —+v— 2IvIv=0. (1.2.3) It is well known that for 8 e (0,2), equation (1.2.3) admits a unique solution called the ground state Q(x) which is smooth,positive, decreases monotoni cally as a functions of lxiand decays exponentially at infinity. We prove that when 1 < 8 < 2, there exists e0 > 0 such that for w E (m — Eo,m), there exists a solution (t, x) = and the mapping from w to is continuous. This result is different from that in [56j where Ounaies claimed it for 0 < 8 < 1. But with the restriction 0 < 8 < 1, we are unable to verify the Lipshitz continuity of the rionlinearities. Thus the contraction mapping theorem is not readily applied to construct solutions.

1.2.4 Instability of standing waves for the nonlinear Dirac equations The stability problem of the standing wave solutions for the nonlinear Dirac equation with scalar self-interaction is considered in [42]. It is shown that the branch of standing waves constructed in [41] is unstable. The question of stability is related to the eigenvalues of the linearized operator. To show the instability, the main goal is to show the linearized operator has an eigenvalue with positive real part. Since the linearized operator is four-by-four matrix, it is important to block-diagonalize it as in [22]. It turns out that the eigenvalue is related to that of the cubic, focusing and radial nonlinear Schrödinger equations. We use formal expansion of the eigenvalue and eigenfunction to show that there exists such an eigenvalue ). with Re A positive. Then we use the “Lyapounov-Schmidt reduction” method from bifurcation theory to verify it rigorously.

16 Bibliography

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22 Chapter 2 Global existence and blow up for Landau-Lifshitz flow

As we introduced in the first chapter, we have obtained global result for the Landau-Lifshitz equation, including harmonic map heat flow. The following content is concentrated on harmonic map heat flow. The proof of global regularity and asymptotic stability results for Landau-Lifshitz equation is similar and is given in [11] (see the remark (*)in Section 2.2).

2.1 Introduction and main results

The harmonic map heat flow we consider is given by the equation = 1u + 2u,IVuI u(x, 0) = Uo(x) (2.1.1) where u(., t) : C R” §, 2S is the 2-sphere {u = 1} = 3(‘ul,u2,u I lul ,3CR denotes the Laplace operator) in R”, 2IVuI= Z— This equa tion written in a more geometric way is 12() = puU Ut = D8u .

where U denotes the orthogonal projection from 3R onto the tangent plane 2TS :={ e 3R Iu =0} to 2 at u, 8 = -. is the usual partial derivative, and 3D is the covariant. derivative, acting on vector fields (x) e 2T()S •PU9 = — (0 . u)u = Oj + (Ou . )u. A version of this chapter has been published. Guan, M., Gustafson, S. and Tsai, T.-P. Global existence and blow-up for harmonic map heat flow, J. Duff. Equations (2009) 246, 1—20.

23 2.1. Introduction and main results

Equation (2.1.1) is the gradient flow for the energy functional

E(u) = L1vuI2 Static solutions of Equation (2.1.1) are harmonic maps from Q to .2S Equation (2.1.1) is a particular case of the harmonic map heat flow between Riemannian manifolds introduced by Eells and Sampson ([8]). On the other hand, Equation (2.1.1) is a borderline case of the Landau-Lifshitz-Gilbert equations which model isotropic ferromagnetic spin systems:

ut=aP/.u+buxP/.u, a>O. (2.1.2)

(see [14, 161). The harmonic map heat flow corresponds to the case a = 1,b= 0. In this chapter, we consider space dimension ii = 2, which makes the energy E(u) invariant under scaling, and so is in some sense a borderline case for the interesting question of singularity formation vs. global regularity: do all solutions with smooth initial data remain smooth for all time, or do they form singularities in finite time for some data? Let us recall some of the important results for n = 2. Struwe in [19] proved that weak solutions to Equation (2.1.1) exist globally for finite-energy initial data, and are smooth except for at most finitely many singular space- time points where non-constant harmonic maps “separate”. Also, solutions are global for small initial energy. Freire showed that the weak solution is unique if the energy is non-increasing along the flow ([9]). Much effort has been devoted to the case where the domain is the unit disk in ,2R and for a special class of solutions:

u(., t) : (r, 8) —÷ (cosm8 sin (r, t), sinm8sin (r, t), cos (r, t)) (2.1.3) for a positive integer m, usually m = 1. (r, 0) are polar coordinates. Then satisfies the equation:

trr+r_m2S1, 00. (2.1.4) r 2r One specifies initial conditions (r, 0) = qSo(r), and typical boundary condi tions are (0,t) = 0, and (1,t) = e R. For m = 1, global regularity is proved if Ic(O,r)I r in [4]. However even if the flow exists for all time, it may develop singularities at T = cc, so that it fails to converge asymptoti cally. In [5] the authors showed (again for m = 1) that, indeed, finite time

24 2.1. Introduction and main results blow-up does occur for finite energy solutions, if q > n. A result of [2] tells us that even if m = 1 and iI < 7t, finite time blow up is still possible if 1(0, r) rises above r for some r e (0, 1). Recently, the generic blow-up be havior (and blow-up rate) was analyzed via formal asymptotics in [1],where they observed that whether or not singularities occur appears to depend on the degree m, as well as on the initial and boundary data. One of the purposes of our study is to provide a rigorous proof of this observation. We note that finite-time singularities may also form in the harmonic map heat flow when n 3 ([3, 7]). It is worth remarking that the blow-up vs. global smoothness question is also currently studied for both the wave and Schrödinger “analogues” of the harmonic map heat flow. The possibility of finite-time blow-up for the energy-space critical (n = 2) wave maps was established recently ([15, 18]), while the problem remains open for n = 2 Schrödinger maps (the a = 0 case of (2.1.2)), though a partial answer was given in [13]: in contrast to the wave map case, high-degree equivariant (see next section for the definition) Schrödinger maps with near-harmonic energy are globally smooth. The main goal of the present paper is to address the global regularity vs. finite-time blowup question for a larger class of maps than (2.1.3), and for the problem on the plane, rather than a disk. This means that the evolution is no longer described by a single, simple nonlinear heat equation like (2.1.4), but rather by a more complex system. In particular, maximum principles are no longer available (at least directly).

To be more precise, we consider m-equivariant maps u : R x .• 2S 2 2 with m E Z a non-zero integer. An m-equivariant map u : —‘ is of the form u(r, ) = emOR v(r) 52, where (r,9) are polar coordinates on ,2R v : [0,co) — and R is the matrix generating rotations around the u3-axis: /0 —1 0\ /cos c — sin c 0 R 1 0 0 , sin c cos c 0 = ) e° = \o Do) \o o 1

In what follows, we will take m> 0 (the m < 0 cases are equivalent, by a simple transformation). If u is m-equivariant, we have 2IVuI = 2IUrI+ 1u = 2Ivr + IRvI2 and so 201 p00/ 2 r E(u)=lrJ rdr. (IvrI+—-(v+v))r / 2 25 2.1. Introduction and main results

For finite energy E(u), it is necessary to have v(0),v(oo) = ±, where k = (0,0, i)T (see [10] Section 2.2 for details). We fix v(0) = —kand denote by 2m the class of m-equivariant maps with v(oo) = k:

emGRv(r), = {u : u = (u) v(0) = —, v(oo) <, = We measure distances between maps in m in the energy norm lu — ulI = IIV(u— 2ü)11L The class contains (3.1.1) as a special case. (up to a trivial reflection m ‘U3 —# —‘U3, and ignoring boundary conditions). For u m-equivariant, the energy E(u) can be rewritten as follows:

00 2 E(u) = irf (IvTl2 + IJ0RvI2) rdr = irf lVr_JvRhl2rth+Emin where J0 := vx is a ir/2 rotation on 2TS and p00 , p00 Emin = 27rJ J’Rvrdr 1] r = 27r1m1J3(v)dr = 27r1m1[v3(oo)+ (using v + v + V 1). The number Emin, which depends only on the boundary conditions, is in fact 47r times the absolute value of the degree of the map u, considered as a map from 2S to itself by compactifying the domain 2R (via stereographic projection); the degree is defined, for example, by integrating the pullback by u of the volume form on It provides a lower bound for the energy of an m-equivariant map, E(u) > Emin, and this lower bound is attained if and only if

VT = HJVRV (2.1.5)

If v(oo) = —, the minimal energy is Emin = 0 and is attained by the constant map, u —k. On the other hand, if u E so that v(oc) = k, the minimal energy is E(u) Emin = 4rlml and is attained by the 2-parameter family of harmonic maps

:= {em0hs(r) [0,27r)} Is>0, a where h8’°(r) := e00h(r/s), 26 2.1. Introduction and main results and hi(r) / \ 2 1rIm — r_ImI h(r) = I 0 1, h,(r) = , ha(r) = rIm rImI rim rHmi \ It3T)/ \ /1 1 + 1 + We record for later use that h(r) satisfying (2.1.5) means m m (hi)r = ——h,h )r(h = —h,.2 3 r 3 r So (3m is the orbit of the single, harmonic map emORh(r) under the sym metries of the energy which preserve equivariance: scaling, and rotation. Explicitly, / cos(mO + c)h,(r/s) emORh8a(r) sin(m9 + a)hi(r/s) = ( h3(r/s) We begin with the energy-space local-in-time theory:

Theorem 2.1.1 Let m > 1. There exist S > 0 and C > 0 such that if U0 C Dm and (uo) = 4-,rm+ S for some 5o 5, then the following hold: (a) there exists T = T(uo) > 0 and a unique solution u(t) C C([0, T); m) to Equation (2.1.1). E(u(t)) is non-increasing forte [0,T). (b) there exist 8(t) e C([0,T); (0,oo)) and c(t) e C([0,T);R) so that u(x,t) — e(m0t))?h(r/s(t))W. ,9

Remark 2.1.2 Statement (b) of Theorem 2.1.1 implies the orbital stability of harmonic maps (at least up to the possible blow-up time) under the heat flow. If the initial data u0 is close to 0m in H’, then solutions of equation (2.1.1) will stay close to the harmonic maps in H’ (though not necessarily in 2).H Statement (c) can be viewed as a characterization of blow-up for energy near Emin: solutions blow-up if and only if the H’- nearest harmonic map “collapses” (i.e., its length-scale goes to zero). Here s(t) and c(t) are determined by finding, at each time t, the harmonic map which is H’- closest to u(t).

27 2.1. Introduction and main results

A theorem identical to Theorem 2.1.1 is established in [12] for the (more delicate) corresponding Schrödinger flow problem. The proof there uses the same geometric representation and decomposition of the solution used in the present paper, and indeed we show here that the same estimates (and more) hold for the linearized problem (Section 2.2) and the nonlinear terms (Section 2.3), and so the proof carries over with no significant alteration. For this reason, and since the full energy space local well-posedness (without symmetry or energy restrictions) is already well-understood for the heat flow (in particular, Struwe [19]), we will not provide the details. We remark that the blow-up characterization (2.1.7) corresponds to the “separation” of a harmonic map at a singularity in [19]. The next theorem, our main result, shows that when the degree is at least 4, singularities do not form, and we can describe precisely the asymptotic behavior:

Theorem 2.1.3 Let m > 4. There exists ö1 e (0, ó) and C> 0 such that if 8o < 6, then the existence time T = T(uo) in Theorem 2.1.1 can be taken to be T = cc. One also has IIV(u(x,t)— emSRh(5(t) t)))IIL2Lc,flLoOL2 < .0Co (2.1.8) Moreover there exist c, and positive s such that (s(t), c(t)) — (s, ) as t —* cc. (2.1.9) Remark 2.1.4 1. Not only is the solution global, but (2.1.8) and (2.1.9) show that u(., t) converges to a fixed harmonic map as t — cc (at least in a time-averaged sense) — in particular, this gives asymptotic stability of the harmonic maps for m 4.

2. For the cases m = 2, 3, we conjecture that solutions are still global, but this is presently beyond the reach of our methods. The technical reason is that we need r2hi(r) e 2L(rdr), which requires m > 3. The final theorem shows that when m = 1, finite-time blow-up does occur within our class of solutions.

Theorem 2.1.5 If m = 1, for any 6 > 0, there exists u0 E >J with 0 < E(uo) — < 62 such that the corresponding solution of the harmonic map heat flow blows up in finite time, in the sense that IIVu(.,t)ILc,o —‘ cc.

28 2.2. Derived nonlinear heat equation

Remark 2.1.6 Our result that blowup occurs for degree one, but not for higher degree, is consistent with the formal asymptotic analysis of [1].

The paper is organized as follows. In Section 2 we derive, from the harmonic map heat flow equation, a related nonlinear heat equation, by a choice of frame on the tangent space. We also establish space-time es timates (including “endpoint” -type estimates) and weighted estimates for the linear operator which comes from the perturbation about the harmonic maps. Even though the potential appearing in the linear operator behaves like 2l/1x1 both at the origin and as lxi—* oo, we can treat it by an energy inequality to avoid the difficulty. In Section 3, we obtain explicit equations for the parameters (s(t), c(t)) by a choice of suitable orthogonality condi tion which only works for m 3. On the basis of the space-time estimates obtained in Section 2, we give the proof of Theorem 2.1.3. In Section 4, we construct an example to show that finite time singularities really occur for energy close to the harmonic map energy when m = 1, proving Theo rem 2.1.5. Throughout the paper, the letter C is used to denote a generic constant, the value of which may change from line to line.

2.2 Derived nonlinear heat equation

In this section we derive a nonlinear heat equation associated to the har monic map heat flow. We use the technique introduced in [6], obtaining an equation for the coordinates of the tangent vector field v,- — mJvRv with respect to a certain orthonormal frame. Under the m-equivariance assumption that the solution to equation (2.1.1) has the form u(x, t) = emG?v(r, t), v satisfies the evolution equation:

Vt = (D + — ---)(vT — tmJVRV) where,2 recall, D is the , acting on vector fields tangent to at v. Let e E 2TS be a unit tangent vector field parallel transported along the curve v(., t) De=O. Then {e,J’-’e} is an orthonormal frame on 2TS Let q(r,t) = qj(r,t) + — !!2JvRv iq2(r, t) be the complex coordinates of the vector. field ‘vj,. 2TS in this basis m v. — JVRV = qie + Jve. r q2

29 2.2. Derived nonlinear heat equation

JU We sometimes write qe qj.e + q e for convenience. Define JveJvRv=vie+v v=v+izi Now is 12 it a straightforward2 matter to show that the complex function q(r, t) solves the following nonlinear heat equation. with a non-local nonlin earity — (1 —mV3) — m(v3)rq = 2 q — qN(q) (2.2.1) where

1 —my N(q) Q(r’)dr’, Q := i Tm (rT + mP + 3 q]) = f°° [r

We will use equation (2.2.1) to obtain estimates on q. Given an m-equivariant map u(x,t) E with E(uo) — 4irm < we would like to write the solution u = eme?v(r,t) with:

v(r,t) = e t)R(h(r/s(t)) +(r/s(t),t)) (2.2.2) where (r/s(t), t) is a perturbation. Using the explicit orthonormal basis of ,2TS 1 and 3jh 0 3 = ( = ( \oJ \ h1 J it is convenient to decompose the perturbation term into components tan gential and normal to 2S at h(p): (p,t) = z(p,t)3-{- (p,t)h(p,t)Jl3+ (2.2.3) for p = r/s(t). This decomposition defines the complex-valued function z := Using v3(p,t) 27 we find +iz = (p,t), z (v = 12 (p)+ 3)r which.z we substitute into h3(2.2.1) to obtain (p) — (r) qt=—Hq—2m h3 h3 q (2.2.4) — 332m +m m3q — m(3)rq 2h 2— 2 — qN(q), where H is the operator

= 1 + 2m — 2mh H = — + V(r), V(r) 3(r)

30 2.2. Derived nonlinear heat equation

So q(r, t) satisfies a nonlinear heat equation with linear operator H. Now the difficulty comes from the singular potential V(r) which behaves like const./r as r —* 0 and as r — oo (with different constants). To some extent,2 H is like the heat operator with an inverse-square potential which is studied in [21]. But their arguments only work for dimension n 3 because of the lack of Hardy inequality in dimension 2. In this chapter we need to obtain space-time estimates for e, the one-parameter semigroup generated by —H. We know that for the free heat operator the following inequalities hold ([10]):

lie $‘llLL < CIlIlL2, (2.2.5) I e(t—s)t f \ 3 fY S j S)uS LL ‘—‘ Jo t where (r,p) is an “admissible pair” — i.e., 1/r + 1/p = 1/2, (i,) is the conjugate exponent pair of another admissible pair (i, ), excluding the case r = = 2. But in a following Lemma, we prove that not only do estimates like (2.2.5) hold for the operator H, but the “endpoint” version (r = i = 2) also holds for radial functions and f. A preliminary lemma ensures that H is self adjoint.

Lemma 2.2.1 ([17] pp.161 ) Let V(r) be a continuous radial potential on R\{0} satisfying V(r)+ Then —L V(r) is essentially seif-adjoint on. °°(R\{0}). + 3 C On the basis of Lemma 2.2.1, we have the following:0

Lemma 2.2.2 The operator H extends to a positive self-adjoint operator on a domain D(H) with \{0})C8°(R C D(H) C ),L(R hence —H is the 2 {e_t}t>o infinitesimal generator of2 a contraction semigroup on 2).L(R Furthermore, D(H) C 2).L°°(R Proof. We first consider m 2. Since V(r) (1 — /rm) by Lemma 2.2.1, is essentially self-adjoint 2 H on C8°(R\{•0}), and so its closure (which we still denote by H) can be uniquely2extended to a self-adjoint, operator on a dense domain D(H) C 2).L(1R When m = 1, the operator H is simplified as 4 4 Hr+ r2 21+r 31 2.2. Derived nonlinear heat equation

By the above argument H = — + extends to a seif-adjoint operator on 2),L(R and under the bounded perturbation it remains seif-adjoint by the Kato perturbation theory ([17]). So, H generates a semigroup e_tH on ).L(R The non-negativity of e_tH2 2).L(RV immediately implies H 0, and so is a contraction semigroup on The final part of the lemma, the L°° estimate, is more delicate. Let e 2\{0}).C8°(R We have f {lV + }2V1y1 = (,H) and since for a fixed disk DR centered at the origin 2lxIV(lxl) 1 on DR, and V(lxl) bounded on D, (2.2.6) we conclude + C(ltii2 + IlHyll (2.2.7) lxi L2 2). Now multiply Hço = — f2f + Vçoby /jxl and integrate by partsto obtain llHil — — + )drd8 lxi 2L 0 0 2V p27r p00 1 + /r + 2(rV — )drd8 —)2 0 0 ( = J J 2/r and so by (2.2.6) again, and (2.2.7), VlilllxI” + lIlxl_3/2li2 2C(Jlll, + 2).ilHll (2.2.8) Fix p e 2(1,4/3), and set q := (2,4). Using (2.2.8), we have llliLP(DR) llHllLP(DR)+ llVIlLP(DR) + C(H II1x1312VIILQ(DR)Iiixi312col1L2(DR))

llsoilL2(D) llHcoIlL2+ llVllL(D) ISOIIL2C(liHiiL2 + IlOilL2) and a Sobolev inequality, yields the required estimate

IkolILco

32 2.2. Derived nonlinear heat equation

Remark 2.2.3 The Kato perturbation theory for seif-adjoint operators is not applicable here, since V(r) is too singular at the origin. Next we establish some properties of the semigroup e_tH satisfied by the well-known semigroup eta.

Lemma 2.2.4 Let {e_tH}t>o bethe semigroupgenerated by the operator H in 2).L(R Let 1 0 6 IIYIILa (here e’ can be defined by density). Proof. If a = b = 2, the statement just follows from the fact that {e_tH}to is a contraction semigroup on ).L(R Now let C°(R\{0}) C D(H). 2 = He_tHço = e_tHHy, Then u(t) e_tp D(H). Thus Hu(t) 2 and so IHu(t)IIL2 IIHsoI.Using (2.2.9), we find IIu(t)IL°° C(JIH’u(t) 11L2+ IU(t)1IL2) 2C(IIHoIIL+ IIS2IIL2), so there exists M> 0 such that sup, Iu(x,t)I 0 a.e. for each t > 0, since the semigroup et is positivity preserving (see pp. 246 in [17)). Since u(t) = e_to solves

Ut = — V(x)u, and V(x) > 0, given any 0 < o E °°(R\{0}), we have Ut < Lu, which means is a subsolution to the heat equation. Since t) e1ço 02C sup Iu(x, I M, it follows by the maximum principle that

0 < e_tIcp eço for all t> 0, and hence

e_tHLb( < c t_(h/a_1/b) I!ILa(R2).

2 ço = — p+ For general) 0, we can rewrite p where = ma.x{, 0} 0, = max{—,0} 0 and reach the same conclusion since Ie_tI etII. The proof of the inequality for y L follows by the density of C°°(R\{o}) in La. 02 Recall that the potential is singular at the origin. Fortunately, precisely because of its inverse-square form and positivity, it yields “endpoint”-type

33 2.2. Derived nonlinear heat equation space-time estimates. Consider the mixed space-time Lebesgue norms: for an interval I C R+, IfIILL(R2xI) := f2(LIf(x,t)IPdx)dt. Theorem 2.2.5 Let the exponent pairs (r,p) and (i) be “admissible” (i.e. 1/r + 1/p = 1/2), but exclude the case r = = 2. Then we have lift IIeIILL + e_(t_8)Hf(s)dsIILrL < C(IiIIL2 + IifiIL’Ls’) for all functions ,,f(.,t) on .2R If, in addition, m > 2, and ,f(.,t) are radialt functions, then the estimate holds also in the “endpoint” case r = = 2, and we have weighted estimates Iie_tIiLL + Ii(e)TIiLL2 tf e 22t_s)Hf(s)ds11 + li(f e f(5)d5)rIIL2L2t a> 1. For fixed p e (1, ], define F(t) = iIe_tSoiILp. By Lemma 2.2.4

So F is of weak type (1, ---), On the other hand,

Ie_tIiLrL CIROIILP, so F is of strong type (p, oo). By the Marcinkiewicz interpolation theorem, F is of strong type (a,r) with = —, r a>1, and iIetFoIILLp GRLa.

34 2.2. Derived nonlinear heat equation

Now we turn to the nonhomogeneous estimate. For 1 ‘ p oo, we have 1ft e_(t_8)Hf(s)dsiiL f( s)h/’h/P)iif(s)IiLwds, so by the Hardy-Littlewood inequality, tif e_(t_8)Hf(s)dsipLrL

IiUiILoo

IIUTIIL2L2+ IiIILL CIIVvIIL2L2 (2.2.12) since 2IVvi = 2irl + li2. Now v(x,t) solves the equation: 2m — 2mh Vt = LV 3 V (2.2.13) — r2 with initial data eiecp. Multiplying equation (2.2.13) by V, taking the real part and using 2m — 32mh > 0 (since m 2), then integrating over space and time, we arrive at

IiViioLl + IiVvlIL Iiv(0)II = 2riI’JI2.

35 2.2. Derived nonlinear heat equation

Note that using (2.2.11)-(2.2.12) gives us Ie_t OIL1 CIIp!1L2 (which in any case is covered by the above argument). Similarly4 we get:

= II ILLl+IIUrIILL

Now let 13)(i, = (2,oo). If w(r,t) := f e_(t_8)Hf(s)ds, then w(r,O) = 0. By the above arguments we get, for v = e8w, IIWIJL CIIVvIIL 2cff Ifvldxds 6IIvIILo + LiC(E)IIfII — 2 IIWIILLo + ()IIfIILLl

Taking e = 1/2, we obtain IWIIL2L Cf IIL2L1,the “endpoint” estimate we were seeking. We also get the weighted estimate, since IIILL + IPWrIILL IIVVL ff Ifvldxds CIIVILrLPIIfIIL/L!

As a direct result of this proof, we have:

Corollary 2.2.7 Theorem 2i.5 also holds for e_tH where H is any opera tor of the form 1

Remark (*). A theorem similar to Theorem 2.2.5 is obtained for the lin earized operator of Landau-Lifshitz equation. Let a = = 1. A Schrödinger heat type equation similar to equation (2.2.1) is obtained, where the linear part is qt = (1 + i)( — V(r))q. (2.2.14) We can space-time estimates for the linear evolution operator e_(1i)tH with out using maximum principle.

Theorem 2.2.8 Let the exponent pairs (r,p) and (i,) be “admissible” (i.e. 1/r + 1/p = 1/2), includingf the case r = = 2. Then we have lie_ti e_(t_s) LL + II f(S)d5IILrLP C( +

36 2.2. Derived nonlinear heat equation for m 2, and radial functions , f(., t). Moreover the weighted estimates hold

IIe_t(1IILL + II(e_t(1+)rIlLL

1 i f e_(t_8)(1+f(s)dsIIL2L2 + II(f e_(t_8) f(S)d5)rIL2L2

IIUIIL2L°° + IIUrIL2L2+ IIIILfL CIIVWIIL2L2.

Similarly multiplying the equation for w by D, taking the real part, and integrating in space and time (using the positivity of V),

IIVwIILL IIIIL2+ IwfILL.

37 2.3. Proof of the main theorem

Then

IIUIL2L + IIUTIIL2L2+ IHJIL2L2 CI +eIIuIILL +C(e)IfIIL2Li. If e is small, we arrive at the endpoint estimate IIfIILLo + IIUrIILL + IIIILL C(IIIIL2+ 1).IIfIILL By Holder inequality and interpolation yields all the desired estimates.

2.3 Proof of the main theorem

In this section we prove Theorem 2.1.3 which gives the global well-posedness for the equivariant harmonic map heat-flow with near-harmonic energy when the degree m is at least four. This is done through the study of a coupled system of ODEs for the parameters s(t) and a(t), and a nonlinear heat-type PDE for the deviation of the solution from the harmonic maps. In particular, we will show that the length-scales s(t) of certain “nearby” harmonic maps, stay bounded away from zero, and, in fact, converge as t —* oo. For an m-equivariant solution u(x, t) E 2m of (2.1.1), with initial energy E(uo)=4nm+5, so<

Lemma 2.3.1 /13J If m> 3 and 6 is sufficiently small, then for any map ‘U E m with (u) < 4nm + ö, there exists s > 0, a R, and a complex function z = z1 + iz, such that

u(r, 8) = )R[(1 7(p))h(p) zi(p)3 p := 8e(m + + + z2(p)J], r/s, with z satisfying (z,hl)L2(pdp) = 0 and IzIIc

Here X := {z: [0,oo) —* C E with the norm Iz1 2L(pdp), 2L(pdp)} 2 co Z , 2 1 ,‘ 2 zx.— I i)pup Jo p

38 2.3. Proof of the main theorem is the natural space for z, corresponding to the energy space H’ for u(x). As above, for u e , we define v(r) = e_mORu(x) = (1 + ‘y(p))h(p) + z1(p) + 2(p)J =: h(p) + z (p). 7)2 The pointwise constraint lvi= 1 gives 1 = 21z1+ (1 + and since (as we shall prove) remains pointwise small, 7piCIZpZl. 7= —1o,V1—izi 1712Ciz1 Making the decomposition2 given by Lemma, 2.3.1 for u(x, t), at each time t, yields the complex function z(p, t), and time-varying parameters s(t), a(t), which together give a full description of the solution map u(x, t). Since we will use the estimates of the previous section to estimate q(r, t) rather than z(p,t), we need to know that z can be controlled by q. This fol lows from the lemmas below. For convenience, we introduce spaces X, 2 p < cx),with the norm:

100 iIzIl := / (izI + p p so that X = .2X Lemma 2.3.2 /13J Let 2

3, then

lIzIlx CIILOzIILP IlIzI/p+2IiL2izi/p CiILoz/pIiL2 where 0L is the operator Lo:=(a+h(p))=h,(p)8_1 (2.3.1) p h,(p)

Since, modulo nonlinear terms, (Loz)(p) sq(sp), we also have:

Lemma 2.3.3 /13J Under the assumptions of Lemma 2.3.2, if lizlix<< 1, then 3 1—2/p Z Xp(pdp) — ,— q LP(rdr)

IIIIL2(pdp)+ Il-11L2(pdp)< Cs WrWL2(rdr)

39 2.3. Proof of the main theorem

So the original map u(x, t) can be fully described by the function z(p, t) and the parameters s(t)and (t), while z(p,t) can be controlled by q(r,t). So we are going to derive the equation for z(p, t) in order to estimate s(t) and c(t), and then use Lemma 2.3.3 and estimates on the equation for q to complete the proof of Theorem 2.1.3. Rewriting equation (2.1.1) in terms of the vector v(r, t) yields

R2. Vt = MrV + 2(IvrI+ IRvI2)v, Mr : ã + + (2.3.2) Inserting the decomposition

v(r,t) = et[h(p) + (p,t)J, p = r/s(t) into (2.3.2), wearriveat (Mp+Iap(h+)I2+IR(h+)I2)(h+). (2.3.3) Now using the further decomposition of the perturbation into tangent and normal components, = z + Jz2 + 7h, we find, after routine (though somewhat involved) computations, that the tangential components of (2.3.3) yield our desired equation for z: 2SZt = —Nz+ (ims — s26)hi + 1F + 2F (2.3.4) where N denotes the differential operator

N := —8 + -(1 — 2h) = (2.3.5) — 0LL (here L5 is the adjoint of 0L in L(pdp)). We will not write the nonlinear terms 1F and 2F explicitly, but 2only give the necessary estimates (we are omitting many of these details since very similar calculations are presented in [13]): Co>OsuchthatIIzIIx

40 2.3. Proof of the main theorem

We would like to impose some orthogonality condition on z which ensures: (a) solutions of (2.3.7) decay; (b) certain norms of z(p, t) are controlled by norms of q(r, t). Since N is seif-adjoint in L(pdp), and from (2.3.5)- (2.3.1) we see that ker(N) = span{hi}, it is natural2 to impose

(z, hl)L2 z(p)hj(p)pdp 0. (2.3.8) = f Lemma 2.3.3 then gives the desired control of z by q. Now we may explain the source of our restriction m 4. Firstly, in the energy space we have z X, and in general z .2L But we have (z,hl)L21 IIIIL2IPhlIL2 1zxph and so to make sense of the condition (2.3.8), we require z/p E ,2L which leads to the restriction m 3. The further restriction m > 3 is needed for (seemingly) technical reasons in the second estimate of Lemma 2.3.2 (and hence also in Lemma 2.3.3). The next step is to estimate the parameter velocities:

Lemma 2.3.4 If z satisfies (2.3.4), IzIIx<<1, and (z,hl)L2 0, then J

• 11z11L00

41 2.3. Proof of the main theorem

• 2liphliiLoo

Lemma 2.3.5 For cr > 0, set I := [0,u), Q := x I and define the norm

iill + + iITiiLL(Q)

If IlqoiIL2= 6// is sufficiently small, we have

iiqii C (iiqoliL2+ lJs’iiLr([o,])ils‘ilLr([o,u])iiqIl+ lilJ + ilil).

Proof. Note that

iiqll2(rdr) = iIvr — —J RvilL2(d) = (E(u) — 4irm) <(E(uo) - 4rm) = can be taken small. We start by rewriting equation (2.2.4) in integral form:

— (p) q(t) = e_tHqo e_(t_8)H(F(q(s)) h3 q(s))ds (2.3.10) + f + for 0 < t < u where

— 2m + m — m3q — m( : 33 F(q) = 2h 2 2 3)r q — qN(q) =: I +11+111. (2.3.11)

Due to Lemma 2.2.5 (including the endpoint case) we have + - (p) C(ilqoilL2 (r) h3 ilF(q) 1h3 + (2.3.12) liqily IiLL 1IL4I3L4/3)•

42 2.3. Proof of the main theorem

Note ha(r) — h3(p) h3(r) — (r/s) II IILL CIIqI2I h3 r2 (2.3.13) < CIIqI2 1IsIILi’oIIs — lIILi’° where the last estimate comes from expressing (r)—ha(r/s) as the integral of its derivative with respect to s. Next we use Lemma 2.3.3 to estimate IIF(q)IJ4/34/3(Q)h3 term by term. Note that the estimate of F(q) = I + II + III has some overlap with the nonlinear estimates appearing in [9], and so we only give brief computations. Recall v3(r,t) = h3(p,t) +3(p,t) and = z2h1 7h3+ for p = r/s(t), hence 2 IVIIL4’3C(s IqIILs+ (‘+ qIIL4) 34 PL8 PL

So we obtain

II’11L4/3L4/3C (iiqiii + IIILLf) C (IIqII+ IqII). (2.3.14)

Nextweestimate := II(m(3)T/r)qM4/34/3.Compute

— mh m7h] = [12 z1h32 + h3 + Again using Lemma 3.3, we arrive at III’HIL4/3L4/3C 4IIqIILL(1+ C(q + IIqI) (2.3.15) Finally, using the Hardy inequality ‘1 i/p (L(Lfd) XP_ldx) (f(Yf(u))PP_’dY) for f 0, inthecasep=p=2, wefind IIN(q)IILfCQI[L2 4C(Iq + and since i-’ <1, we obtain

II”UL4I3L/3 IIqULLfHN(q)WLL + IIq/rII 2 (2.3.16) C (IIqII+ IIqII). ) 43 24. Finite time blow up

Combining (2.3.12)- (2.3.16), completes the proof of Lemma 2.3.5. Now we are ready to finish the proof of Theorem 2.1.3. Completion of the proof of Theorem 2.1.3. From Lemma 2.3.1, we have = e(me+a[(1 +7(r/so))h(r/so) + (zo)i(r/so)+ (zo)(r/so)J’3] with (zo,hl)L2 = 0 and0 lizolix C5o.Let (r,t) u(sor,st).2 Then ü is also a solution to the heat flow equation (2.1.1) with initial data (r,0) = e(mO 1o)R[( 0+7(r))h(r) + (zo)i(r)3+ 2(zo)(r)J], and time-dependent decomposition

= e(me(t))R[(1 + 7(r/s(t)))h(r/s(t)) + zi(r/s(t),t) + (r/s(t),t)Jj with s(t) E C([0,T);Rj, (t) E C([0,T);R), s(0) = 1, z2and c(0) = cEO. If 5o is sufficiently small, the estimates of Lemma 2.3.4 and Lemma 2.3.5 together yield 118sIlL + IIlIL Cllql G8, and in particular that s(t) Co > 0. Hence the solution extends to T = and as t —* 00, s(t) — > 0, and a(t) —> a. Furthermore, for any pair (r,p)with+=,2roo, s

(t IIV(u— 9emRh8 t))IILrLP CS’IIZlILXp CIIqIIr CIIqy Coo. Finally, undoing the rescaling u(r, t) = ü(r/so, t/s) completes the proof of Theorem 2.1.3.

2.4 Finite time blow up

In this section we give the proof of Theorem 2.1.5 by constructing a 1- equivariant finite-time blow-up solution in 21R with near-harmonic energy. The proof is a variant of that of [5], adapted to the plane .2R One special subclass of 1-equivariarit solutions is given by

u(., t) (r, 8) — (cos 8 sin (r, t), sin 8 sin q(r, t), cos (r, t)), (2.4.1)

44 2.4. Finite time blow up where (r, 8) are the polar coordinates on the plane, and /(r, t) is the angle with the 3‘u-axis. If u solves the harmonic map heat flow, then, as is easily checked, (r, t) satisfies 1 sin2ql OO, 22r (2.4.2) = O(r).

The energy of u can be written in terms of q:

E(u(t)) = e() := + sm2 )rdr.

In order to have a degree-i solution with finite energy, we impose the bound ary conditions (O, t) = 0, lim t) = ir. (2.4.3) r—oo (r, We take C’ initial data:

tlo e C’([O,oo)), limo(r) = 0, lim o(r) = r. (2.4.4) r—*O r—oo

Local existence of a classical solution is straightforward: there is T> 0 such that (2.4.2)—(2.4.4) admits a unique solution (r,t) e ([0,oo)))C([0,Tj;C flC°°((0,oo) x (0,T))

(one way to see this is to solve the full harmonic map heat-flow with the initial data corresponding1 to co, locally in time in classical spaces, use the fact that the form (2.4.1) is preserved ([4]), and then recover (r, t)). Next we establish an extension to 2R of the comparison principle of [4] for the unit disk (where they observed that although equation (2.4.2) is singular at r = 0, the maximum principle may still be applied). Lemma 2.4.1 Let q1,12 E BC([0,oo) x [0,T]) fl C((0,oo) x (0,T)) be solutions of the problem (2.4.2)— (2.4.4) with initial 2data If ç5j then bi(r,t) b2(r,t), (r,t) [0,oo) x [0,T]. Proof. Let o := — i. Then satisfies = rr + + p(r, t), (2.4.5)

45 2.4. Finite time blow up where

sin 22 — sin 1 sin( — p(r,t) := = ——cos(h +2) 2 — 2r 2 @2—&) r Fix 1T e (0,T). Since 1(0,t) = 2(0,t) = 0, there exists S > 0 such that , c E [—7r/8,lr/8] in (0,6) x (0,Tij (continuity of and 2), and hence p < 0 on this set. Therefore, there is K 0 such that p K on (0,oo) x (0,7’i). Setting v(r,t) := e_(4)tp(r,t), (5.1.5) yields

Vt = Vrr + + (p(r,t) — K — 1)v. And setting we(r, t) := v(r, t) + 2f(T — t)_1eT/(4(T2_t)) for some 2T > ,1T we find 2 — 1)(we — w = w + + (p(r, t) — K — 2f(T t)_1eT/(4(T2_t))). (2.4.6) Now suppose inf[ ’i][0, 6w <0. By the boundary2 conditions and bound 0 7 wE(r,t) eness of , this) implies = inf[O)[OT w < 0 for some r > 0, t (0,Tij. Hence w(r,t) 0, w(r,t) = 0, and wr(r,t) 0. This contra wE 1 dicts (2.4.6). So we have 0, and] sending e —* 0, we recover 0 in [0,oo) x [0,1].T Since 1T 0, A(0) = .0A If TA := sup{t > 0, A(t) > 0} (the “blow-up time of f”), then the function

A(t) — 2 /,2 — r2(1+v)’\ f(r,t) := arccos 2 r )+arccos (r,t) e (A(t)2 2 2 2(1+v)) (0,1)x(0,TA) satisfies the following properties: (i) f E C°°([0,11 x (ii) limr_o f(r, t) = 0 for t [0,TA), 1imro f(r, TA) = (iii) there exists i > 0 such that for every t > i we can find ii) such that

1 sin2f ft TT+ (r,t) (0,1) x (0,TA). f — 22r for all a

46 2.4. Finite time blow up

Proof of Theorem 2.1.5. Given any small 6> 0, let the initial data qlo(r) to equation (2.4.2) be of the form

/s_r2 3 o(r) = arccos + + r) where (ir) is a non-negative C°° function supported in [, j. We can ensure It < (1) by choosing so = s(6) small enough (depending on 6) so that It — arccos () It — 6, and choosing (1) > 10 (thus can be chosen independent of 6). It is then easy to check that e(qSo) 4ir+ 062. Moreover, C(r) and s0 can be chosen such that e(O)(7/8 t, by continuity there exists T* (0,T) and y > it such that (1,t) > y for 0 < t < T. / 2_r2(l+v)\ Let h(r) = arccos 2+2(1+v)). Choose t sufficiently large to ensure h(1) = arccos <7— it. Let f(r,t) be the function from Lemma 2.4.2, and ()cr choose small enough so that property (iii) if Lemma 2.4.2 holds. And finally, choose )o small enough so that TA

1 sin2g gt=grr+—gr— 2r 0 f(r,0), r e [0,1], e(o) <4it+C6 (the last property can be achieved2 since it holds for both and 0), o(r) f(r, the latter on [0, 1]). Let 0T be the maximal existence time of the classical solution (r,t) with initial data co(r). By the comparison principle Lemma 4.1, (r, t) > /(r, t) for (r, t) E (0, oo) x (0, min{To, T}), and in particular, (1,t) > (1,t) > for 0 < t < T*. So (r,t) is a supersolution for prob lem (2.4.7), while f(r, t) is a subsolution. So by the maximum principle for this problem on the disk ([4]), for 0 < r < 1, we have (r, t) f(r, t). Hence (r, t) blows up (in the C’ sense) at or before time TA.

47 [10] [9] [8]

[4] [5] Bibliography [7] [6] 12] [3] [1] folds, flow flows ularity rio. de., 186 pp. Comm. applications eral Heat 161(2002) in of A. J. Y. J.-M. N.-H. K.-C. K.-C. J.B. M. harmonic Y. the 2, —212. 1682—1717. BELLS, Kluwer targets, FREIRE, CHEN, of BERTsCH, Flow Am. of GIGA, 507—515. BERG, harmonic of CoRoN, Pure harmonic CHANG, CHANG, harmonic CHANG, Weak 93-112. J. of W.-Y. Academic Comment J.H. harmonique, maps, Solutions Uniqueness Math AppI. J. Harmonic Solutions R. J.-M. HuLsH0F, W.Y. map W.-Y. SAMPSON, J. maps maps Invent. DING, 86 D. Math. SHATAH, heat for Publishers, math. GHIDAGLIA PAsso (1964), DING, from from of Maps DING, C.R. of Semilinear Blow 53 Math flow, & the the Helv., Harmonic (2000), surfaces, D 2 & J.R.KING, Acad. 109-160. & harmonic on & up A Navier- R. SIAM R. into 1990, 99. the Explosion result K. and V. 70(1995), YE, Sci Parabolic no. 567—578 Disk, S 2 , UHLENBEcK, D. J. J. global 37 mappings Paris Stokes on 5, Formal map Finite-time APP1. Differential Nemantics, HouT, — 590—602. Arch. the 48. en pp. existence flow Ser. (1990). Equations system, temps global MATH. asymptotics 310—338. Nonuniqueness of Rational I from 308 Riemannian Schrödinger blow-up fini J.-M. Geom. existence for J. surfaces (1989) Vol. in pour Duff. the Mech. L’ Corori of 36 of 63, heat le Eqns and Bubbling 339-344. for the flot (1992), to for No. mani maps, Anal. et flows Reg gen heat heat 61, des the 48 al. 5, Chapter 2. Bibliography

[11] M. GuAN, S. GusTAFs0N, K. KANG, T.-P. TsAI, Global Questions for Map Evolution Equations, Centre de Recherches Mathé matiques, CRM Proceedings and Lecture Notes,Vol. 44, 2008(61-73).

[12] S. GusTAFs0N, K. KANG, T.-P. TsAI, Schrödinger flow near har monic maps. Comm. Pure Appi. Math. 60 (2007), 463-499.

[13] S. GusTAFs0N, K. KANG, T.-P. TsAI, Asymptotic stability of har monic maps under the Schrodinger flow, Duke Math. J. 145, No. 3 (2008), 537-583.

[14] A. KosEvicH, B. IVANOV, & A. KOvALEv, Magnetic , Phys. Rep. 194 (1990) 117-238.

[15] J. KRIEGER, W. ScHLAG, D. TATARu, and blow up for charge one equivari ant critical wave maps, preprint, arxiv:math.AP/0610248.

[16] L. D. LANDAU & E. M. LIFsHITz, On the theory of the dispersion of magnetic permeability in ferromagnetic bodies, Phys. Z. Sowj. 8 (1935), 153; reproduced in Collected Papers of L. D. Landau, Pergamon Press, New York, 1965, 101-114.

[17] M. REED, B. SIMON, Method of Modern Mathematical Physics Vol. II: Fourier Analysis, Self-adjointness, New York: Springer-Verlag, 1990.

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49 Chapter 3 Well-posedness and scattering for a model equation for Schrödinger maps

3.1 Introduction and main results

Some geometric evolution equations from R° x R to g2 (the unit 2-sphere): harmonic map heat flow (HMHF) Utr=PLU

([1, 2, 5—7,10]), Schrödinger maps (SM) JPIU

([4, 8, 9]) and wave maps (WM) PU = PLU

([12, 13]) in critical dimension d = 2 have been studied (here P denotes the orthogonal projection from 3R onto the tangent plane of g2 and J = U x). For HMHF and WM equations, much effort has been devoted to a subclass of m-equivariant maps U(x, t) : 2R x R —* 2S

U(., t) : (r, 8) —* (cosm8 sinu(r, t), sin mO sinu(r, t), cos u(r, t)) (3.1.1)

A version of this chapter will be submitted for publication, Guan, M. Well-posedness and scattering for a model equation for Schrodinger maps.

50 3.1. Introduction and main results where u(r, t) stands for the longitudinal angle. Then the map equations are reduced to scalar PDEs for u as

ut(orutt) = u— -sin2u. (3.1.2)

However this subclass is not preserved by Schrodinger maps which makes the construction of singular solutions for Schrödinger flow much harder. This is our motivation to study for this model equation:

2m sin(21u1) jUt+U u=O, u(x,O)=uo(x). (3.1.3) 2 21u1 where u(x, t) : x IR — C is radial and m is a nonzero integer. Without loss of generality, we assume in > 0 in this context. Equation (3.1.3) is a non linear Schrodinger equation with smooth, but spatially varying nonlinearity. It is invariant under “gauge” rotation: u —* eiau, c E R. This equation is a natural Schrödinger analogue of equation (3.1.2). We observe that an energy is formally preserved by equation (3.1.3):

E(u(t)) =0, where the energy is defined by poo !_ 2 E(u) = 7t J 2(uJ + 2sin u)rdr.

Finite energy solutions require sin Iuo(x)I= 0 both at lxi= 0 and xl= cc. Therefore this yields the following boundary conditions

uo : = {uo: {0,oo) —* C,E(uo)

Throughout this chapter, we are interested in the global existence and long time behavior of the solutions.

51 3.1. Introduction and main results

Rewriting the energy E(n), we find out for solutions in the class u(O) = 0, uo(oo) = ir, E(u) has a minimal lower bound 4irm 00 2m E(u) = f 2(Iui + —- 2sin Iuhrdr msinu 2 1°°sinluj =ir f u,. — — rdr + 2irm Re I üurdr Jo r ui I .‘o u where sin 2m Ref üurdr = mf lul(ittI2)dT o Iui o iul dr = —27rm — cos(iuhdr = 4irm. J dr Theref ore E(u) > 4irm. The minimal energy is attainable when

— rnsiniul Ur = 0. (3.1.5) r ui

The solution to equation (3.1.5) is obtained by the 2-parameter family of harmonic maps: := {eQ(r/s)iQ(r) = m),o2arctan(r E IR,s > 0}. These harmonic maps are the stationary solutions of (3.1.3). Thus there are two natural questions: whether we can draw the same conclusion as in [9], the Schrödinger flow case, i.e. harmonic maps are stable under this equation for large m; and whether we can construct singular solutions when m = 1? Moreover equation (3.1.3) possesses constant solutions kir(k e Z) with finite energy. It is also natural to consider the stability of these static solutions. Compared to equation (3.1.2), the analysis of equation (3.1.3) is more complicated. It turns out to be related to the Gross-Pitaveskii equation(NLS with nonzero boundary conditions, see [11]). Let u(r, t) = S(r)+(r,t), where S(r) can be taken as either kir or Q(r), equation (3.1.3) becomes m m sin 2S(r) m = —77+ —-cos2S(r)Re,7+i----2 2 Im+ N(i),2 2S(r) (3.1.6) i(r,0) = iio(r), ?Jo(0)= ?70(oC)= 0.

52 3.1. Introduction and main results where N(ij) represents quadratic and higher order terms of ii

= sin2lii±SI — sin2S — sin2S N(ii) (ii + S) — cos 2S Re ii Tmii.

The convenient way to study equation (3.1.6) is to write the linear operator as a matrix operator acting on (Re ii Tm)T: = Lîj + nonlinear terms (3.1.7) where L= (3.1.8) (- ‘h-) L=-+---cos2S,2m msin2S r L=-+-- 2r 2S The operators L+, L_ are seif-adjoint with continuous spectrum [0,oo). For the non-seif-adjoint operator L, the imaginary axis is the continuous spec trum. Dispersive estimates for this kind of operator were obtained under various decay assumptions on the potential and the assumption that zero is neither an eigenvalue nor a resonance of L. But unfortunately these as sumptions do not hold for L if S = Q(r). Since on one hand Q(r/s) is the stationary solution to equation (3.1.3), then

- (irs -!sin2Q(r/s)) is=i = 0.

This yields LsinQ=0. Thus L has sin Q as the unique ground state if m 2(sin Q e )2L and as a resonance if m = 1(Isin QIIL2= oo). On the other hand, for the stationary solution eQ(r),

-(er - sin 2Q(r)e) =0 gives a resonance Q for L_, 2m L_Q = -Q+ —sin2Q22r = 0 since Q 0 2L for m 1. So it is unknown at this point how to get the dispersive estimates for the evolution operator et.

53 3.1. Introduction and main results

Because of the difficulties described above, in this chapter we will only consider finding local in time solutions with finite energy and global solutions with small energy. When E(uo) is small, we must have that uo(O) = uo(oo) = 0 and then zero is the static solution. Rewriting equation (3.1.3), we have m m sin I2u 2 2 —1)u=0. (3.1.9) r 12u1 This equation resembles cubic NLS with inverse square potential. The boundedness (smallness) of m I (ILr + )rdr—-juI Jo 2r implies boundedness (smallness) of E(u). Hence the natural space for u is u e H’ and e .2L This is different from usual cubic NLS equations where u E or u E H’. Let us introduce some Banach spaces. Define X := {u: [0,cc) —* Cpu,- E 2L(rdr), 2L(rdr)}, with the norm := {1ur12+ m2} rdr. IIII f°° For 2 < p < cc, also define X’ := {u [0,cc) —* CIUrE L?(rdr), E LP(rdr)}, with the norm IIuIIcp:= [ {ir + mJ-} rdr. So X = .2X For radial complex-valued function u(r), v(r), define the follow ing inner product,

(u, v)L2 ãvrdr = f and (u,V)x = f (ür(r)vr(r) + ü(r)v(r)) rdr. For an interval I c R, define space-time norms: IUI(I,x) f (f(lurIP+mP)rdr)dt. In this chapter, we will use the following Strichartz estimate and Sobolev type embedding theorem.

54 3.1. Introduction and main results

Lemma 3.1.1 (Strichartz estimate /3]) In space dimension , we say that a pair of exponents (q,r) is admissible if + = r < oo. Then we have (i) lie < CilllL2 (ii) ei(t_T)g(.,r)dr

One can find this Lemma in [8]. Here we provide a very elementary proof. For any radial function f e 02),C°°(R 00 00 f2(r) = _2f f(s)f’(s)ds = _2f -f’(s)sds. Thus by Holder inequality

If112) C (f(ifrl2 + m24)rdr).

The lemma follows by approximating f E X by functions in C fl X. Now we are in a position to state our theorems.

Theorem 3.1.3 (Local weilposedness) Let m 1. Let either S = 0 or S = Q(r) = 2arctan(rm). For any jj E X, there exists maximal time interval I = (Tmin, Tmax) containing 0, such that the integral equation of (3.1.6) has a unique solution in the class satisfying

r(r, t) = u(r, t) — S(r) e C(I; X) n L(I; )TX where2

55 3.2. Local weilposedness

We know from Lemma 3.2.1 in the next section, E(u) is finite if E X. The energy is not necessarily near the harmonic map energy. For maps with energy close to the harmonic map energy E(u) = 4irm + 62,0 < 6 << 1, the local existence can be extended to global solutions if we have a space-time estimate for the linear operator £. We hope to develop the global existence theory in forthcoming research.

Theorem 3.1.4 (Global weliposedness and scattering) For m 1, there exists Eo > 0 such that when uo e , k1 = k2 = 0 and

Iluolx Eo, then the solution u to equation (3.1.3) given in Theorem 3.1.3 is defined for all time u E C(R;X)flL”(IR;X Furthermore, there exist unique).T functions u+, u E X such that Iie_t_u(t) — uIix 0, as t

This result is consistent with Schrodinger flow in [4] (small energy implies global weilposeness). Since u(t) is radial, the operator — + - acting on u(t) is like — acting on function of the form v(x,t) = eimu(r,t). It suffices to prove that v is global and scatters in X. 6 Notation. In this chapter we use the notation A B whenever there exists some constant C > 0 so that A GB. Similarly, we use A B if A 5 B A. A << B means that for some constant c> 0, which may be choosen arbitrarily small, A cB. The letter C is used to denote a generic constant unless specified, the value of which may change from line to line. The proofs of Theorem 3.1.3 and Theorem 3.1.4 are given in section 3.2 and section 3.3 respectively.

3.2 Local wellposedness

In this section, we aim to get local in time solutions for ij equation. Let S = 0 or S = Q = 2arctan(r Substitution u = S + i into equation (3.1.3) yields ).m

2m . 2m sin 2S 2m it=—+-cos2SReij+’t- 2S Imi+N(ij), (3.2.1) (r,0) = m = uo — S(r) 2 56 __

3.2. Local weliposedness where N() = 775sin2frl±SI( sin2S Im—cos2SRe—i are nonlinear terms.) Let = + , and sin 2 21S + ui f(171,u2)= 2IS+uj (S+u), then using Taylor expansion for the function f u2), we have

IN(ui)I (Ifxx(1,2)7??I + Ify(1,2)’I + Ifxy(1,2)u717?2I) I72C(Su + 5).Iu1 where i is between 0 and u, 2 is between 0 and u. It is worth remarking that on the right hand, the role of S(r) is very important since we need S(r)/r to be bounded (seen the reason from the estimate (3.2.13)). Because of this, for the constant solution S(r) = r, even the local existence of the solutions to equation (3.1.6) is hard to obtain. In order to prove local exis tence, we need to have dispersive estimates for the linear operator near the origin. As r —* 0, £ is basically like —/. + - since sin 2S(r) hmcos2S(r) = 1, lim = 1. r—O r—*O 2S(r)

We treat the operator —L + ! as the linear operator and the differences !(cos 25— 1) — 1) as the perturbations. Then the natural space for u is X. In fact, u X implies E(u) is finite in the following lemma.

2 °° 2 2m 2 Lemma 3.2.1 Suppose ‘1I, = f0 (hr! +--H )rdr < co,i(0,t) = u(oo,t) = o and u(r,t) = 5(r) + u(r,t), then u E D. 7 Proof. If S = Q,rewriting the energy as

roo 2 2 m .2 .2 E(u) = 4irm + I + 2QrReuir + —-(sm + — sin Q))rdr. (IuI r IQ iI Using integration by parts

co 2 f 2QrRerkrdr = _f -sin2QReurdr. (3.2.2)

57 3.2. Local weilposedness

For the difference of the squares, writing the first few terms in the Taylor series for 2sin (Q+ ) , we get )2 n2 IQ+ — 2sin Q = sin 2Q Re ?7+ cos 2Q(Re sin2Q (3.23) + (Imp) 2 +R(?7). 2Q where R()I .3G Using (3.2.2), (3.2.3), the energy can be estimated as sm2Q E(u) < 4irm+f (177r12+-cos 2Q1Re?712+- ImI2+CII3)rdr.

To show E(u) is finite, it suffices to prove that the integral on the right hand is finite. Since II1IIx< oo, we claim that

f(Iii2 + cos2Q)Re7)l2 + 51IImj2)rdr <

The claim is true since cos2Q 2 asrO T ( —,- asr—÷oo and msin2Q f asr—*O 2r2 2Q as r —* oo —

From Lemma 3.1.2, HIL,co

E(n) = = (IrI E() f 1 < 2 + 2sinI)rdr The proof is complete.

58 3.2. Local weilposedness

Now we are ready to prove Theorem 3.1.3. The operator — + is basically — conjugated by eImOwhen acting on radial functions. By changing of variable from to with (x,t) = &meq(r,t), we get V’ IrIP+!cIIP,2

:= {v : — CIVv e L, v/ri }2L (3.2.4) and (P = {v : CIVv E L”, v/ri E L,2

Proof of local well-posedness. Let S = Q(r) in equation (3.1.6). The proof of S = 0 is similar. Since = eimSri, then solves the equation

= — + -(cos2Q — 1)(Re)eme + — 1)(Im)eime

+ —N(rl)eim8, o = e”°r1o. 1 (3.2.6) We use this equation to construct a contraction mapping. By Duhamel’s formula, it is enough to find solutions to the integral equation

= eto i ei(t_F((s))ds (t) + f (3.2.7) where .m (S1n2Q F(i) = -(cos 2Q —1)Re eimO + —1) jim8 + N()em6.

Define the solution map by

M()(x,t) = etto + if ei(t_5F((s))ds

We want to find fixed point of the map M in the set 4); D {(x, t) = (r, t)eimoi L°(I; ) fl L(I; iIiIL (3.2.8)

59 3.2. Local weilposedness for 6 > 0 to be specified later. Let I = (—T,T) E IRwith 0 e I. Suppose that for some 6> E ,1H L satisfies <6. (3.2.9) Then

IiM()IILr(J.)flL(I,4) < 26 + CIIVFIIL4/3(IL4/3) (3.2.10) where we have used Strichartz estimate Lemma 3.1.1 and IIIIL CIIVIILP. Then we estimate IIVFIIL4/3L4/3term by term. Let (r) = (cos2Q— t S f1 —m sin2Q 1), —1). Both functions f2(r) ——-(--— are smooth. Since IV(fi(r)Reeimo)I CIfiIIVI+IfirUD, By using of Holder inequality in space and time, we have

imO’ I HV(fiRee

lIM()lILnL <26+ 4 lIL4C(T” S 3 + + IIIIL44) T’44IIII 2 t S <2ö+C(Ti6+T62+63)4 <36

60 3.2. Local weilposedness if 6 and Tare small enough such that C(Ti+Ti6+62) 1/2. Then choosing the time interval I sufficiently small, we can ensure equation (3.2.9). Hence M maps to itself. Then we need to prove the contraction under the metric )12d( = IIi — 2IILooflL44. We will use the two inequalities, II2 — I2I I2 I1C(I + I2I)I1 — 2I and IIiI2i — + I22)I1 22II2I 12C([ — 2I. Let T be small enough. Then by Strichartzj estimates ),Jv1(d(.A4( 1CV(F( — /aF())IJL 12)) ) — 243LV2IIL4L4 +T’(IIV + / - 2VIIL4L4 41+ 12II(IIV + IIVlII)LLfIIVl — 24VIL4L I< C(T’ + T1/46 + 12 2 ) if 6,T are chosen sufficiently small. By the fixed point theorem, we get a solution on (—T,T). The regularity property of the solution follows from Strichartz estimates. It remains to establish the blowup alternative. We show the blow up alternative by contradiction. Suppose Tmax < co and III’L4((oT )4) < Let 0 < t < t + T < Tmax. It follows that

eitV(r) = V(t + r) — i ei(tt’)VF((r + t’))dt’.

Strichartz estimate and 111,4IlVIILfyield

it/,f \ r itLr7,-f \ e çiT ((O,Tmaxt),X e vc-r) ((O,Tmaxt),L 4L <2PlVIlL4((tTmax)L4)4L + ) + T lIViIL4((tTmax)L4)) + IIIl4((t,Tmax),L4))IIIIL((t,Tmax),L)

61 3.3. Global small solutions and scattering states

Therefore for t sufficiently close to Tmax(r —> 0) such that + T’/IIVIIL4((t,Tmax),L4) + IVII4((t,Tmax),L4)) and 2 o HIL4((t,Tmax),L4) we obtain Ii X7 itL.,-i7 ye çi ) ((O,Tmax_t),L By the existence theorem, can4L be extended past Tmax which is a contrac tion. This shows ) “‘RL4((O,Tmax),4) = 00. The local well-posedness theory for is a direct result of(r, t) = e_tmO(x, t). The energy E(u(t))(t e I) is conserved since

(sin2 E(u(t)) = 4m + f (ITI2+ 2QrRer + I(Q+ )I — 2sin Q))rdr.

This integral is a conserved quantity which follows formally from multiplying equation (3.2.1) by integrating over ,2R and taking the real part. This can be rigorously justified following along the line of [3]. The proof is complete.

3.3 Global small solutions and scattering states

In this section we prove Theorem 3.1.4. We first show that for small energy solutions, the local solutions and be extended to global solutions in time, then construct the scattering states and the wave operators. Recall equation (3.1.9)

m m sin 12u1 2 2 —1)u=O, u(x,O)=uo(x). I2uF There exists E such that if mlix EU, then u < ,0CE E(u) < 0CE and = 1G(u)l si2 2u - ii

We show that the corresponding maximal solution given by Theorem 3.1.3 is global in time, i.e. Tmin = Tmax= DO.

62 3.3. Global small solutions and scattering states

Let v(x, t) = eimGu(r,t), then v solves the equation

ivt + v + G(u)v = 0, vo(x) = 8uoeim (3.3.1) By Duhamel’s formula,

= etvo e(t_8)G(u)vds, v(t) + i L t I. For 0

g(t) = IVIIL((ot)) + IIVIL4((o,t),x4)

It follows from Strichartz estimates

2 g(t) CIIVvOIIL2+ L/IIVG(u)vIIL/

IIVliL4((O,Tmax),.4)<00, so that Tmax = co by the blow up alternative. This implies g(t) is bounded as t —*00 and v e L((0,oo),Xr). Next we construct the scattering states. Let w(t) = e_itIv(t), we have w(t) = vo+ f ei8G(u(s))v(s)ds. Therefore for 0 < t < T, = if w(t) — w(r) eG(u(s))v(s)ds.

63 3.3. Global small solutions and scattering states If follows from is unitaryf Hw(t)- w(r)II IeIv(s)I2v(s)IIids

II II4((t,r);L4)IIHL4((t,r);L4) + II II4((t,r);L4) By the global existence for v in 4LX , —* IIw(t)— w(r)II — 0 as r,t 00.

Therefore there exists v+ E X such that

Ie_ttv(t)— vII —* 0 as t —* oo.

One can show as well that there exists v E X such that

IIetv(t) — vIIi — 0 as t — —oo. We now construct the wave operators for v, which completes the proof of Theorem 3.1.4.

Lemma 3.3.1 (1) For every v+ E X, there exists a unique E X such that the solution v e C(R, X) of equation (3.3.1) satisfies

IIetv(t) — vIl. —* 0 as t 00

(2) For every v e X, there exists a unique L’ e X such that the solution V E C(R, X) of equation (3.3.1) satisfies

IIe_itv(t)— vIL —* 0 as t —> —00. Proof. We only prove (1), the proof of (2) is similar. Consider T> 0, by Duhamel’s formula on [T,oo), v satisfies the equation

v(t) = etv+ — if et8G(u(s))v(s)ds (3.3.2) for t > T. Now the idea is to solve equation (3.3.2) by the fixed-point theorem. Taking admissible pair (q, r) = (4,4) and applying Strichartz estimate, we get itL+ e V LX—

64 3.3. Global small solutions and scattering states

So CT —* 0 as T —* cc. Define the set D = {v E 4L(IT,X flL°° (IT,X) : IIVIIL4(IT4) 2C} and T(v) by ) 00 2 T(v)(t) = if ei(t_TG(u(s))v(s)ds.

Then

IIT(v)IIL(IT) + IIT()IIL4(IT,5C4) C(IIv/rII4(ITL4) + IVv4(JT,L4)) C(2C. We see if T is sufficiently large, such that 3C(2CT) CT, then IIT(v)IL(JT) + IT(v)IL4(IT,4) CT. Thus the solution map M defined by M(v)(t) = ettv+ + T(v)(t) for t > T maps D to itself if T is large enough. We can easily verify that 2d(Mvi,Mv 2),d(vi,v V1,V2 E D. So M has a fixed) point v e D satisfying equation (3.3.2) on [T,cc). Let = v(T) e X, and then ft v(t + T) = eit(T) + ei(t_G(u(s + T))v(s + T)ds.

Therefore v is the solution of the equation (3.3.1) with v(T) = . By the global existence solution of equation (3.3.1), we know v(0) e X is well defined and e_2tv(t) e18G(u(s))v(s)ds. — = if

Since v D, then

je_itv(t) —* 0 —, — vII 3 00((t,IIVII as t cc. therefore, v(0) = satisfies the conclusion)4 of the lemma. 65 3.3. Global small solutions and scattering states

Finally, we show uniqueness, let ,1i,b 2i,b E X and ,v1 v2 be the corre sponding solutions of (3.3.1) satisfying

IIe_itvj(t)— vII — 0 as t — co for j = 1, 2. It follows by the above arguments that v is a solution of equation (3.3.2), and satisfies vj 4L(R, 4).X By the routine argument we obtain vi(t) = v2(t) for t sufficiently large. The uniqueness of the Cauchy problem at finite time gives = .b2 The proof of Theorem 3.1.4 is complete.

66 Bibliography

[1] J.B. BERG, J. HuLsH0F, & J. R. KING. Formal asymptotics of Bub bling in the harmonic map heat flow. SIAM J. APP1. MATH. Vol. 63, No. 5, pp. 1682—1717

[2] M. BERTsCH, R. D. PAsso & R. V. D. HouT. Nonuniqueness for the Heat Flow of Harmonic Maps on the Disk. Arch. Rational Mech. Anal. 161(2002) 93-112

[3] T. CAzENAvE. Semilinear Schrödinger equations, Courant Lecture Notes in Mathematics, 10, New York University, Courant Institute of Mathe matical Sciences, New York; American Mathematical Society, Providence, RI, 2003

[4] N.-H. CHANG, J. SHATAH & K. UHLENBE0K. Schrodinger maps. Comm. Pure Appi. Math. 53 (2000), no. 5, 590—602

[5] K.-C. CHANG,W.Y. DING & R. YE. Finite-time blow-up of the heat flow of harmonic maps from surfaces. J. Duff. Geom. 36 (1992), no. 2, 507—515

[6] K.-C. CHANG, W.-Y. DING. A result on the global existence for heat flows of harmonic maps from 2D into .2S Nemantics, J.-M. Coron et al. de., Kiuwer Academic Publishers, 1990, 37—48

[7] M. GuAN, S. Gu5TAFs0N & T.-P. TsAI. Global existence and blow up for harmonic map heat flow. J. Duff. Equations 246 (2009) 1—20

[8] 5. Gu5TAF50N, K. KANG & T.-P. TsAI. Schrödinger flow near har monic maps. Comm. Pure Appl. Math. 60 no. 4 (2007), 463-499

[9] S. GusTAFs0N, K. KANG & T.-P. TsAI. Asymptotic stability of har monic maps under the Schrodinger flow. Duke Math. J. Volume 145, Num ber 3 (2008), 537-583

[10] J. F. GRoTowsKI, J. SHATAH. Geometric evolution equations in cir itcal dimensions. Calc. Var. (2007) 30: 499-512

67 Chapter 3. Bibliography

[11] S. GusTAFs0N, K. NAKANIsHI & T.-P. TsAI. Global Dispersive So lutions for the Gross-Pitaevskii Equation in Two and Three Dimensions. Ann. Henri Poincaré 8 (2007), 1303-1331

[12] J. KRIECER, W. SCHLAG, D. TATARu. Renormalization and Blow Up for Charge One Equivariant Critical Wave Maps, Invent. Math. 171 (2008), no. 3, 543—615

[13] I. R0DNIANsKI, J. STERBENz. On the formation of singularities in the critical 0(3) a-model, arxiv:math.AP/0605023

68 Chapter 4 Solitary wave solutions for a class of nonlinear Dirac equations

4.1 Introduction

A class of nonlinear Dirac equations for elementary spin-i particles (such as electrons) is of the form

— m + F() = 0. (4.1.1)

Here F : R —‘ R models the nonlinear interaction, : 41R — 4C is a four- component wave function, and m is a positive number. 8, = 8/ax, and ‘y are the 4 x 4 Dirac matrices: k) 7k = (_k k = 1,2,3 = ( ) where k are Pauli matrices:

1 — (0 1” 2 — (0 i’\ — (1 0 i o)’ o)’ —1 We define

= 70 = () = ()

A version of this chapter has been submitted for publication. Guan, M. Solitary wave solut ions for a class of nonlinear Dirac equations.

69 4.1. Introduction where (.,.)is the Hermitian inner product in C’. Throughout this chapter we are interested in the case

F(s) = IsI°, 0 < 8 < oo. (4.1.2)

The local and global existence problems for nonlinearity as above have been considered in [5, 8]. For us, we seek standing waves (or solitary wave solu tions, or ground states solutions of (4.1.1)) of the form b(xo,x) = e_t(x)

Cz where x0 = t, x = (x,, X2, x3). It follows that : 3R —+ solves the equation

— m + + F() = 0. (4.1.3)

Different functions F have been used to model various types of self couplings. Stationary states of the nonlinear Dirac field with the scalar fourth order self coupling (corresponding to F(s) = s ) were first considered by Soler [11, 12] proposing them as a model of extended fermions. Subsequently, existence of stationary states under certain hypotheses on F was studied by Balabane [1], Cazenave and Vazquez [3] and Merle[6], where by shooting method they established the existence of infinitely many localized solutions for every 0 < w < m. Esteban and Séré in [4], by a variational method, proved the existence of an infinity of solutions in a more general case for nonlinearity F() = + 7bIS2), 75 = 70717273 for 0 < ai, c2 < . Vazquez [15]prove the existence of localized solutions ob tained as a Klein-Gordon limit for the nonlinear Dirac equation (F(s) = s). A summary of different models with numerical and theoretical developments is described by Ranada [10]. None of the approaches mentioned above yield a curve of solutions: the continuity of with respect to w, and the uniqueness of was unknown. Our purpose is to give some positive answers to these open problems. These issues are important to study the stability of the standing waves, a question we will address in future work.

70 4.1. Introduction

Following [11], we study solutions which are separable in spherical coor dinates,

(x) = where r = lxi,(‘.1’,) are the angular parameters and f, g are radial func tions. Equation (4.1.3) is then reduced to a nonautonomous planar differ ential system in the r variable fI+f=(g2_f26_(m_w))g (414) = 2(1g_1218_ (m+w))f.

Ounaies in [9] studied the existence of solutions for equation (4.1.3) using a perturbation method. Let e = m — . By a rescaling argument, (4.1.4) can be transformed into a perturbed system

u’ + — 1v1 + v — (iv — Eu — = 0, v28 2 2 I )v28iv1 (4.1.5) v’ + 2mu — E(1 + 2iv — 2eul°)u = 0 If = 0, (4.1.5) can be related to the nonlinear Schrodinger equation

_+v_ivl20v=0, u=—--—. (4.1.6) 2m 2m

It is well known that for e E (0,2), the first equation in (4.1.6) admits a unique positive, radially and symmetric solution called the ground state Q(x) which is smooth, decreases monotonically as a function of xl and decays exponential at infinity(see [13] and references therein). Let 0U = (Q,—Q’), then we want to continue Uo to yield a branch of bound states with parameter 6 for (4.1.5) by contraction mapping theorem. Ounaies carried out this analysis for 0 < < 1 and he claimed that the nonlinearities in (4.1.5) are continuously differentiable. But with the restriction 0 8 1 we are < < unable to verify it. The term 21v — 2i°eu has a cancelation cone when v = Along this cone, the first derivative of — is unbounded for 0 < 8 1. But Ounaies’ argument may go Iv2 2Eu < through for 9 1, which gives us the motivation of the current research. However we can not work in the natural Sobolev space H’ 3(1R 2).1R Since ‘—* we lose regularity. To overcome , we )3H’(1R 63),L(1R these difficulties, 71 4.1. Introduction want to consider equation (4.1.5) in the Sobolev space W’P(IRS, 2II),p > 2 and 8> 1. To state the main result, we introduce the following notations. For any 1 < p < oo,L = 3L(1R denotes the Lebesgue space for radial functions on .3R = W,’’(R)) denotes the Sobolev space for radial functions on .3R Let X? = x Y,? = L? x Li?. Unless specified, the constant C is generic and may vary from line to line. In this chapter, we assume that m = , since after a rescaling b(x) = (2m)W(2mx), equation (4.1.1) becomes +F()=O.

We prove the following results:

Theorem 4.1.1 Let e = m — . For 1 < 8 < 2 there exists €j = 60(8) > 0 and a unique solution of (4.1.4) (f,g)(e) E ),W,’(1R,RC((0,e satisfy ing )) f(r) = 6(-Q’(/r) +042 e2(r)) g(r) = S(Q(vr) + ei(r)) with IIejiIWi,2 Ce for some C = C(8) > 0,j = 1,2. Remark: The necessary condition w m must be satisfied in order to guarantee the existence of localized states for the nonlinear Dirac equation (see [15], [7]).

The solutions constructed in Theorem 4.1.1 have more regularity. In fact, they are classical solutions and have exponential decay at infinity.

Theorem 4.1.2 There exists C = C(e) > 0,o = u(e) > 0 such that Iej(r)I+ Iörej(r)I TCe j = 1,2. Moreover, the solutions (f,g) in Theorem 4.1.1 are classical solutions f,ge fl w,’P. 2

72 4.2. Preliminary lemmas

Remark. From the physical view point, the nonlinear Dirac equation with F(s) = s (Soler model) is the most interesting. In fact, Theorem 4.1.1, Theorem 4.1.2 are both true for the Soler model. In fact, from (4.1.5) one can find out that 2(v — )2eu — v2 = 2—eu which is Lipschitz continuous. An adaption of the proofs of the above theorems will yield:

Theorem 4.1.3 For the Soler model F(s) = s, there is a localized solution of equation (4.1.3) satisfying Theorem 4.1.1 and Theorem 4.1.2.

Next we proceed as follows. In section 2, we introduce several prelim inary lemmas. In section 3, we give the proof of Theorem 4.1.1, Theorem 4.1.2.

4.2 Preliminary lemmas

We list several lemmas which will be used in Section 3. Lemma 4.2.1 Let g : R —p R be defined by g(t) = tt,28 0 > 0, then g(a + g(a) — (26 + 1)IaI29u + C2uI201)2 ) — 29(CiIa where depends on 0 and = 0 if ’ 12C,0 1C 0<0 Proof. We may assume that a> 0 in our proof. It is trivial if a = 0. So we assume that a 0. If a < 21a1,then a + °i <31o1and

g(a + a) — g(a)— (26 + 1)a29a

0, so that g(a+a) = ’.20(a+a) Taylor’s theorem gives = g(a + a) — g(a)— (26 + a261)a

73 4.2. Preliminary lemmas where is between a+ and a. Since g”() = 28(28+1)29_1, if 28—1 <0, then g”()I ’.C28 If 28 — 1 > 0, we have < Cmax{(a + ’}u)28’,a C(a°’ + o1281). Hence we prove the lemma.

Lemma 4.2.2 For any a, b E IR,8> 0, we have

Ia— 8bI — IaI 0. If a < 2IbI,then

- 8b1 - aI C(Ia° + IbI°)

On the other hand, if a 21b1,then a — bI a — IbI IbI.So by using the mean value theorem Ia- bI°- IaI = 8’IbIOItI where t is between a — b and a. If 8 — 1 > 0, then

ItI°’ < C(a°’ + IbI°’), hence bI°- Ia- IaI IbI

Lemma 4.2.3 For any a,b,c e R, ifl 8<2, then

a + b+ 9c1 — a + 9b1 — a + cI°+ IaI° C(IcI°’ + IbI’)IbI, where C depends on 8.

74 4.2. Preliminary lemmas

Remark. This inequality is symmetric about b, c, so the right hand side can be equivalently replaced by C(lcI’ + lbI°’)lcl.Without loss of generality, weassumethat bi Id in the following. Proof. For simplicity, let L = Ia+ b + 9Cl — Ia+ bI° — a + 8c1 + .9al It is trivial for 8 = 1, since if lal 5IbIthen L = 0. If la 51b1,

ILl< C(IbI+ Id),

So next we consider 8 > 1. If al 51b1,by triangle inequality and Lemma 4.2.2, we have LI

If lal 5lbI,by using Taylor’s theorem ILl= c)I°lbcI.CI(a+tib+t where t12,t E (0,1) and + tib 2 — 2lbl — (a + t2c)l > lal id Id. Soifl<8<2,wehave ILl< 11b1.CIeI° The proof is complete.

Lemma 4.2.4 Let 2

Proof. We begin with p = cc. Using integration by parts

f(r) = (af + f)p2dp. (4.2.1) r2 fT0 P Hence f f2Ir I< iIf + fIIL s2ds = IIfr + fIIL

75 4.3. Proof of the main theorems which gives IIi

I = 2ir + f)Lr2dr.

By Holder inequality, I < 2(D)lIfrCIILIIL + fiIL2(D). On the other hand, we have 1 llil2(D) + 2(r2f(r2) - 2rif(ri)). Since rf)2(r > 0 we have Illi2(D)

Let T2 —p cc, r1 —> 0, we obtain

2 lIliL2f C8,. + flIL2.

The intermediate case 2

4.3 Proof of the main theorems

Similar to [9], we use a rescaling argument to transform (4.1.4) into a per turbed system. Let e = m — (remember m = ). The first step is to introduce the new variables

f(T) = E 20 u(/T), g(T) 620 where (f,g) are the solutions of (4.1.4). Then (u,v) solve

u’ + — 1v1 + v — (1v— — 1v1 = 0, v28 2 2i°eu )v20 (4.3.1) ‘ + — e(1 + 21v — 2eu 8)u = 0.

76 4.3. Proof of the main theorems

Our goal is to solve (4.3.1) near E = 0. If e = 0, (4.3.1) becomes

2 u’ + —u — + v = 0 r vIv20 (4.3.2) VI + U = 0. This yields the elliptic equation

—v + v = v,281v1 u = —v” (4.3.3) It is well known that for 0 < 6 < 2, there exists a unique positive radial solution Q(z) = Q(IxI)of the first equation in (4.3.3) which is smooth and exponentially decaying. This solution called a nonlinear ground state. Therefore U = (—Q’,Q)is the unique solution to (4.3.3) under the condition that v is real and positive. We want to ensure that the ground state solutions Uo can be continued to yield a branch of solutions of (4.3.1). Let v(r) = Q(r) + ei(r), u(r) = -Q’(r) + e2(r). Substitution into (4.3.1) gives rise to

e(r) + e2(r) + e1 — (26+ 291)Q = Ki(e,ei,e e1 (4.3.4) = 2 e(r) + e2(r) ) where Ki(e,ei,e IQ+e(Q+ei)—(26+1)Q 1+28_Q )2 + 2(v2820 — 286U — v)v29 2K(e, ci, e2) e(1 + 21v — J28eu)u. Define L the first order e1linear differential operator L : X — Y,? by e1 = (1—(26+1)Q 8r+ (ei e2) 28 Or 1 )e2 Then we aim to solve the equation Le=K(E,e) (4.3.5) where e = (ei,e)T,K(e,e) = (Ki,K)T(c,e). Let 1= (O,),u>0. We say e(e) is a weak2 X-solution to equation2 (4.3.5) if e satisfies e = L’K(e, e) (4.3.6) for a.e. e e I. L is indeed invertible as we learn from the following lemma.

77 4.3. Proof of the main theorems

Lemma 4.3.1 Let 0 < 8 < 2, the linear differential operator L_(1(28+1 8r+ 1 is an isomorphism from Xf onto Y??for 2 p 00. Proof. First we prove that L is one to one. Suppose that there exist radial functions el, e2 e such that e1 L ( = 0. \\ e2 J Then —rel + e1 —(28 + e1261)Q = 0, e = —e. (4.3.7) It is well known (see, eg. [14]) that e1 = 0 is the unique solution in .1H Next we prove that L is onto. Indeed L is a sum of an isomorphism and a relatively compact perturbation: L= ( 288r-i-)+(_(20+1)Q(r) ) =L+i. M is relatively compact because of the exponentially decay of the ground state at infinity. So we only need to prove that L is an isomorphism from X, to Y,°, i.e. for any (1,2) e L? x L, there exist (el,e2) e W, x W,’’ such that ‘e2J \2 It is equivalent to solve

e1 + (ôr + )e2 = 1 (4.3.8) ôrel + e2 = and show that ei, e2 e By eliminating e2 we know that ei satisfies

(— + 1)ei = —(ãr + (4.3.9)

Define G(x) = (47r)_hIxI_1e_khi. (4.3.9) has the solution

ei = G(x) * - ( + = 1G(x)*q1 +8,G(x)*b .2 78 4.3. Proof of the main theorems

Here we have used the property of convolution and the fact (ãr + )*f(r) = —8rf(r) in .3JR By Young’s inequality and G,0rG 3),L’(R we have IIelIILp IIGILLi11111LP+ IIDrGIIL1II2IIL which implies ei E L.

Similarly e2 satisfies —8r&.(—r+1+)e2= Let H(x) = G(x), then

e2 —H(x)*(8rcii)2 =H(x)* =H(x)*+(arH+H)*i eL since H, (ar+ )H e2L’(R ). To 3 improve the regularities2 of ei, e2, we go back to (4.3.8). Since = — e E L, we have e1 E Regarding the regularity of e2, we know that —e(aT+)e EL. By Lemma 4.2.4 21= II8re2ILp 0 such that for every 0 < e < e, there is a unique solution to equation (4.3.6) e = L’K(E,e)

79

For Thus

then Let where

and available

and for Let Y,?

in

(Iv 20 ’

a

Fix

any

if

Ki(e,e)

us

IKflIL4

suppose

IKjIjL4,leta=v 2 =(Q+el) 2 ,b=ru 2

small

K(E,

e

C

consider

e

3,

q

+

K 2 (,ei,e 2 ) Ki(e,

for

Xi?.

if

to

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ball

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p>

<

is 11L’K(E,

=

be

K 2 . e

=

Recall

Cge(Q

C(QI G

e 1 ,

a

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in

chosen

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3.

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Q.

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e2)

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Li’.

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constant

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e 1 1 28 (Q

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that

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+

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that

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show

IIKNIL

that

< +

=

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C(IQ

IQ+e1I28(Q+e1)_tQ+f1I29(Q+fi)_(26+1)IQ+fi28(ei_fi)

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4.3.

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+

that

the

+ fIIw —

- to

-

different

theorems

IIei

ei)218)

4.2.3.

+ +

Q’

IaIi

I(Q

third

estimate

ei)2 (Q b, ei)2 - -

-

+

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us

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1

f)

and 82

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regularity.

following sufficiently

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there Therefore Thus

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then Next

can

for

unique

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e,

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its

continuity

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6

we

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contractibility. sufficiently

us

assume

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can

4.3.2

prove

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fixed

standard

only

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if

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used

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a

8

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0

1,

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b

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f)IiLP

ia+b+ci

smail.

lemma:

a

done

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ci

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cl-Ia

consider

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C 8 6 112 contraction

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<8

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6

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map

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L’

has

taking

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LI

(4.3.5).

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more 5IcI},

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that

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83

e Slci},

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Next Lemma

So

Since and Recall

and

Proof

It

Let

follows

K(ei,e 2 )

by

L

gives

from

el,e2

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that

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e

el,

isomorphism

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we

4.3.2,

K(f 1 ,

if

e2

u

have

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4.1.2.

1K 2 1

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r

1

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IK1I IVF(u)IILr

Vu

Lemma

from

e2)

(

Proof

L°°(R 3 ),

el,e2

p

First

E

e 1

(Iel—flI+1e2—f2D.

e(IuI

E

C,(IvI 20 ’

E

L,

X

4 p<+oo

q

4 p

+ of

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E

+ we

fl

< fl

then

Q’1 28

4 p

the

4 p

then

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vI 2 ’

fl

can

Y’.

fl

and

main

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14’’

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(

K 1

We

prove

+

Iei 28

LxL.

Lemma

+

K 1

IuI 28 ’)

x

theorems

x

x

know

IuI 26 )

W,’’

K 2

that

+

L T

4.2.3

e2 2 °

that

and

x

+

L

f 1 I

for

+

p

f2 28 )

4.

By 84

Thus

with

where We

If

if g

Since find

generality, where

know

theorem.

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and are =

ii

the

We

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classical

prove

is

e

g(ro)

g”(r)

el,

claim

h’

small

f

uj,6 back

— conclude

=

€2

e2

e 1 ”

h,

>

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v(_e_(r_r0)

suppose

are

then

is

E

to

<

enough

0

by solutions. —

el(ro)

we

not

W 2 ’

0,

is

e2

e 1

equation

classical

g”

an

g’(ru)

that

g

arbitrary show =

=

true,

derivatives

satisfies

application e

and

cri(r)e 2

Si(r)eu

such

el(r)I

(1

4.3.

there

(ro) (1

=

then

that

+

solutions

h(r)

+

+

1o’I,

(4.3.5),

that

0.

6 i)g

= g(r)O

/3e1(7’_T0))

Proof

+

1 3)

and

+

exist

But +

g(r) 2€ je2p2P

=

ei,

e2(r)I 6

<

in

6 2 (r)eç

u 2 (r)e

+

of

(TO

e2

this 0,g(oo)

0

we

52g (4.3.2)

of

obtains constants

and

+

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<

have

is Ce(i

the

know

<

contradicts

for

<

+ +

ii

sufficiently

+

+ maximum eu,

Ce” T

zih

(1 main

6 3 (r)Q

<

and

3 (r)Q

< +

=

exponential

II

maximum

rro, that

1e21 0.

eT_T

and

1,2,3)

1

r 0 ,

after

Thus

is

for

theorems

<

v(e),

0.

el,e2

+

Q

to

with

C€

r

principle.

large).

for

for

öu

for

tedious

>

be

we

C(e)

by

at

+

h,

r

r

r 0 .

E

equation

decay

r

claim

r

determined

large

large

Sobolev’s

then

5 3 1)h

W’’ large.

=

Let

positive

computations

r 1

Without

at

that

C

and

(4.3.13)

infinity.

C 2 .

embedding

such

g(r 1 )

later.

So

(4.3.13)

(4

(4.3.12)

loss

(f,g)

since

that

3

>

We

11)

we

85

0.

of If

where

We

mined

Then

in

if E(ei,

not and

Remark. Letting Thus Then

for the claim

E

a

r

IE(ei(ro), want

right

valid,

small

e

similar

large

Iei(ro)

fi)

under

similarly

is

h

later,

E

/3 true

=

H 2 . hand

=

to

IE(ei(r),fi(r))I

enough. —+

Let

,,/jQ’(ro)l.

For

enough.

(

way.

know this

we

0

if

(Q+ei) 2 —E(Q’) 2 This

fi(ro))I

us

fi(ro) side

,

0

we

z-’

E(ei(ro),fi(ro))I

assume

we

ansatz,

<

<

Once

consider

whether

can

completes Letting

ei(r)

of

8

have

ei(r)

/1

Q(ro) Q(ro)

The

ei(r) 4.3. < =

=

(4.3.13)

Then

show we

that

1,

sh

[(s 2

exponential

C

+

+

a

Proof

our

have

or

r 0

—h(r)

special

ei(ro)

fi(ro)

that

+

h(r)

Iei(r)

and

the

not

10_

large

is

method

2s)°

(5.2.5),

positive of

=

IQ+ei proof

=

then the =

= if e_T_

the

example.

h28Iei(ro)

enough if

-

<

r

decay

‘/IQ’(ro)I(1

i/Q’(ro)I.

((1

following

r

fi(r)t,

Ce” T .

is

does

main

of

120_

it

is

+ evaluated

large

Theorem

is

large

s) 2 e

estimate

I(Q+fi) 2 —e(Q’) 2 1 8 +IQ+fi

and

not obvious

+

theorems

Suppose enough.

/3eu)(T_T0). inequality

r enough.

work

s

E

1)]h 2 ’ + =

-

at

(0,oo) 4.1.2.

s),

that for

fi(ro)I.

e,

r

since e2

=

e2 o

=

Iãrej(r)I

L

is r 1 . >

= can

f2

Lemma

true

g(s)h 2 ’,

0 Therefore

=

to

be

0,

be

obtained

<

then

(4.3.14)

4.2.3

Ce

deter

29 )(Q+fi)

the

86 is

not

since In

So and since We

fact,

claim

hold

8

+

we

for

cx(8

that

have every

if

>

1)

cx>

Cs 8 ’h 28

<0.

r

(1

4.3.

(O,oo).

+

The

s) 2 °

s

Proof then

=

claim

h 8 >>

(s 2

CIQF(ro)j 28 E 8 + 0 _l)

g(s)

+

of

is

2s)° the

,

2

proved

Cs 9

main

>

as

+

Cs 8

s 20 )

and theorems

—*

<

consequently,

0.

>>

1

as

(4.3.14) e

‘.

0

does 87

[10]

[9] [7]

[8]

[6]

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for

Chapter

Instability

this

are

By

the

define

A

version

(x,t)

(.,)

solitary Pauli

a

chapter

nonlinear

Introduction

real

nonlinear

are

While

is

of

of

matrices:

parameter extensively

=

1

solitary

the

:

this

R 3

wave,

we

Dirac

Hermitian

by

/0

chapter

x

\o

/12

show

5

waves

shooting

or

o)’

iN

equation

and

—12)

standing —

the

studied

will

0’\ for

=

C 4 ,m>0

(x,t)

j=’

of

(x)

inner

be

instability

nonlinear

(Q)

3

‘Y

2

method

submitted

=i

k

in wave

=

product

decays

/0

Dirac solitary

=

[2,

Dirac

e_t(x) and

=

4,

[2,

we

ZN

of

o)’

for

5,

4,

as

solitary

mean

equations.

in

publication.

9—12]

10]

lxi C’.

—*

and

3

a

for

=o waves,

solution

co.

equations

k

variational

/1

a

Guan,

The

large

waves

1,2,3,

()

or

—1

0

existence

of

M.

standing

variety

the

and

method

form

Gustafson,

of

of

(5.1.2)

(5.1.1)

waves

non

such

[5], 90

suggests stability, But variation

does the below. be

that method tive metry where

Shatah is ear w

of in is

E() and near

sufficiently structed in form of the

—, ities

Gordon

e

unstable.

solitary

the R 3 .

a

positive

However We

PDEs

second

authors

Strauss

very

this (0,

eigenvalue,

the

with

the

not

that

be

form that f,

The

m).

and

left

equations

to

ground

that

g

the

method

Dirac

in

have

just

general

operator

the

such

state

waves

are

near

variation

Dirac

and

an Guan

gives

Strauss

spectrum

[9].

(5.1.2),

[7,

proved

energy

there

This

the

form

like

a

real

open

operator

8]

as

bounded

d”(w)

a

Stability

states

local

(at

this

ground

setting,

cannot

the

proved

in

equations.

kernel

Klein-Gordon,

(5.1.4).

and

issue

JI

functions,

are

also

there

functional,

L()

least

problem for

[9]

state

of

solitary

minimum

of

<0 are

=

some

nonlinear

refined

w

came

the

Dm

Dm

has

be

states

of

a

which

E”(b)

away of

=

up

exists

e

unstable

Werle

gives

general

where

1

dimension

applied

f

energy

a (m

5.1.

is

been

to

and

partial

about

wave

up

Bogolubsky

IkIdx).

solitary

the

in

(Dm)

—i

from

8 and

can

at

rise

symmetries)

infinity

with

if(r)

g(r) < if(r)cos

[161,

and

o,

Schrödinger

r,

[9]

Introduction

d(w)

extensively

orbital

the

result

if dynamics

L”(q) 2,

functional ,

be

to

L()

the

to

are

zero.

rn)

results

they

Schrodinger

or

this

Strauss sin

=

ground waves

Dirac one

Their applied

=

a

stability

with

unstable.

y 0 yJt3j

many

(‘)&,

are

(—oo,m]

solution

in

be

E() ‘Pe

stability

as

exist,

Then

in

and

[11]

the

standard

operator to

the

about

means

assumptions

for

some

(in

[1]

equations.

states.

and

studied

as

to

localized

+

the

have

to

since there

charge

sharp

instability

required

later of

the

m 0

traveling

a

which fl

Recall

and

wL().

and

Vázquez

show

ej

rest

necessary

the

the

{m,+oo).

that

only

case

The

>

the

directly.

spherical

is

is

times.

wave

for

instability

instability

related

solitary

of

application

0.

solutions

exists

a

that

not

for

any

energy

Grillakis,

one

of

continuous

the

allow

condition

nonlinear

the

These

waves

criterion

in

e

equations.

solitary

bounded

for

initial condition

=

simple

Otherwise

positivity

and

spectrum

[14]

Contrary

to

coordinates

waves

the

m—>

nonlinear

functional

of

are

condition

condition

for

the

remains

claimed

nonlin

Shatah

of

in

second

datum

(5.1.4)

(5.1.4)

(5.1.3)

Klein-

waves

of

nega

curve

every

sym

from

con

[13].

this

Let

the

for

91

to

to

of

0, it

eh/ 2 v(/gr,t),

the

In Here equations. But where

to of Q

and

Since at the

is

a nonlinear infinity

[9],

For

ground

eigenvalues

Q(x)

smooth

coupled

this Introducing

f(r,

d’(w)

we

equation

t), is

=

used

(see

states

g(r, not

and Q(IxI) II&11L2

=

Dirac

system

then

f

—L()

(

[6]

rescaling

of

I

t) positive,

-wf

a

(x)

(5.1.1),

two

d”(w)=—I(&Il 2

iaV

and

the

are

rigorous

(u,v) satisfies equations

= )

rQ+Q=Q 29 Q, new

= the -

- -

Ce

C-valued

linearized

+ the

=

—(II1I)2

t)

iOtf

(

the

°

and solve

E(0U

problem

decreases functions

=

references

(x) i(x)

the proof.

e_t

5.1.

solitary

+

perturbation

is

the

0rg

+

nonlinear

0(e),

functions.

harder

operator.

)

+

Introduction

with coupled

-

monotonically,

(u, The - -

= ll2II,2),

if(r, waves

if(r, g(r,t)

therein).

(lgI 2

v)

(E(x)

(IvI 2

nonlinearity

than

question

such

e(x)

elliptic

t) t)

-

Then

system

arguments.

In

have

IvI 2

II2II2

cos

sin 1<6<2.

(

If

then

that

as

EIuI 2 )v

that

general

I 2 )f

We

re’

1!et

—eIuI 2 )u,

equation

the

equation

if

of

of

and

f(p,

have +

=

I

0> form

mf.

nonlinear

+

stability

0(E).

the

decays

t) Let

v).

) I°&have ,

=

(5.1.1)

+

stability

we e

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t),

ansatz

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w,

517 515 g(p,

p

92 to

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verify

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io2

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series

CQ,

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linearly

asymptotics

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expansion

a

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direct

result

is

for

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the

from

linearized

Theorem

operator

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and

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[11]

[10] [9]

[8]

16]

[7] [5] [4]

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States.

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of

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nonlinear

nonlinear

472—491.

Corn

108 rest

decomposes estimates of

system potential

tion different try. solutions.

harmonic the to given proof

dinate function, dimensional butions

Compared among Landau-Lifshitz the map Lifshitz

around in maps. — This

6.1

Chapter

Conclusions

potential.

R 2

that

In

flow

“generalized

on

the

The

heat

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to

of

is

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systems”

My

the

(2.3.3)

radial

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Summary

of

to

flow

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global

analyze proved

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equations

but

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are

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2,

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need 114

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