Bifurcation for a free boundary problem modeling a small arterial plaque††
Abstract
Atherosclerosis, hardening of the arteries, originates from small plaque in the arteries; it is a major cause of disability and premature death in the United States and worldwide. In this paper, we study the bifurcation of a highly nonlinear and highly coupled PDE model describing the growth of arterial plaque in the early stage of atherosclerosis. The model involves LDL and HDL cholesterols, macrophage cells, and foam cells, with the interface separating the plaque and blood flow regions being a free boundary. We establish finite branches of symmetry-breaking stationary solutions which bifurcate from the radially symmetric solution. Since plaque in reality is unlikely to be strictly radially symmetric, our result would be useful to explain the asymmetric shapes of plaque.
keywords:
free boundary problem, atherosclerosis, bifurcation, symmetry-breaking.1 Introduction
Atherosclerosis, known as an inflammatory disease, is a major cause of disability and premature death in the United States and worldwide. It occurs when fat, cholestrol, and other substances build up in and on the artery walls. These deposits are called plaques, which harden and narrow the arteries over time. The plaque can rupture, triggering a blood clot which restricts blood flow. During this process, a heart attack, stroke, or sudden cardiac death may occur. Every year about 735,000 Americans have a heart attack, and about 610,000 people die of heart diseases in the United States — that is 1 in every 4 deaths (cf.,[1, 22]).
There are several mathematical models that describe the growth of plaque in the arteries (see [2, 3, 8, 9, 13, 18, 19]). All of these models recognize the critical role of the “bad” cholesterols, low density lipoprotein (LDL), and the “good” cholesterols, high density lipoprotein (HDL), in determining whether plaque will grow or shrink. Recently, a free boundary PDE model was proposed in [13], in which a risk-map was generated for any pair values of (LDL, HDL), showing the important influence of LDL and HDL on plaque formation. Later, on the foundation of the model, Hao and Friedman added the impact of reverse cholesterol transport (RCT) in [8]. In addition, the existence of a small radially symmetric stationary plaque and its stability condition were theoretically established for a simplified free boundary model in [9]. Nevertheless, there is no theoretical work to analyze the bifurcation of plaque model. As the plaque in reality is unlikely to be radially symmetric, it is necessary to investigate the non-radially symmetric solutions. Hence in this paper we shall carry out the bifurcation for the plaque model proposed in [9] (also see [7, Chapters 7 and 8]).

The process of plaque formation is as follows: when a lesion develops in the inner surface of the arterial wall, it enables LDL and HDL to move into the intima and become oxidized by free radicals. Oxidized LDL triggers endothelial cells to secrete chemoattractant proteins that attract macrophage cells (M) from the blood. Macrophage cells can engulf oxidized LDL, they then become foam cells (F), and the accumulation of foam cells results in the formation of plaque. The effect of oxidized LDL on plaque growth can be reduced by the good cholesterols, HDL: HDL can remove harmful bad cholesterol out from the foam cells and revert foam cells back into macrophage cells; moreover, HDL also competes with LDL on free radicals, decreasing the amount of radicals that are available to oxidize LDL. In the model, we let
Assuming the artery is a very long circular cylinder with radius 1 (after normalization), we consider a circular cross section of the artery. As can be seen in Fig. 1, the cross section is divided into two regions: blood flow region and plaque region , with a moving boundary separating these two regions (since plaque can either grow or shrink). The variables satisfy the following equations in the plaque region (cf., [7, Chapters 7 and 8] and [9]):
(1.1) | |||
(1.2) | |||
(1.3) | |||
(1.4) |
where , , and denote the natural death rate of , , , and , respectively. In equations 1.1 — 1.4, the aforementioned transitions between macrophage cells () and foam cells () are included: accounts for the fact that becomes foam cell by combining with , describes the removal of foam cell by , and the extra term in equation 1.3 models the effects that oxidized attracts while decreases this impact by competing for free radicals.
We assume that the density of cells in the plaque is approximately a constant, and take
(1.5) |
Since there are cells migrating into and out of the plaque, the total number of cells keeps changing and, under the assumption 1.5, cells are continuously “pushing” each other. This gives rise to an internal pressure among the cells which is associated with the velocity in 1.3 and 1.4. We further assume that the plaque texture is of a porous medium type, and invoke Darcy’s law
(1.6) |
where is the internal pressure relative to the outside pressure (and therefore can admit positive or negative sign). Combining 1.3 – 1.6, we derive
(1.7) |
Due to the assumption 1.5, we can decrease the number of equations by 1, and replace by in 1.1 – 1.4, hence we shall have 4 PDEs, for , , and , respectively. In particular, combining with 1.7, we write the equation for in the following form
(1.8) |
We now turn to the boundary conditions. We assume no flux condition on the blood vessel wall () for all variables (no exchange through the blood vessel):
(1.9) |
while on the free boundary , we take
(1.10) | |||||
(1.11) | |||||
(1.12) | |||||
(1.13) |
where is the outward unit normal for which points inward towards the blood region (as shown in Fig. 1), and is the corresponding mean curvature in the direction of (i.e., if ). The cell-to-cell adhesiveness constant in front of is normalized to 1. The flux boundary conditions 1.10 and 1.11 are based on the fact that the concentrations of and in the blood are and , respectively; and the meaning of 1.12 is similar: there are, of course, no foam cells in the blood.
Furthermore, we assume that the velocity is continuous up to the boundary, so that the free boundary moves in the outward normal direction with velocity ; based on 1.6, the normal velocity of the free boundary is defined by
(1.14) |
In [9], Friedman et al. analyzed the system 1.1 – 1.14 in the radially symmetric case and established the existence of a unique radially symmetric steady state solution in a ring-region with being small. It is, however, unreasonable to assume plaque is of strictly radially symmetric shape, hence we’d like to investigate the symmetric-breaking bifurcation for the system. To do that, we study the corresponding stationary problem of 1.1 – 1.14:
(1.15) | |||||
(1.16) | |||||
(1.17) | |||||
(1.18) | |||||
(1.19) | |||||
(1.20) | |||||
(1.21) | |||||
(1.22) |
In recent years, considerable research works have been carried out on bifurcation analysis for various tumor growth models (see [5, 6, 10, 11, 15, 14, 16, 17, 20, 23, 24, 25, 27, 21]), where the Crandall-Rabinowitz theorem (will be mentioned in Section 2) is a primary tool. Compared with tumor growth models, our system 1.15 – 1.22 contains more equations which are highly nonlinear and coupled together, therefore it is a formidable task to analyze our model. Besides, the absence of an explicit stationary solution presents a big challenge to verify the Crandall-Rabinowitz theorem. Even though the problems in [26, 27] do not admit explicit representations, the structure of the problem studied here is very different. To overcome it, we establish a lot of sharp estimates in Section 4. To the best of our knowledge, this is the first paper on the study of bifurcation for the system 1.1 – 1.14. Our main result is stated as follows:
For convenience we shall use as our bifurcation parameter. We will keep all parameters fixed except and , and vary by changing .
Theorem 1.1.
Remark 1.1.
Unlike tumor protrusions which are usually unstable and may cause metastases, the protrusions of plaques are towards the blood region with limited spatial freedom. As gets bigger, becomes negative with larger absolute value. By the definition of , this means that the concentration of the good cholesterol (HDL) must be substantially larger than the concentration of the bad cholesterol (LDL) for the bifurcation to occur. The more protrusions, the larger over will be required to balance the protrusion forces. Based on the stability results from [9], it is likely to have some stable bifurcation branches.
The structure of this paper is as follows. In Section 2, we give some preliminaries; in section 3, we rigorously justify some expansions which will be needed in applying the Crandall-Rabinowitz theorem; and then we carry out our proof of Theorem 1.1 in Section 4. Some well-known results are collected in the Appendix.
2 Radially symmetric stationary solution
2.1 A small radially symmetric stationary solution
We consider a radially symmetric stationary solution in a small ring-region , and denote the solution by . Based on 1.15 – 1.22, the solution satisfies
(2.1) | |||||
(2.2) | |||||
(2.3) | |||||
(2.4) | |||||
(2.5) | |||||
(2.6) | |||||
(2.7) | |||||
(2.8) |
Viewing as , and following Theorem 3.1 in [9], for every and small, we can find a unique and a constant , such that there is a unique classical solution to the above system with . The existence theorem for radially symmetric solution of this form, however, is not good enough for the bifurcation theorem.
There are many parameters in our system. We need to choose one as the bifurcation parameter. We let to be our bifurcation parameter. We can vary by, say, keeping and fixed while changing only. For simplicity, we shall assume all the parameters are fixed and of order except and . With these settings, varying corresponds to varying . In the rest of this paper, we shall thus use and as our parameters.
Here is our existence theorem for the radially symmetric solutions. We define
(2.9) |
Theorem 2.2.
Proof.
The proof is similar to that in [9] but much more involved. Following Lemma 3.1 of [9], for all parameters of order , the system 2.1 – 2.7 admits a unique solution for small . In order for this solution to be the solution of our problem, we need to verify 2.8. We shall do so by keeping all parameters fixed except .
Note that 2.8 is equivalent to
(2.10) |
As in [9, (3.29)–(3.32)], recalling also (see Appendix 5.1) (the formulas in [9, (3.23)–(3.25), (3.26)–(3.28), (3.29)] are all missing minus signs; as a result, the corrected [9, (3.29)] should read:
([9,(3.29)]) |
and [9, (3.30),(3.31)] should be corrected in a similar manner; this correction does not change the proof in [9]), we can establish the following:
(2.12) | |||||
Substituting these expressions into the formula 2.10 for , we find that the terms in the bracket cancel out, and
(2.14) |
A direct computation shows that
(2.15) |
It follows that, for small , and for large , hence there must be a value of on which .
To finish the proof, it suffices to show ; the proof is similar to that of [9, Theorem 3.1] in the second part, but is actually a little easier. ∎
Remark 2.1.
By ODE theories, the solution can be extended to the bigger region while maintaining regularity. For notational convenience, we still use to denote the extended solution.
Remark 2.2.
The case is certainly true within reasonable parameter range.
Following the above proof, we also derive
Lemma 2.3.
Let . Then
(2.16) | |||||
(2.17) |
Remark 2.3.
The following estimates are useful later on:
Lemma 2.4.
The following estimate holds for first derivatives,
(2.18) |
2.2 The Crandall-Rabinowitz theorem
Next we state a useful theorem which is critical in studying bifurcations.
Theorem 2.5.
(Crandall-Rabinowitz theorem, [4]) Let , be real Banach spaces and a map, , of a neighborhood in into . Suppose
-
(1)
for all in a neighborhood of ,
-
(2)
is one dimensional space, spanned by ,
-
(3)
has codimension 1,
-
(4)
.
Then is a bifurcation point of the equation in the following sense: In a neighborhood of the set of solutions consists of two smooth curves and which intersect only at the point ; is the curve and can be parameterized as follows:
3 Bifurcations - preparations
Let’s consider a family of perturbed domains and denote the corresponding inner boundary to be , where , and . Let be the solution of
(3.1) | |||||
(3.2) | |||||
(3.3) | |||||
(3.4) | |||||
(3.5) | |||||
(3.6) | |||||
(3.7) |
The existence and uniqueness of such a solution is guaranteed by the following lemma.
Lemma 3.6.
Proof.
We shall use the contraction mapping principle to prove this lemma. Let
(3.8) |
Step 1. For each , we define a map as follows: we first solve and from the elliptic equations
with the boundary conditions
By the maximum principle, we clearly have
(3.9) |
We then define by the solution of the system
(3.10) | |||
(3.11) |
Since are all bounded, the right-hand side of 3.10 is bounded under supremum norm, i.e.,
(3.12) |
Also, we use the mean-curvature formula, i.e.,
(3.13) |
to derive that
(3.14) |
By the maximum principle,
(3.15) |
where is defined in Appendix 5.1. Next we are going to estimate and show that it is actually independent of and . To do that, we shall use the Schauder estimates; but before using the Schauder estimates directly, let’s apply the following transformation:
and denote . Clearly, maps to a long stripe region . Based on the calculations from Appendix 5.2, satisfies
where coefficients , are bounded, and is also bounded based on 3.8. Applying the interior sub-Schauder estimates (Theorem 8.32, [12]) on the region , recalling also 3.14, we obtain
where is independent of and . We use a series of sets to cover the whole region , as a result,
We then relate with to derive
and hence
(3.16) |
where is independent of and .
Finally, recalling equation 3.3, we define as the solution to the equation
(3.17) |
with the boundary conditions
(3.18) |
By the maximum principle, and, using this result, we employ the maximum principle again to derive the inequality All together, these two inequalities indicate
(3.19) |
In the next step, we claim that this bound for can be improved. By 3.8 and 3.19, the right-hand side of equation 3.17 is bounded; assume the bound is constant . According to Appendix 5.1, can be a supersolution for , hence the maximum principle leads to
(3.20) |
After we show this, we can employ the sub-Schauder estimates on 3.17 – 3.18 in a similar way as we did for to obtain
(3.21) |
where is a constant which does not depend upon and .
Above, we have shown that , which means maps into itself. We shall next prove that is a contraction.
Step 2. Suppose that for , and set
Based on our definitions of , , , in the first step and recalling 3.16 as well as 3.21, we derive, for some constant ,
Next we shall use the maximum principle to derive bounds for , , and . To do that, we use the function defined in Appendix 5.1. As a result,
where both and are independent of and . The above inequalities imply that
hence we obtain a contraction mapping by taking sufficiently small and so that
The unique fixed point of the contraction mapping is the unique classical solution to the system 3.1 – 3.7. ∎
With being uniquely determined in the system 3.1 – 3.7, we define by
(3.22) |
where is our bifurcation parameter. We know that is a symmetry-breaking stationary solution if and only if .
In order to apply the Crandall-Rabinowitz theorem, we need to compute the Fréchet derivatives of . For a fixed small , we formally write as
(3.23) | |||
(3.24) | |||
(3.25) | |||
(3.26) |
In the following, we shall first justify 3.23 – 3.26. The structure of the proofs is similar to that in [5, 16, 17, 20, 23, 27]. However, our problem is much more involved since the system 3.1 – 3.7 is highly nonlinear and coupled, hence we shall use very delicate estimates and the continuation lemma (see Appendix 5.3) to tackle the problem.
3.1 First-order estimates
Lemma 3.7.
Fix sufficiently small, if and , then we have
where is independent of and .
Proof.
We combine 2.1 – 2.7 and 3.1 – 3.7 to obtain the equations for , , and . For example, we have
where and are both bounded since , , and based on Lemma 3.6 and Lemma 3.1 in [9]. In addition, the boundary conditions for are
Since are all bounded and by 2.18, we know from the equation 2.1 that is bounded with a bounded independent of and . Hence we can find a constant, we denote it by , which does not depend upon and , such that
(3.28) |
Similarly, we can write the equations of , and as
(3.29) | |||||
(3.30) | |||||
(3.31) |
where , are all bounded, and it is shown earlier that and are bounded; for simplicity, we shall use the same constant to control and , namely,
(3.32) |
Furthermore, the boundary conditions for , and satisfy
(3.33) | |||
(3.34) | |||
(3.35) | |||
(3.36) |
where the last inequality is based on the formula of in 3.13.
Since the system is highyly coupled, it is not an easy job to prove the estimates in Lemma 3.7. To show that, we use the idea of continuation (Appendix 5.3). We multiply the right-hand sides of 3.1 – 3.31 by with , and we shall combine the proofs for the case as well as the case .
We first assume that, in the case , for some to be determined later on
(3.37) | |||
(3.38) | |||
(3.39) |
where is from 3.28, 3.32, 3.34–3.36, and is a scaling factor which comes from applying the Schauder estimate as we did in Lemma 3.6; both and are independent of and .
Let’s first show 3.39. Based on 3.37, for the case , the right-hand side of 3.31 is bounded, i.e.,
(3.40) |
notice that the above estimates is automatically valid in the case without the assumptions 3.37 since the right-hand side is zero. Let
(3.41) |
then
and
where , again, comes from 3.28, 3.32, 3.34–3.36. Notice that , and we use the smallness of to majorize the right-hand side of 3.40 for a supersolution for when is small and , hence
Using a scaling argument as in 3.16, we further have
(3.42) |
In the next step, let’s consider and . It follows from the assumption 3.37 that
(3.43) |
where is some universal constant. Recalling also 3.32 and 3.42, we have the following estimate for ,
(3.44) | ||||
We use
(3.45) |
as the supersolution with given by
(3.46) |
Taking derivatives of gives us
It is clear that . Moreover, for the boundary condition at ,
Since and for , we have, for and small,
Then
Next we consider the equations 3.1, 3.29, 3.30 in proving is a supersolution. Notice that
For 3.43, it is clear that since the leading order term in is and we can take small. Hence is a supersolution for as well as for . For 3.44, as is shown, the leading order term in bounding 3.44 is ; on the other hand,
the extra term is of order and therefore does not cause a problem. Thus is also a supersolution for .
From the above analysis, we see that the choice of and depends only on , , and , and is therefore independent of and . By the maximum principle,
Using a scaling argument, we further have
These estimates are valid in the case without the assumptions 3.37–3.39 since the right-hand sides are all zero in this case. Conditions (i) and (ii) of Lemma 5.20 are therefore satisfied for the vectors . Since condition (iii) is obvious, we finish the proof. ∎
Remark 3.1.
Based on Lemma 3.7, if we further apply the Schauder estimates on the equations for , , , and , we can actually obtain
where is independent of , but is dependent upon .
3.2 Computation of , , and
In general, if (, ) is a function with bounded second order derivatives, then we have the Taylor’s expansion:
(3.47) |
where the remainder , given by satisfies
(3.48) |
Thus we have:
Lemma 3.8.
Suppose is a linear operator, , . Let be the linearized solution, i.e., . Then
(3.49) |
where by 3.47,
(3.50) |
Later on we shall apply this formula with and . Notice that by Lemma 3.7, , thus we already have . In what follows, we only need to produce correction terms for the linear part of the system, i.e., we shall compute the functions for , , and . Substituting 3.23 – 3.26 into 3.1 – 3.7, and dropping higher order terms of , we obtain the linearized system. This is equivalent to taking total differential of the right-hand side with respect to and . If we write , then, from 1.15, , so that
and this is the right-hand side of the equation for . Similar equations are derived for and . The right-hand side for is similar, but we have to take care of the additional gradient terms in the left-hand side. In summary, we obtain the following linearized system on :
(3.51) | |||||
(3.52) | |||||
(3.53) | |||||
(3.54) | |||||
(3.55) | |||||
(3.56) | |||||
(3.57) | |||||
(3.58) | |||||
(3.59) |
Using the same techniques as in the proof of Lemma 3.7, also recalling Remark 3.1, we can derive and ; their Schauder estimates may depend on , but it is crucial that the estimates are independent of and .
Notice that , , and are all defined in , while , , and are defined in . We would now like to transform , , and from to so that we are able to work on the same domain to derive second-order estimates. To do that, we define a transform
(3.60) |
and let
(3.61) | |||||
(3.62) |
for . Similar as using the Hanzawa transformation in [5, 16, 17, 20, 23, 27], the error incurred from applying is less than .
3.3 Second-order estimates
The first step in deriving second-order estimates is to calculate the equations for , , and . Here we shall only show the derivations of the equation for , since the equation for is more complex than those for other variables.
Combining the equations for and respectively in 2.3 3.3 and 3.53, we derive
(3.63) |
By Lemma 3.8, the right-hand side of 3.63 satisfies
where I is written as, for bounded functions and ,
and II is bounded by , hence
We then turn to the left-hand side of equation 3.63. The terms involving the gradients can be rearranged as
By Lemma 3.7,
(3.64) |
furthermore, we can derive from 3.54 and 3.59 that
as ; using the same technique as in Lemma 3.6, we shall get
hence
for a constant which is independent of and . Together with 3.64, we derive
From the above analysis, we obtain the equation for ,
Now we recall the transform in 3.60 and the change of variables in 3.61 and 3.62, we can derive the equation for , namely,
(3.65) | ||||
where is generated by the tiny changing of domain from to in applying the transformation , and it contains at most second derivatives of , hence
Combining with the estimates we derived before, we have
Notice that the above inequality present similar structure as 3.44, hence we can use the same technique and similar supersolutions to establish
Lemma 3.9.
Fix sufficiently small, if and , then we have
where is independent of and .
Following Remark 3.1, we shall further have
Lemma 3.10.
Fix sufficiently small, if and , then
(3.66) | |||
(3.67) | |||
(3.68) | |||
(3.69) |
where is independent of , but is dependent on .
3.4 Fréchet derivative
Introduce the Banach spaces
(3.70) |
It can be easily proved that the system 3.1 – 3.7 is even in variable if we assume . Together with 3.69, we know that the mapping is bounded when , and the same argument can show that it is also true for any . In order to apply the Crandall-Rabinowitz theorem, we need to verify the continuous differentiability of . As will be shown in the following lemma, the differentiablity is eventually reduced to the regularity of the corresponding PDEs, and explicit formula is not needed if we are only interested in differentiability; therefore a similar argument shows that this mapping is Fréchet differentiable in ; furthermore (or ) is obtained by solving a linearized problem about with respect to (or ). By using the Schauder estimates we can then further obtain differentiability of to any order.
We now proceed to compute those Fréchet derivatives that are crucial in applying the Crandall-Rabinowitz theorem.
Lemma 3.11.
The Fréchet derivatives of at the point are given by
(3.71) | |||
(3.72) |
4 Bifurcations - Proof of Theorem 1.1
In this section, we shall employ the explicit expression of the Fréchet derivative 3.71 to verify the four conditions in the Crandall-Rabinowitz theorem and complete the proof of Theorem 1.1. Unlike [5, 6, 11, 10, 16, 17, 20, 23, 24, 25], we cannot solve and explicitly, since our model is highly nonlinear and coupled. To meet the challenges, we need to derive various sharp estimates on and .
Throughout the rest of this paper, is used to represent a generic constant independent of , which might change from line to line.
4.1 Estimates for
In order to estimate in 3.71, we start with evaluating 2.4 at and substituting the boundary condition 2.8, hence we obtain
(4.1) |
Similar to the proof of Theorem 2.2, we substitute 2.1 – 2.1 into the above formula and combine with 2.16, we find that both and terms cancel out, thus
(4.2) |
Denote
(4.3) |
it follows from 4.2 that is bounded. Besides, we claim that is also bounded. To prove it, we take derivative of equation 4.2, and derive
By substituting the formula of in 2.17, we find that the terms in the above equation cancel out, hence
To sum up, the properties of are listed in the following lemma:
Lemma 4.12.
For function defined in 4.3, there exists a constant which is independent of such that
(4.4) |
4.2 Estimates for
Set the perturbation
as the set is clearly a basis for the Banach space defined in 3.70. Since the solution to 3.51 – 3.59 is unique, we know if we can find a solution of the form
(4.5) | |||||
(4.6) |
then it is the unique solution of 3.51 – 3.59. Substituting 4.5 and 4.6 into 3.51 – 3.59, we need to find satisfying
(4.7) | |||||
(4.8) | |||||
(4.9) | |||||
(4.10) | |||||
(4.11) | |||||
(4.12) | |||||
(4.13) | |||||
(4.14) | |||||
(4.15) |
where by 3.51 – 3.54, , , , and can all be bounded by linear functions of , , and . In particular, is expressed as
(4.16) |
which will be used later.
Denote the operator . For this special operator, one can easily verify the following lemmas.
Lemma 4.13.
The general solution of ( is a constant)
(4.17) | |||
(4.18) |
is given by
(4.21) |
where
(4.25) |
and
(4.28) |
The special solution satisfies
(4.29) |
and
(4.30) |
Proof.
Lemma 4.14.
Lemma 4.15.
For and ,
(4.35) |
Proof.
The function satisfies and for , so that for .
Similarly, the function satisfies and for , so that for . ∎
In order to make the boundary conditions 4.45 – 4.47 homogeneous, let’s instead work with
(4.36) | |||
(4.37) | |||
(4.38) |
Accordingly, , , satisfy the following equations:
(4.39) | |||||
(4.40) | |||||
(4.43) | |||||
(4.44) | |||||
(4.45) | |||||
(4.46) | |||||
(4.47) |
Lemma 4.16.
For sufficiently small , there exist a constant which does not depend on and such that the following inequalities are valid for the above system,
(4.48) | |||
(4.49) |
Proof.
To prove 4.48 and 4.49, we again use the idea of continuation (Appendix 5.3), and multiply the right-hand sides of 4.39 – 4.43 as well as 4.10 by . When , it follows from the maximum principle that , hence 4.48 clearly holds in this case. Furthermore, it can be solved from
(4.50) | |||
(4.51) |
that
and hence for ,
Next we consider the case when . We first assume that
(4.52) | |||
(4.53) |
Then clearly , and is a supersolution for when . It follows that, by Lemma 4.13,
The case when can be easily proved. Similarly, we have . Next let’s prove the estimate for . Under our assumptions, by 2.18, 4.52, and 4.53,
so that, we can use 4.29 to derive
The function satisfies,
for , where we also make use of 2.18 in deriving the above estimate. Therefore, it follows from the maximum principle that
Finally, in order to estimate , we use the explicit formula from Lemma 4.13. Taking and , we obtain from Lemma 4.13 that
(4.54) |
where and are defined in Lemma 4.14. By 4.52,
and together with 4.29 in Lemma 4.13, we have
(4.55) |
Combining 4.54 with 4.32 4.33 and 4.55, we then obtain
hence is valid for sufficiently small . ∎
Based on 4.48 and 4.49, the existence and uniqueness of such a solution to the system 4.7 – 4.15 can be justified through the contraction mapping principle, hence we have the following lemma.
Lemma 4.17.
By 4.49 we already derived the estimate
This estimate, however, is not enough; we need a sharper bound for . To do that, we start with rewriting 4.36 – 4.38 in the same way as in 2.1 – 2.1.
Evaluating 2.1 at , and using 2.1 – 2.1, we obtain
Recall that the boundary condition for is
We combine the above two equations to derive
Similarly, we can also get
Comparing with the definitions of , and in 2.1 – 2.1, we find that
Therefore, the above equations indicate
(4.56) | |||
(4.57) | |||
(4.58) |
After we show 4.56 – 4.58, we can combine them with 4.36 – 4.38 as well as 4.48 to claim that
(4.59) | |||||
(4.60) | |||||
(4.61) |
With 4.59 – 4.61, we are able to derive a more delicate estimate for . Substituting 2.1 – 2.1 and 4.59 – 4.61 all into 4.16, recalling also 2.15 and 2.16, we obtain
(4.62) |
and we are ready to establish the following lemma.
Lemma 4.18.
For each nonnegative and small , the following inequality holds:
(4.63) |
where , and the constant is independent of and .
Proof.
The estimate 4.63 shall be established by using the explicit formula from Lemma 4.13. Specifically, we take and . From 4.62, we have
we then combine it with Lemma 4.13 to derive
(4.64) |
Following Lemmas 4.13 and 4.14, we can explicitly solve as
For , we use 4.25 and Lemma 4.15 to obtain
and
(4.65) |
Together with 4.32 4.33 as well as 4.64 the first derivative of at evaluates to
which is equivalent to 4.63. It is clear from 4.65 that the above formula is also valid for . ∎
Like in 4.3, we denote
(4.66) |
which indicates
(4.67) |
From Lemma 4.18, we immediately obtain that there exists a constant which is independent of and such that
In addition, we also need to estimate . To do that, we take derivative of equation 4.67 to obtain
(4.68) |
In order to estimate the right-hand side of 4.68, we differentiate the whole system 4.7 – 4.15 in and follow the same procedures as in Lemmas 4.16 and 4.18. Consequently, a similar result as 4.63 can be obtained, i.e.,
Combined with 4.68, it follows that . Therefore we have the following lemma.
Lemma 4.19.
For function defined in 4.66, there exists a constant which is independent of and such that
(4.69) |
At this point, we are finally ready to prove our main result Theorem 1.1.
Proof of Theorem 1.1.
Substituting 4.6 into 3.71, we obtain the Fréchet derivative of in at the point , namely,
we then combine the above formula with 4.3 and 4.67 to derive
(4.70) |
For fixed nonnegative ,
when is sufficiently small so that . In this case, the equation is satisfied if and only if
(4.71) |
Notice that both and contain , it is impossible to solve explicitly from equation 4.71. However, we are able to claim that for each small , 4.71 admits a unique solution . To prove it, we first find that ; in addition, if we take partial derivative on both sides of 4.71 and evaluate the value at , we have
Therefore, it follows from the implicit function theorem that, for each small , there exists a unique solution, which is close to , such that equation 4.71 is satisfied; we denote the unique solution by . In what follows, we shall justify that with and is a bifurcation point for the system 1.15 – 1.22 when is sufficiently small.
What we need to do is to verify the four assumptions of the Crandall-Rabinowitz theorem (Theorem 2.5) at the point . To begin with, the assumption (1) is naturally satisfied due to Theorem 2.2. To be more specific, for each , we can find a small , such that for , there exists a unique radially symmetric stationary solution, hence . Next let’s proceed to verify the assumption (2) and (3) for a fixed small . It suffices to show that for every , ,
(4.72) |
or equivalently,
(4.73) |
To establish statement 4.72 (or statement 4.73), we split the proof into three cases:
Case (i) and , where will be determined later. Using the inequality , together with Lemma 4.15, we deduce that
hence (recall that so that in this case)
(4.74) |
In addition, by Lemma 4.12 and Lemma 4.19, there exists a constant which does not depend on and such that,
(4.75) |
Substituting 4.74 and 4.75 into 4.73, we derive
It is clear that for large as the leading order term in the brackets is ; hence we can find such that when ,
Case (ii) and . In this case, we have
and hence (since , we also have in this case)
Similar as in Case (i), we substitute the above inequality as well as 4.75 into 4.73, and derive
notice that the leading order term is , we can easily find a bound for , denoted by , such that when ,
Case (iii) . From our previous analysis, we know that is close to . Since is a finite number, we can choose small and similarly define all for so that is close to ; in this case if and only if . To be more specific, we have
Since and , it follows that
(4.76) | ||||
Recall again is bounded in this case, we can find a bound for , denoted by , such that when ,
together with 4.76, we obtain
By combining all three cases, the assumptions (2) and (3) in Theorem 2.5 are satisfied when is sufficiently small, i.e.,
such that the spaces listed here (codimension space, non-tangential space) meet the requirements of the Crandall-Rabinowitz Theorem. To finish the whole proof, it remains to show the last assumption. Differentiating 4.70 in , we derive
(4.77) | ||||
By Lemma 4.12 and Lemma 4.19, there exists a constant independent of and such that
(4.78) |
Based on 4.78, we can find a bound (depending on ), such that when ,
and hence , i.e., the assumption (4) is satisfied.
Combining all pieces together, we take , then we know that all the assumptions of the Crandall-Rabinowitz theorem are satisfied when . Hence we conclude that is a symmetry-breaking bifurcation point. ∎
5 Appendix
5.1 A supersolution
5.2 Transformation
The transformation
maps to a long stripe region . Let satisfies
(5.2) |
and set . Obviously, should be -periodic in . Using the chain rule, we obtain:
Hence we can write the equation of as
where , and are thus bounded. Furthermore, since contain at most first derivative of , they are if .
5.3 A continuation lemma
The next lemma concerns the continuation of estimates. The proof is standard and we omit the details.
Lemma 5.20.
Let be a finite collection of real vectors, and define the norm of the vector by . Suppose that , and
(i) ;
(ii) For any , if , then ;
(iii) is continuous in .
Then for all .
Remark 5.1.
If the finite collection is replaced by an infinite collection, then (iii) will need to be replaced by “uniform continuity” in .
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