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6. Perturbation to Calabi-Yau metrics on the neck [054R]

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6. Perturbation to Calabi-Yau metrics on the neck

In Section 4.1 we have constructed a family of C2,Ξ±C^{2,\alpha}-KΓ€hler structures (Ο‰T,Ξ©T)(\omega_{T},\Omega_{T}) on β„³T\mathcal{M}_{T} with weighted error estimate by Proposition 4.23. Our goal in this Section is to perturb Ο‰T\omega_{T} to a genuine Calabi-Yau metric for TT sufficiently large. This amounts to applying the quantitative implicit function theorem (Lemma 6.1). The main result is Theorem 6.3. In Section 6.4 we also compute the measured Gromov-Hausdorff limit of these metrics at an appropriate scale. As mentioned in the Introduction, it is the proof, but not Theorem 1.1 itself, that will be immediately used in the proof of Theorem 1.1.

6.1. Framework of perturbation

The studies and applications of the implicit function theorem have been well developed in various contexts. We refer the readers to the book [KP13] for seeing the comprehensive discussions and the history of the whole methodology. For our practical and specific applications, we need the following quantitative version of implicit function theorem (Lemma 6.1), which is based on Banach contraction mapping principle.

To avoid confusions, we clarify several notations as follows:

  • β€’

    Let β„’:𝔄→𝔅\mathscr{L}:\mathfrak{A}\to\mathfrak{B} be a bounded linear operator between normed linear spaces 𝔄\mathfrak{A} and 𝔅\mathfrak{B}, then the operator norm of β„’\mathscr{L} is defined by

    (6.1) βˆ₯β„’βˆ₯o​p≑inf{M0βˆˆβ„+|βˆ₯β„’(𝒗)βˆ₯𝔅≀M0β‹…βˆ₯𝒗βˆ₯𝔄,βˆ€π’—βˆˆπ”„}.\|\mathscr{L}\|_{op}\equiv\inf\Big\{M_{0}\in\mathbb{R}_{+}\Big|\ \|\mathscr{L}(\bm{v})\|_{\mathfrak{B}}\leq M_{0}\cdot\|\bm{v}\|_{\mathfrak{A}},\ \forall\bm{v}\in\mathfrak{A}\Big\}.
  • β€’

    We use the common notation 𝟎\bm{0} for the zero vector in every normed linear space.

Lemma 6.1 (Implicit function theorem).

Let β„±:𝔄→𝔅\mathscr{F}:\mathfrak{A}\to\mathfrak{B} be a map between two Banach spaces such that for all π―βˆˆπ”„\bm{v}\in\mathfrak{A},

(6.2) ℱ⁑(𝒗)βˆ’β„±β‘(𝟎)=ℒ⁑(𝒗)+𝒩⁑(𝒗),\mathscr{F}(\bm{v})-\mathscr{F}(\bm{0})=\mathscr{L}(\bm{v})+\mathscr{N}(\bm{v}),

where the operator β„’:𝔄→𝔅\mathscr{L}:\mathfrak{A}\to\mathfrak{B} is linear and the operator 𝒩:𝔄→𝔅\mathscr{N}:\mathfrak{A}\to\mathfrak{B} satisfies 𝒩⁑(𝟎)=𝟎\mathscr{N}(\bm{0})=\bm{0}. Additionally we assume the following properties:

  1. (1)

    (Bounded inverse) β„’:𝔄→𝔅\mathscr{L}:\mathfrak{A}\to\mathfrak{B} is an isomorphism and there is some constant CL>0C_{L}>0 such that

    (6.3) β€–β„’βˆ’1β€–o​p≀CL,\|\mathscr{L}^{-1}\|_{op}\leq C_{L},

    where β„’βˆ’1\mathscr{L}^{-1} is the inverse of β„’\mathscr{L}.

  2. (2)

    There exists a constant CN>0C_{N}>0 and there is some r0∈(0,12​CL​CN)r_{0}\in(0,\frac{1}{2C_{L}C_{N}}) satisfying the following:

    1. (a)

      (Controlled nonlinear error) for all 𝒗1,𝒗2∈Br0​(𝟎)Β―βŠ‚π”„\bm{v}_{1},\bm{v}_{2}\in\overline{B_{r_{0}}(\bm{0})}\subset\mathfrak{A},

      (6.4) ‖𝒩⁑(𝒗1)βˆ’π’©β‘(𝒗2)‖𝔅≀CNβ‹…r0⋅‖𝒗1βˆ’π’—2‖𝔄.\|\mathscr{N}(\bm{v}_{1})-\mathscr{N}(\bm{v}_{2})\|_{\mathfrak{B}}\leq C_{N}\cdot r_{0}\cdot\|\bm{v}_{1}-\bm{v}_{2}\|_{\mathfrak{A}}.
    2. (b)

      (Controlled initial error) ℱ⁑(𝟎)\mathscr{F}(\bm{0}) is effectively controlled as follows,

      (6.5) ‖ℱ⁑(𝟎)‖𝔅≀r04​CL.\|\mathscr{F}(\bm{0})\|_{\mathfrak{B}}\leq\frac{r_{0}}{4C_{L}}.

Then the equation ℱ⁑(𝐱)=𝟎\mathscr{F}(\bm{x})=\bm{0} has a unique solution 𝐱∈Br0​(𝟎)\bm{x}\in B_{r_{0}}(\bm{0}) with the estimate

(6.6) ‖𝒙‖𝔄≀2​CL⋅‖ℱ⁑(𝟎)‖𝔅.\|\bm{x}\|_{\mathfrak{A}}\leq 2C_{L}\cdot\|\mathscr{F}(\bm{0})\|_{\mathfrak{B}}.
Remark 6.1.1.

In our applications, the constants CL>0C_{L}>0, CN>0C_{N}>0 and r0>0r_{0}>0 will be fixed as uniform constants (independent of T≫1T\gg 1). We will see this from the global linear and nonlinear estimates, which will be stated and proved in next subsections. With the specified weight parameters Ξ΄,ΞΌ,Ξ½\delta,\mu,\nu, the error estimate in Proposition 4.23 in fact guarantees β€–ErrC​Y‖𝔅→0\|\mathrm{Err}_{CY}\|_{\mathfrak{B}}\to 0 as Tβ†’βˆžT\to\infty, which particularly implies ‖ℱ⁑(𝟎)‖𝔅→0\|\mathscr{F}(\bm{0})\|_{\mathfrak{B}}\to 0 and hence β„±\mathscr{F} satisfies (b) of Item (2) in the above lemma.

To set up the perturbation problem in our setting, we define the Banach spaces

𝔖1\displaystyle\mathfrak{S}_{1} ≑{βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•βˆˆΞ©1,1​(β„³T)|Ο•βˆˆC2,α​(β„³T)​is​S1​-invariant and satisfiesβ€‹βˆ‚Ο•βˆ‚n|βˆ‚β„³T=0},\displaystyle\equiv\Big\{\sqrt{-1}\partial\bar{\partial}\phi\in\Omega^{1,1}(\mathcal{M}_{T})\Big|\phi\in C^{2,\alpha}(\mathcal{M}_{T})\ \text{is}\ S^{1}\text{-invariant and satisfies}\ \frac{\partial\phi}{\partial n}\Big|_{\partial\mathcal{M}_{T}}=0\Big\},
(6.7) 𝔖2\displaystyle\mathfrak{S}_{2} ≑{f∈C0,α​(β„³T)|f​is​S1​-invariant andβ€‹βˆ«β„³Tfβ‹…Ο‰Tn=0}.\displaystyle\equiv\Big\{f\in C^{0,\alpha}(\mathcal{M}_{T})\Big|f\ \text{is}\ S^{1}\text{-invariant and}\ \int_{\mathcal{M}_{T}}f\cdot\omega_{T}^{n}=0\Big\}.

endowed with the weighted HΓΆlder norms

(6.8) β€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•β€–π”–1\displaystyle\|\sqrt{-1}\partial\bar{\partial}\phi\|_{\mathfrak{S}_{1}} β‰‘β€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•β€–CΞ΄,Ξ½+2,ΞΌ0,α​(Xt),\displaystyle\equiv\|\sqrt{-1}\partial\bar{\partial}\phi\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(X_{t})},
(6.9) β€–f‖𝔖2\displaystyle\|f\|_{\mathfrak{S}_{2}} β‰‘β€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•β€–CΞ΄,Ξ½+2,ΞΌ0,α​(Xt).\displaystyle\equiv\|\sqrt{-1}\partial\bar{\partial}\phi\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(X_{t})}.

Notice an S1S^{1} invariant function Ο•\phi on β„³T\mathcal{M}_{T} can be identified with a function on the quotient QTQ_{T}, and the Neumann boundary condition βˆ‚Ο•βˆ‚n|βˆ‚β„³T=0\frac{\partial\phi}{\partial n}|_{\partial\mathcal{M}_{T}}=0 amounts to the condition βˆ‚zΟ•=0\partial_{z}\phi=0 on βˆ‚QT\partial Q_{T}.

In this section, the weight parameters are specified as follows:

  1. (NP1)

    (Fix Ξ½\nu) The parameters Ξ½βˆˆβ„\nu\in\mathbb{R} is chosen such that

    (6.10) ν∈(βˆ’1,0).\displaystyle\nu\in(-1,0).

    In our context, Lemma 6.5 requires ν∈(βˆ’1,1)\nu\in(-1,1). To effectively apply Proposition 4.23, we need ν∈(βˆ’1,0)\nu\in(-1,0).

  2. (NP2)

    (Fix α\alpha) The Hâlder order α∈(0,1)\alpha\in(0,1) is chosen sufficiently small such that

    (6.11) Ξ½+Ξ±<0.\nu+\alpha<0.
  3. (NP3)

    (Fix Ξ΄\delta) Ξ΄>0\delta>0 is chosen such that

    (6.12) 0<Ξ΄<Ξ΄N≑1nβ‹…(|kβˆ’|+|k+|)nβ‹…min⁑{Ξ΄b,Ξ΄e,Ξ»D},0<\delta<\delta_{N}\equiv\frac{1}{n\cdot(|k_{-}|+|k_{+}|)^{n}}\cdot\min\{\delta_{b},\delta_{e},\sqrt{\lambda_{D}}\},

    where Ο΅X>0\epsilon_{X}>0 is the constant in Theorem 5.2, Ξ»D\sqrt{\lambda_{D}} is in Lemma 6.7 (Liouville theorem on QQ), Ξ΄b>0\delta_{b}>0 is in Proposition 5.14 (Liouville theorem on the Calabi space π’žn\mathcal{C}^{n} around the boundary of the neck), Ξ΄e>0\delta_{e}>0 is in the error estimate Proposition 4.23.

  4. (NP4)

    (Fix ΞΌ\mu) The parameter ΞΌ\mu is fixed by

    (6.13) ΞΌ=(1βˆ’1n)​(Ξ½+2+Ξ±).\mu=(1-\frac{1}{n})(\nu+2+\alpha).

    This condition guarantees that the weight function ρδ,ν,μ(α)\rho_{\delta,\nu,\mu}^{(\alpha)} with parameters specified as the above is uniformly bounded from below. This will be used in proving Proposition 6.4.

We first normalize the holomorphic volume form. For T≫1T\gg 1, starting with the C2,Ξ±C^{2,\alpha}-KΓ€hler structure (Ο‰T,Ξ©T)(\omega_{T},\Omega_{T}), we will solve the Calabi-Yau equation

(6.14) 1n!​(Ο‰T+βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•)n=(βˆ’1)n2​2βˆ’nβ‹…Ξ©T∧.Ω¯T.\frac{1}{n!}(\omega_{T}+\sqrt{-1}\partial\bar{\partial}\phi)^{n}=(\sqrt{-1})^{n^{2}}2^{-n}\cdot\Omega_{T}\wedge.\bar{\Omega}_{T}.

Notice that

(6.15) βˆ«β„³T(βˆ’1)n22n​ΩT∧Ω¯T\displaystyle\int_{\mathcal{M}_{T}}\frac{(\sqrt{-1})^{n^{2}}}{2^{n}}\Omega_{T}\wedge\bar{\Omega}_{T} =βˆ«β„³Thβ‹…Ο‰Dnβˆ’1(nβˆ’1)!​𝑑z∧Θ=∫Tβˆ’T+d​zβ€‹βˆ«Dh​ωDnβˆ’1(nβˆ’1)!\displaystyle=\int_{\mathcal{M}_{T}}h\cdot\frac{\omega_{D}^{n-1}}{(n-1)!}dz\wedge\Theta=\int_{T_{-}}^{T_{+}}dz\int_{D}h\frac{\omega_{D}^{n-1}}{(n-1)!}

and

(6.16) βˆ«β„³TΟ‰Tnn!=T2βˆ’nβ€‹βˆ«β„³TΟ‰~​(z)nβˆ’1(nβˆ’1)!​𝑑z∧Θ=T2βˆ’n(nβˆ’1)!β€‹βˆ«Tβˆ’T+d​zβ€‹βˆ«DΟ‰~​(z)nβˆ’1=C1​T2\displaystyle\int_{\mathcal{M}_{T}}\frac{\omega_{T}^{n}}{n!}=T^{2-n}\int_{\mathcal{M}_{T}}\frac{\tilde{\omega}(z)^{n-1}}{(n-1)!}dz\wedge\Theta=\frac{T^{2-n}}{(n-1)!}\int_{T_{-}}^{T_{+}}dz\int_{D}\tilde{\omega}(z)^{n-1}=C_{1}T^{2}

for some computable constant C1>0C_{1}>0. So by (4.14) we get

(6.17) βˆ«β„³T(βˆ’1)n22n​ΩT∧Ω¯T=(1+O⁑(Tβˆ’2))β€‹βˆ«β„³TΟ‰Tnn!.\int_{\mathcal{M}_{T}}\frac{(\sqrt{-1})^{n^{2}}}{2^{n}}\Omega_{T}\wedge\bar{\Omega}_{T}=(1+O(T^{-2}))\int_{\mathcal{M}_{T}}\frac{\omega_{T}^{n}}{n!}.

Now we replace Ξ©T\Omega_{T} by

(6.18) (βˆ«β„³T(βˆ’1)n22n​ΩT∧ΩTΒ―βˆ«β„³TΟ‰Tnn!)βˆ’12​ΩT\Big(\frac{\int_{\mathcal{M}_{T}}\frac{(\sqrt{-1})^{n^{2}}}{2^{n}}\Omega_{T}\wedge\bar{\Omega_{T}}}{\int_{\mathcal{M}_{T}}\frac{\omega_{T}^{n}}{n!}}\Big)^{-\frac{1}{2}}\Omega_{T}

Then we have

(6.19) (βˆ’1)n22n​ΩT∧Ω¯T=(1+ErrC​Y)​ωTnn!\frac{(\sqrt{-1})^{n^{2}}}{2^{n}}\Omega_{T}\wedge\bar{\Omega}_{T}=(1+\mathrm{Err}_{CY})\frac{\omega_{T}^{n}}{n!}

where

(6.20) βˆ«β„³TErrC​Y​ωTn=0.\int_{\mathcal{M}_{T}}\mathrm{Err}_{CY}\omega_{T}^{n}=0.

Applying Proposition 4.23 and (6.13),

(6.21) β€–ErrC​Yβ€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³T)=O⁑(TΞ½+Ξ±).\|\mathrm{Err}_{CY}\|_{C^{0,\alpha}_{\delta,\nu+2,\mu}(\mathcal{M}_{T})}=O(T^{\nu+\alpha}).

Let β„±\mathscr{F} be the map sending every βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•βˆˆπ”–1\sqrt{-1}\partial\bar{\partial}\phi\in\mathfrak{S}_{1} to the function which satisfies

(6.22) ℱ⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•)β‹…Ο‰Tn≑(Ο‰T+βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•)nβˆ’Ο‰Tn​(1βˆ’ErrC​Y).\mathscr{F}(\sqrt{-1}\partial\bar{\partial}\phi)\cdot\omega_{T}^{n}\equiv(\omega_{T}+\sqrt{-1}\partial\bar{\partial}\phi)^{n}-\omega_{T}^{n}(1-\mathrm{Err}_{CY}).

Then (6.21) immediately tells us that

(6.23) ‖ℱ⁑(𝟎)‖𝔖2=O⁑(TΞ½+Ξ±).\|\mathscr{F}(\bm{0})\|_{\mathfrak{S}_{2}}=O(T^{\nu+\alpha}).
Lemma 6.2.

ℱ⁑(𝔖1)βŠ‚π”–2\mathscr{F}(\mathfrak{S}_{1})\subset\mathfrak{S}_{2}.

Proof.

This amounts to proving that

(6.24) βˆ«β„³Tℱ⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•)​ωTn=0.\int_{\mathcal{M}_{T}}\mathscr{F}(\sqrt{-1}\partial\bar{\partial}\phi)\omega_{T}^{n}=0.

By Stokes’ theorem,

(6.25) βˆ«β„³T(Ο‰T+βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•)nβˆ’βˆ«β„³TΟ‰Tn=βˆ«βˆ‚β„³TΞ³,\int_{\mathcal{M}_{T}}(\omega_{T}+\sqrt{-1}\partial\bar{\partial}\phi)^{n}-\int_{\mathcal{M}_{T}}\omega_{T}^{n}=\int_{\partial\mathcal{M}_{T}}\gamma,

where Ξ³\gamma is the sum of terms involving one factor dc​ϕd^{c}\phi and either d​dc​ϕdd^{c}\phi or Ο‰T\omega_{T}. We claim that Ξ³\gamma identically vanishes on βˆ‚β„³T\partial\mathcal{M}_{T}. It suffices to show βˆ‚tβŒŸβ€‹Ξ³=0\partial_{t}\lrcorner\gamma=0. Since by assumption Ο•\phi is S1S^{1}-invariant, so we have βˆ‚tΟ•=0\partial_{t}\phi=0. By the Neumann boundary condition, we also have dcΟ•(βˆ‚t)=0d^{c}\phi(\partial_{t})=0 on βˆ‚β„³T\partial\mathcal{M}_{T}. This follows from the observation that Jβˆ‚t=βˆ‡zJ\partial_{t}=\nabla z. Now

(6.26) βˆ‚tβŒŸβ€‹Ο‰T|βˆ‚β„³T\displaystyle\partial_{t}\lrcorner\omega_{T}|_{\partial\mathcal{M}_{T}} =d​z|βˆ‚β„³T=0,\displaystyle=dz|_{\partial\mathcal{M}_{T}}=0,
(6.27) βˆ‚tβŒŸβ€‹d​dc​ϕ\displaystyle\partial_{t}\lrcorner dd^{c}\phi =β„’βˆ‚t​(dc​ϕ)βˆ’d⁑(βˆ‚tβŒŸβ€‹dc​ϕ)=βˆ’d⁑(βˆ‚tβŒŸβ€‹dc​ϕ).\displaystyle=\mathcal{L}_{\partial_{t}}(d^{c}\phi)-d(\partial_{t}\lrcorner d^{c}\phi)=-d(\partial_{t}\lrcorner d^{c}\phi).

The last term vanishes on βˆ‚β„³T\partial\mathcal{M}_{T} since dcΟ•(βˆ‚t)=0d^{c}\phi(\partial_{t})=0 pointwise on βˆ‚β„³T\partial\mathcal{M}_{T}. ∎

Now we are ready to state the main result in this section.

Theorem 6.3 (Existence of S1S^{1}-invariant Calabi-Yau metrics).

For each sufficiently large TT, there exists an S1S^{1}-invariant Calabi-Yau metric Ο‰T,C​Y=Ο‰T+βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•\omega_{T,CY}=\omega_{T}+\sqrt{-1}\partial\bar{\partial}\phi for Ο•βˆˆπ”–1\phi\in\mathfrak{S}_{1}, such that

(6.28) β€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•β€–π”–1≀C0β‹…TΞ½+Ξ±,\|\sqrt{-1}\partial\bar{\partial}\phi\|_{\mathfrak{S}_{1}}\leq C_{0}\cdot T^{\nu+\alpha},

where C0>0C_{0}>0 is a uniform constant independent of T≫1T\gg 1 and the weighted HΓΆlder norm of 𝔖1\mathfrak{S}_{1} is defined in (6.8) for parameters Ξ½\nu, Ξ±\alpha, Ξ΄\delta and ΞΌ\mu satisfying (6.10), (6.11), (6.12) and (6.13).

To prove Theorem 6.3, we decompose the map β„±:𝔖1→𝔖2\mathscr{F}:\mathfrak{S}_{1}\to\mathfrak{S}_{2} as follows,

(6.29) ℱ⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•)βˆ’β„±β‘(𝟎)=ℒ⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•)+𝒩⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•),\mathscr{F}(\sqrt{-1}\partial\bar{\partial}\phi)-\mathscr{F}(\bm{0})=\mathscr{L}(\sqrt{-1}\partial\bar{\partial}\phi)+\mathscr{N}(\sqrt{-1}\partial\bar{\partial}\phi),

for any βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•βˆˆπ”–1\sqrt{-1}\partial\bar{\partial}\phi\in\mathfrak{S}_{1}, where

(6.30) ℒ⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•)\displaystyle\mathscr{L}(\sqrt{-1}\partial\bar{\partial}\phi) =Δ​ϕ,\displaystyle=\Delta\phi,
(6.31) 𝒩⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•)β‹…Ο‰Tn\displaystyle\mathscr{N}(\sqrt{-1}\partial\bar{\partial}\phi)\cdot\omega_{T}^{n} =(Ο‰T+βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•)nβˆ’Ο‰Tnβˆ’n​ωTnβˆ’1βˆ§βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•.\displaystyle=(\omega_{T}+\sqrt{-1}\partial\bar{\partial}\phi)^{n}-\omega_{T}^{n}-n\omega_{T}^{n-1}\wedge\sqrt{-1}\partial\bar{\partial}\phi.

By the definition of the weight function and Lemma 4.20, we have the following nonlinear error estimate.

Lemma 6.4 (Nonlinear error estimate).

For any sufficiently large T≫1T\gg 1, let β„³T\mathcal{M}_{T} be the neck endowed with the C2,Ξ±C^{2,\alpha}-structure (Ο‰T,Ξ©T)(\omega_{T},\Omega_{T}). Then there exists a constant CN>0C_{N}>0 independent of T≫1T\gg 1 such that for all

(6.32) ϱ∈(0,12)\varrho\in(0,\frac{1}{2})

and

(6.33) βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•2∈Bϱ​(𝟎)Β―βŠ‚π”–1,βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•2∈Bϱ​(𝟎)Β―βŠ‚π”–1,\sqrt{-1}\partial\bar{\partial}\phi_{2}\in\overline{B_{\varrho}(\bm{0})}\subset\mathfrak{S}_{1},\quad\sqrt{-1}\partial\bar{\partial}\phi_{2}\in\overline{B_{\varrho}(\bm{0})}\subset\mathfrak{S}_{1},

we have the pointwise estimate

(6.34) ‖𝒩⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•1)βˆ’π’©β‘(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•2)‖𝔖2≀CNβ‹…Ο±β‹…β€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹(Ο•1βˆ’Ο•2)‖𝔖1.\displaystyle\|\mathscr{N}(\sqrt{-1}\partial\bar{\partial}\phi_{1})-\mathscr{N}(\sqrt{-1}\partial\bar{\partial}\phi_{2})\|_{\mathfrak{S}_{2}}\leq C_{N}\cdot\varrho\cdot\|\sqrt{-1}\partial\bar{\partial}(\phi_{1}-\phi_{2})\|_{\mathfrak{S}_{1}}.
Proof.

By definition,

(𝒩⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•1)βˆ’π’©β‘(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•2))⋅ω​(t)n\displaystyle\Big(\mathscr{N}(\sqrt{-1}\partial\bar{\partial}\phi_{1})-\mathscr{N}(\sqrt{-1}\partial\bar{\partial}\phi_{2})\Big)\cdot\omega(t)^{n}
(6.35) =\displaystyle= βˆ‘k=2n(nk)⋅ω​(t)nβˆ’k∧((βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•1)kβˆ’(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•2)k).\displaystyle\sum\limits_{k=2}^{n}\begin{pmatrix}n\\ k\end{pmatrix}\cdot\omega(t)^{n-k}\wedge\Big((\sqrt{-1}\partial\bar{\partial}\phi_{1})^{k}-(\sqrt{-1}\partial\bar{\partial}\phi_{2})^{k}\Big).

By the definition of the norm on 𝔖1\mathfrak{S}_{1}, we have

(6.36) β€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•1β€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³T)≀ϱ,β€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•1β€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³T)≀ϱ.\|\sqrt{-1}\partial\bar{\partial}\phi_{1}\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{T})}\leq\varrho,\quad\|\sqrt{-1}\partial\bar{\partial}\phi_{1}\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{T})}\leq\varrho.

With ΞΌ\mu specified by (6.13), by Lemma 4.20, the weight function ρδ,Ξ½+2,ΞΌ(Ξ±):β„³T→ℝ+\rho_{\delta,\nu+2,\mu}^{(\alpha)}:\mathcal{M}_{T}\to\mathbb{R}_{+} satisfies for any π’™βˆˆβ„³T\bm{x}\in\mathcal{M}_{T},

(6.37) ρδ,Ξ½+2,ΞΌ(Ξ±)​(𝒙)β‰₯1.\rho_{\delta,\nu+2,\mu}^{(\alpha)}(\bm{x})\geq 1.

This implies the following weight-free estimates,

(6.38) β€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•1β€–C0,α​(β„³T)≀C0β‹…Ο±andβ€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•2β€–C0,α​(β„³T)≀C0β‹…Ο±,\|\sqrt{-1}\partial\bar{\partial}\phi_{1}\|_{C^{0,\alpha}(\mathcal{M}_{T})}\leq C_{0}\cdot\varrho\quad\text{and}\quad\|\sqrt{-1}\partial\bar{\partial}\phi_{2}\|_{C^{0,\alpha}(\mathcal{M}_{T})}\leq C_{0}\cdot\varrho,

where C0>0C_{0}>0 is a uniform constant independent of T≫1T\gg 1.

Since the L∞L^{\infty}-norm of the KΓ€hler form Ο‰T\omega_{T} is bounded by a uniform constant (independent of T≫1T\gg 1), so the above estimates imply the pointwise estimate for 𝒩\mathscr{N},

(6.39) |𝒩⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•1)βˆ’π’©β‘(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•2)|≀CNβ‹…Ο±β‹…|βˆ’1β€‹βˆ‚βˆ‚Β―β€‹(Ο•1βˆ’Ο•2)|,|\mathscr{N}(\sqrt{-1}\partial\bar{\partial}\phi_{1})-\mathscr{N}(\sqrt{-1}\partial\bar{\partial}\phi_{2})|\leq C_{N}\cdot\varrho\cdot|\sqrt{-1}\partial\bar{\partial}(\phi_{1}-\phi_{2})|,

where CN>0C_{N}>0 is a uniform constant independent of TT. Write the above in terms of the weighted norms, we have

(6.40) ‖𝒩⁑(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•1)βˆ’π’©β‘(βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•2)β€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³T)≀CNβ‹…Ο±β‹…β€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹(Ο•1βˆ’Ο•2)β€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³T).\|\mathscr{N}(\sqrt{-1}\partial\bar{\partial}\phi_{1})-\mathscr{N}(\sqrt{-1}\partial\bar{\partial}\phi_{2})\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{T})}\leq C_{N}\cdot\varrho\cdot\|\sqrt{-1}\partial\bar{\partial}(\phi_{1}-\phi_{2})\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{T})}.

The proof is done.

∎

To apply the implicit function theorem, we still need to prove the weighted linear estimate, which will be completed in the following subsections.

6.2. Some Liouville type theorems and removable singularity theorems

In this subsection, we introduce some removable singularity and Liouville type theorems, which will be needed in the proof of Proposition 7.15. For the convenience of discussions, we give precise statement here.

Lemma 6.5 (Removable singularity).

Let (Mn,g)(M^{n},g) be a Riemannian manifold such that BR​(p)B_{R}(p) has a compact closure in B2​R​(p)B_{2R}(p). Let KβŠ‚MnK\subset M^{n} be a smooth submanifold with dim(K)=k0≀nβˆ’3\dim(K)=k_{0}\leq n-3. If uu is harmonic in BR​(p)βˆ–KB_{R}(p)\setminus K and there is some ϡ∈(0,1)\epsilon\in(0,1) such that

(6.41) |u⁑(x)|≀Cdg​(x,K)(nβˆ’2βˆ’k0)βˆ’Ο΅,|u(x)|\leq\frac{C}{d_{g}(x,K)^{(n-2-k_{0})-\epsilon}},

then uu is harmonic in BR​(p)B_{R}(p).

Proof.

The point is to apply integration by parts to show that uu is a weak solution to Δ​u=0\Delta u=0 on BR​(p)B_{R}(p). The computations are routine and standard in the literature, so we just skip it. ∎

Lemma 6.6 (Liouville theorem on ℝm+n\mathbb{R}^{m+n}).

Given m,nβˆˆβ„€+m,n\in\mathbb{Z}_{+} with m+nβ‰₯3m+n\geq 3, Let ΞΌp∈(βˆ’1,1)βˆ–{0}\mu_{p}\in(-1,1)\setminus\{0\} and let u∈Cβˆžβ€‹(ℝm+n)u\in C^{\infty}(\mathbb{R}^{m+n}) be a harmonic function on the Euclidean space (ℝm+n,gℝmβŠ•gℝn)(\mathbb{R}^{m+n},g_{\mathbb{R}^{m}}\oplus g_{\mathbb{R}^{n}}). If uu satsifies

(6.42) |u⁑(x,y)|≀C|x|ΞΌp,βˆ€(x,y)∈(ℝmβˆ–{0})×ℝn,\displaystyle|u(x,y)|\leq\frac{C}{|x|^{\mu_{p}}},\ \forall(x,y)\in(\mathbb{R}^{m}\setminus\{0\})\times\mathbb{R}^{n},

then u≑0u\equiv 0 on ℝm+n\mathbb{R}^{m+n}.

Proof.

The proof is rather standard and straightforward, which can be achieved by using separation of variables.

For the simplicity of notations, we denote

(6.43) d≑m+nβ‰₯3.d\equiv m+n\geq 3.

Let (r,Θ)βˆˆβ„d(r,\Theta)\in\mathbb{R}^{d} be the polar coordinate system in ℝd\mathbb{R}^{d}, so the Laplacian of uu can be written as

(6.44) Δℝd​u=βˆ‚2uβˆ‚r2+dβˆ’1rβ‹…βˆ‚uβˆ‚r+1r2β‹…Ξ”π•Šdβˆ’1​u.\Delta_{\mathbb{R}^{d}}u=\frac{\partial^{2}u}{\partial r^{2}}+\frac{d-1}{r}\cdot\frac{\partial u}{\partial r}+\frac{1}{r^{2}}\cdot\Delta_{\mathbb{S}^{d-1}}u.

We make separation of variables on the punctured Euclidean space ℝdβˆ–{0d}\mathbb{R}^{d}\setminus\{0^{d}\}. Let

(6.45) Ξ»j≑j⁑(j+dβˆ’2),jβˆˆβ„•,\lambda_{j}\equiv j(j+d-2),\ j\in\mathbb{N},

be the spectrum of the unit round sphere π•Šdβˆ’1\mathbb{S}^{d-1}. Correspondingly, let Ο†j∈Cβˆžβ€‹(π•Šdβˆ’1)\varphi_{j}\in C^{\infty}(\mathbb{S}^{d-1}) satisfy

(6.46) βˆ’Ξ”π•Šdβˆ’1​φj​(Θ)=Ξ»j​φj​(Θ).-\Delta_{\mathbb{S}^{d-1}}\varphi_{j}(\Theta)=\lambda_{j}\varphi_{j}(\Theta).

Then the function u⁑(r,Θ)u(r,\Theta) has the expansion along the fiber π•Šdβˆ’1\mathbb{S}^{d-1},

(6.47) u⁑(r,Θ)=βˆ‘j=0∞uj​(r)β‹…Ο†j​(Θ).u(r,\Theta)=\sum\limits_{j=0}^{\infty}u_{j}(r)\cdot\varphi_{j}(\Theta).

Immediately, for each jβˆˆβ„•j\in\mathbb{N}, the coefficient function uj​(r)u_{j}(r) solves the Euler-Cauchy equation,

(6.48) uj′′​(r)+dβˆ’1rβ‹…uj′​(r)βˆ’1r2β‹…Ξ»jβ‹…uj​(r)=0,u_{j}^{\prime\prime}(r)+\frac{d-1}{r}\cdot u_{j}^{\prime}(r)-\frac{1}{r^{2}}\cdot\lambda_{j}\cdot u_{j}(r)=0,

which has a general solution

(6.49) uj​(r)=Cjβ‹…rpj+Cjβˆ—β‹…rqj,u_{j}(r)=C_{j}\cdot r^{p_{j}}+C_{j}^{*}\cdot r^{q_{j}},

where pj=2βˆ’d+(dβˆ’2)2+4​λj2β‰₯0p_{j}=\frac{2-d+\sqrt{(d-2)^{2}+4\lambda_{j}}}{2}\geq 0 and qj=2βˆ’dβˆ’(dβˆ’2)2+4​λj2<0q_{j}=\frac{2-d-\sqrt{(d-2)^{2}+4\lambda_{j}}}{2}<0 solve the quadratic equation

(6.50) w2+(dβˆ’2)​wβˆ’Ξ»j=0.w^{2}+(d-2)w-\lambda_{j}=0.

So it is obvious

p0\displaystyle p_{0} =0,q0=2βˆ’dβ‰€βˆ’1,\displaystyle=0,\quad q_{0}=2-d\leq-1,
pj\displaystyle p_{j} β‰₯p1=1,\displaystyle\geq p_{1}=1,
(6.51) qj\displaystyle q_{j} ≀q1=1βˆ’dβ‰€βˆ’2,jβˆˆβ„€+.\displaystyle\leq q_{1}=1-d\leq-2,\quad j\in\mathbb{Z}_{+}.

In the following, we will show that, given the growth condition (6.42) for ΞΌp∈(βˆ’1,1)βˆ–{0}\mu_{p}\in(-1,1)\setminus\{0\}, then for each jβˆˆβ„•j\in\mathbb{N} and for each r>0r>0, the coefficient uj​(r)u_{j}(r) satisfies

(6.52) |uj​(r)|≀QjrΞΌp,|u_{j}(r)|\leq\frac{Q_{j}}{r^{\mu_{p}}},

where Qjβˆˆβ„Q_{j}\in\mathbb{R}. In fact, so it follows from the expansion (6.47) that for each jβˆˆβ„•j\in\mathbb{N},

(6.53) uj​(r)=βˆ«π•Šdβˆ’1u⁑(r,Θ)β‹…Ο†j​dvolπ•Šdβˆ’1,u_{j}(r)=\int_{\mathbb{S}^{d-1}}u(r,\Theta)\cdot\varphi_{j}\dvol_{\mathbb{S}^{d-1}},

which implies

(6.54) |uj​(r)|≀|Ο†j|Lβˆžβ€‹(π•Šdβˆ’1)β‹…βˆ«π•Šdβˆ’11|x|ΞΌp​dvolπ•Šdβˆ’1.|u_{j}(r)|\leq|\varphi_{j}|_{L^{\infty}(\mathbb{S}^{d-1})}\cdot\int_{\mathbb{S}^{d-1}}\frac{1}{|x|^{\mu_{p}}}\dvol_{\mathbb{S}^{d-1}}.

Next, we will write the above integral in the polar coordinates Ξ˜β‰‘(ΞΈ1,…,ΞΈdβˆ’1)\Theta\equiv(\theta_{1},\ldots,\theta_{d-1}) with ΞΈ1,…,ΞΈdβˆ’2∈[0,Ο€]\theta_{1},\ldots,\theta_{d-2}\in[0,\pi] and ΞΈdβˆ’1∈[0,2​π]\theta_{d-1}\in[0,2\pi]. Denote by dβ€‹Ξ˜β‰‘d​θ1∧d​θ2βˆ§β€¦βˆ§d​θdβˆ’1d\Theta\equiv d\theta_{1}\wedge d\theta_{2}\wedge\ldots\wedge d\theta_{d-1}, then it is by elementary calculations that, |x|=rmβ‹…βˆk=1dβˆ’m|sin⁑θk||x|=r^{m}\cdot\prod\limits_{k=1}^{d-m}|\sin\theta_{k}| and dvolπ•Šdβˆ’1=∏k=1dβˆ’2(sindβˆ’kβˆ’1⁑θk)β‹…dβ€‹Ξ˜\dvol_{\mathbb{S}^{d-1}}=\prod\limits_{k=1}^{d-2}(\sin^{d-k-1}\theta_{k})\cdot d\Theta. Therefore,

(6.55) βˆ«π•Šdβˆ’11|x|ΞΌp​dvolπ•Šdβˆ’1=1rΞΌpβ€‹βˆ«π’ŸΞ˜βˆk=1dβˆ’2(sindβˆ’kβˆ’1⁑θk)∏k=1dβˆ’m|sin⁑θk|ΞΌpβ‹…π‘‘Ξ˜,\int_{\mathbb{S}^{d-1}}\frac{1}{|x|^{\mu_{p}}}\dvol_{\mathbb{S}^{d-1}}=\frac{1}{r^{\mu_{p}}}\int_{\mathcal{D}_{\Theta}}\frac{\prod\limits_{k=1}^{d-2}(\sin^{d-k-1}\theta_{k})}{\prod\limits_{k=1}^{d-m}|\sin\theta_{k}|^{\mu_{p}}}\cdot d\Theta,

where π’ŸΞ˜β‰‘{0≀θ1,…,ΞΈdβˆ’2≀π, 0≀θdβˆ’1≀2Ο€}\mathcal{D}_{\Theta}\equiv\{0\leq\theta_{1},\ldots,\theta_{d-2}\leq\pi,\ 0\leq\theta_{d-1}\leq 2\pi\}. By assumption, ΞΌp∈(βˆ’1,1)βˆ–{0}\mu_{p}\in(-1,1)\setminus\{0\}, then ∏k=1dβˆ’2(sindβˆ’kβˆ’1⁑θk)∏k=1dβˆ’m|sin⁑θk|ΞΌp\frac{\prod\limits_{k=1}^{d-2}(\sin^{d-k-1}\theta_{k})}{\prod\limits_{k=1}^{d-m}|\sin\theta_{k}|^{\mu_{p}}} is integrable in π’ŸΞ˜\mathcal{D}_{\Theta} and we denote

(6.56) ℐ0β‰‘βˆ«π’ŸΞ˜βˆk=1dβˆ’2(sindβˆ’kβˆ’1⁑θk)∏k=1dβˆ’m|sin⁑θk|ΞΌpβ‹…π‘‘Ξ˜.\mathcal{I}_{0}\equiv\int_{\mathcal{D}_{\Theta}}\frac{\prod\limits_{k=1}^{d-2}(\sin^{d-k-1}\theta_{k})}{\prod\limits_{k=1}^{d-m}|\sin\theta_{k}|^{\mu_{p}}}\cdot d\Theta.

Therefore, for each jβˆˆβ„•j\in\mathbb{N}, it holds that

(6.57) |uj​(r)|≀ℐ0β‹…|Ο†j|Lβˆžβ€‹(π•Šdβˆ’1)rΞΌp≑QjrΞΌp|u_{j}(r)|\leq\frac{\mathcal{I}_{0}\cdot|\varphi_{j}|_{L^{\infty}(\mathbb{S}^{d-1})}}{r^{\mu_{p}}}\equiv\frac{Q_{j}}{r^{\mu_{p}}}

for all r>0r>0.

Now we go back to the representation of uj​(r)u_{j}(r) in (6.49) and we analyze the growth behavior of function as rβ‰ͺ1r\ll 1 and r≫1r\gg 1. Applying the assumption ΞΌp∈(βˆ’1,1)βˆ–{0}\mu_{p}\in(-1,1)\setminus\{0\} and the gap obtained in (6.51), we have that, for each jβˆˆβ„•j\in\mathbb{N}, Cj=Cjβˆ—=0C_{j}=C_{j}^{*}=0. Therefore,

(6.58) u≑0​on​ℝm+n.u\equiv 0\ \text{on}\ \mathbb{R}^{m+n}.

∎

Lemma 6.7 (Liouville theorem on a cylinder).

Let (Q,gQ)≑(D×ℝ,gQ)(Q,g_{Q})\equiv(D\times\mathbb{R},g_{Q}) be a cylinder with a product Riemannian metric gQ=gDβŠ•d​z2g_{Q}=g_{D}\oplus dz^{2}, where (D,gD)(D,g_{D}) is a closed Riemannian manifold. Denote by Ξ»D>0\lambda_{D}>0 the lowest eigenvalue of the Laplace-Beltrami operator of (D,gD)(D,g_{D}) acting on functions. If uu is a harmonic function on QQ satisfying the growth control

(6.59) |u|=O⁑(eΞ»cβ‹…z)|u|=O(e^{\lambda_{c}\cdot z})

for some Ξ»c∈(0,Ξ»D)\lambda_{c}\in(0,\sqrt{\lambda_{D}}), then u≑0u\equiv 0.

The proof follows from standard separation of variables, very similar to the proof of Proposition 3.31. We omit the details.

6.3. Weighted analysis and existence of incomplete Calabi-Yau metrics

We first prove

Proposition 6.8 (Uniform injectivity estimate on the neck).

For any sufficiently large parameter T≫1T\gg 1, the linearized operator defined in (6.30)

(6.60) β„’:𝔖1→𝔖2,βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•β†¦Ξ”β€‹Ο•\mathscr{L}:\mathfrak{S}_{1}\rightarrow\mathfrak{S}_{2},\quad\sqrt{-1}\partial\bar{\partial}\phi\mapsto\Delta\phi

is an isomorphism and satisfies the uniform injectivity estimate,

(6.61) β€–βˆ’1β€‹βˆ‚βˆ‚Β―β€‹Ο•β€–π”„β‰€CL⋅‖Δ​ϕ‖𝔅.\|\sqrt{-1}\partial\bar{\partial}\phi\|_{\mathfrak{A}}\leq C_{L}\cdot\|\Delta\phi\|_{\mathfrak{B}}.

Here the constant CL>0C_{L}>0 is independent of the parameter T≫1T\gg 1.

A preliminary ingredient in proving Proposition 6.8 is the following weighted Schauder estimate on β„³T\mathcal{M}_{T}.

Proposition 6.9 (Weighted Schauder estimate on the neck, the global version).

For every sufficiently large parameter T≫1T\gg 1, let β„³T\mathcal{M}_{T} be the neck region with an S1S^{1}-invariant KΓ€hler metric Ο‰T\omega_{T} constructed in Section 4.1. Then the following estimate hold:

(6.62) β€–uβ€–CΞ΄,Ξ½,ΞΌ2,α​(β„³T)≀C⁑(‖Δ​uβ€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³T)+β€–βˆ‚uβˆ‚nβ€–CΞ΄,Ξ½+1,ΞΌ1,Ξ±+β€–uβ€–CΞ΄,Ξ½,ΞΌ0​(β„³T)),\|u\|_{C_{\delta,\nu,\mu}^{2,\alpha}(\mathcal{M}_{T})}\leq C\Big(\|\Delta u\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{T})}+\Big\|\frac{\partial u}{\partial n}\Big\|_{C_{\delta,\nu+1,\mu}^{1,\alpha}}+\|u\|_{C_{\delta,\nu,\mu}^{0}(\mathcal{M}_{T})}\Big),

where the constant C>0C>0 is independent of T≫1T\gg 1.

Proof.

The proof follows directly from Proposition 4.22 and standard covering argument. We just skip the detailed proof.

∎

Next, the key part of the injectivity estimate in Proposition 6.8 is the following weighted estimate for higher derivatives with respect to the Neumann boundary value problem.

Proposition 6.10 (Uniform injectivity estimate on the neck).

Given a large parameter T≫1T\gg 1, let β„³T\mathcal{M}_{T} be the neck region with an S1S^{1}-symmetric KΓ€hler metric Ο‰T\omega_{T} constructed in Section 4.1. Let the parameters ΞΌ\mu, Ξ½\nu, Ξ±\alpha, Ξ΄\delta satisfy satisfying

(6.63) βˆ’1<Ξ½<0,Ξ½+Ξ±<0,0<Ξ΄<Ξ΄N,ΞΌ=(1βˆ’1n)​(Ξ½+2+Ξ±)\displaystyle-1<\nu<0,\quad\nu+\alpha<0,\quad 0<\delta<\delta_{N},\ \mu=(1-\frac{1}{n})(\nu+2+\alpha)

as fixed in (6.10), (6.11), (6.12) and (6.13), then there exists a uniform constant C>0C>0 (independent of TT) such that for every u∈C2,α​(β„³T)u\in C^{2,\alpha}(\mathcal{M}_{T}) satisfying the boundary condition βˆ‚uβˆ‚n|βˆ‚β„³T=0\frac{\partial u}{\partial n}|_{\partial\mathcal{M}_{T}}=0, we have

(6.64) β€–βˆ‡uβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„³T)+β€–βˆ‡2uβ€–CΞ΄,Ξ½+2,ΞΌ0​(β„³T)≀C⋅‖Δ​uβ€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³T),\displaystyle\|\nabla u\|_{C_{\delta,\nu+1,\mu}^{0}(\mathcal{M}_{T})}+\|\nabla^{2}u\|_{C_{\delta,\nu+2,\mu}^{0}(\mathcal{M}_{T})}\leq C\cdot\|\Delta u\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{T})},
(6.65) [u]CΞ΄,Ξ½,ΞΌ2,α​(β„³T)≀C⋅‖Δ​uβ€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³T).\displaystyle[u]_{C_{\delta,\nu,\mu}^{2,\alpha}(\mathcal{M}_{T})}\leq C\cdot\|\Delta u\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{T})}.
Proof.

The proof of the uniform estimate consists of two primary steps: In the first step, we will prove the weighted C1C^{1} and C2C^{2} estimates,

(6.66) β€–βˆ‡uβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„³T)+β€–βˆ‡2uβ€–CΞ΄,Ξ½+2,ΞΌ0​(β„³T)≀C⋅‖Δ​uβ€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³T).\|\nabla u\|_{C_{\delta,\nu+1,\mu}^{0}(\mathcal{M}_{T})}+\|\nabla^{2}u\|_{C_{\delta,\nu+2,\mu}^{0}(\mathcal{M}_{T})}\leq C\cdot\|\Delta u\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{T})}.

Next, based on the above weighted estimate and the weighted Schauder estimate (by Proposition 6.9), we will prove

(6.67) β€–βˆ‡uβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„³T)+β€–βˆ‡2uβ€–CΞ΄,Ξ½+2,ΞΌ0​(β„³T)≀C⋅‖Δ​uβ€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³T).\|\nabla u\|_{C_{\delta,\nu+1,\mu}^{0}(\mathcal{M}_{T})}+\|\nabla^{2}u\|_{C_{\delta,\nu+2,\mu}^{0}(\mathcal{M}_{T})}\leq C\cdot\|\Delta u\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{T})}.

Step 1. (Weighted C1C^{1} and C2C^{2} estimates)

Now we start to prove the estimate (6.66), which will be proved by contradiction. Suppose no such a uniform constant C>0C>0 exists. That is, for fixed parameters

(6.68) βˆ’1<Ξ½<0,Ξ½+Ξ±<0,0<Ξ΄<Ξ΄N,ΞΌ=(1βˆ’1n)​(Ξ½+2+Ξ±),-1<\nu<0,\quad\nu+\alpha<0,\quad 0<\delta<\delta_{N},\quad\mu=(1-\frac{1}{n})(\nu+2+\alpha),

there are the following contradicting sequences:

  1. (1)

    A sequence of S1S^{1}-invariant KΓ€hler metrics gj=gTjg_{j}=g_{T_{j}} (or Ο‰j=Ο‰Tj\omega_{j}=\omega_{T_{j}}) on the neck β„³Tj\mathcal{M}_{T_{j}} constructed in Section 4.1 with Tjβ†’+∞T_{j}\to+\infty.

  2. (2)

    A sequence of C2,Ξ±C^{2,\alpha}-functions ujβˆˆπ”„u_{j}\in\mathfrak{A} satisfying

    (6.69) βˆ‚ujβˆ‚n|β„³j\displaystyle\frac{\partial u_{j}}{\partial n}\Big|_{\mathcal{M}_{j}} =0,\displaystyle=0,
    (6.70) β€–βˆ‡ujβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„³j)+β€–βˆ‡2ujβ€–CΞ΄,Ξ½+2,ΞΌ0​(β„³j)\displaystyle\|\nabla u_{j}\|_{C_{\delta,\nu+1,\mu}^{0}(\mathcal{M}_{j})}+\|\nabla^{2}u_{j}\|_{C_{\delta,\nu+2,\mu}^{0}(\mathcal{M}_{j})} =1,\displaystyle=1,
    (6.71) ‖Δ​ujβ€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³j)\displaystyle\|\Delta u_{j}\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{j})} β†’0,jβ†’+∞.\displaystyle\to 0,\quad j\to+\infty.

So it follows that either β€–βˆ‡ujβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„³j)β‰₯12\|\nabla u_{j}\|_{C_{\delta,\nu+1,\mu}^{0}(\mathcal{M}_{j})}\geq\frac{1}{2} or β€–βˆ‡2ujβ€–CΞ΄,Ξ½+2,ΞΌ0​(β„³j)β‰₯12\|\nabla^{2}u_{j}\|_{C_{\delta,\nu+2,\mu}^{0}(\mathcal{M}_{j})}\geq\frac{1}{2}. Without loss of generality, we only consider the first case and let 𝒙jβˆˆβ„³j\bm{x}_{j}\in\mathcal{M}_{j} satisfy

(6.72) |ρδ,Ξ½+1,ΞΌ(0)​(𝒙j)β‹…βˆ‡uj​(𝒙j)|=β€–βˆ‡ujβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„³j)β‰₯12.|\rho_{\delta,\nu+1,\mu}^{(0)}(\bm{x}_{j})\cdot\nabla u_{j}(\bm{x}_{j})|=\|\nabla u_{j}\|_{C_{\delta,\nu+1,\mu}^{0}(\mathcal{M}_{j})}\geq\frac{1}{2}.

Now we renormalize the functions uju_{j} as follows,

(6.73) vj​(𝒙)=uj​(𝒙)βˆ’uj​(𝒙j).v_{j}(\bm{x})=u_{j}(\bm{x})-u_{j}(\bm{x}_{j}).

Immediately, vj​(𝒙j)=0v_{j}(\bm{x}_{j})=0, βˆ‚vjβˆ‚n|β„³j=0\frac{\partial v_{j}}{\partial n}|_{\mathcal{M}_{j}}=0 and

(6.74) β€–βˆ‡vjβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„³j)\displaystyle\|\nabla v_{j}\|_{C_{\delta,\nu+1,\mu}^{0}(\mathcal{M}_{j})} =β€–βˆ‡ujβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„³j)≀1,\displaystyle=\|\nabla u_{j}\|_{C_{\delta,\nu+1,\mu}^{0}(\mathcal{M}_{j})}\leq 1,
(6.75) β€–βˆ‡2vjβ€–CΞ΄,Ξ½+2,ΞΌ0​(β„³j)\displaystyle\|\nabla^{2}v_{j}\|_{C_{\delta,\nu+2,\mu}^{0}(\mathcal{M}_{j})} =β€–βˆ‡2ujβ€–CΞ΄,Ξ½+2,ΞΌ0​(β„³j)≀1,\displaystyle=\|\nabla^{2}u_{j}\|_{C_{\delta,\nu+2,\mu}^{0}(\mathcal{M}_{j})}\leq 1,
(6.76) ‖Δ​vjβ€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³j)\displaystyle\|\Delta v_{j}\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{j})} =‖Δ​ujβ€–CΞ΄,Ξ½+2,ΞΌ0,α​(β„³j)β†’0,\displaystyle=\|\Delta u_{j}\|_{C_{\delta,\nu+2,\mu}^{0,\alpha}(\mathcal{M}_{j})}\to 0,
(6.77) β€–vjβ€–CΞ΄,Ξ½,ΞΌ0​(β„³j)\displaystyle\|v_{j}\|_{C_{\delta,\nu,\mu}^{0}(\mathcal{M}_{j})} ≀C0.\displaystyle\leq C_{0}.

So we are led to apply the weighted Schauder estimate in Proposition 6.9, which gives

(6.78) β€–vjβ€–CΞ΄,Ξ½,ΞΌ2,α​(β„³j)≀C0.\|v_{j}\|_{C_{\delta,\nu,\mu}^{2,\alpha}(\mathcal{M}_{j})}\leq C_{0}.

Moreover, it is straightforward that

(6.79) |ρδ,Ξ½+1,ΞΌ(0)​(𝒙j)β‹…βˆ‡vj​(𝒙j)|=β€–βˆ‡vjβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„³j)\displaystyle|\rho_{\delta,\nu+1,\mu}^{(0)}(\bm{x}_{j})\cdot\nabla v_{j}(\bm{x}_{j})|=\|\nabla v_{j}\|_{C_{\delta,\nu+1,\mu}^{0}(\mathcal{M}_{j})} β‰₯12.\displaystyle\geq\frac{1}{2}.

We will rescale contradicting spaces (β„³j,gj)(\mathcal{M}_{j},g_{j}) around the above reference points 𝒙j\bm{x}_{j} such that the desired contradiction will arise in the limiting space. Let gjg_{j} be a sequence of contradicting metrics, then we denote the rescaling factors as follows:

  1. (1)

    Rescaling of the metrics:

    Let g~j=Ξ»j2β‹…gj\tilde{g}_{j}=\lambda_{j}^{2}\cdot g_{j}, then with respect to the fixed reference point 𝒙jβˆˆβ„³j\bm{x}_{j}\in\mathcal{M}_{j} picked as the above, we have the convergence,

    (6.80) (β„³j,g~j,𝒙j)β†’G​H(X∞,d~∞,π’™βˆž).(\mathcal{M}_{j},\tilde{g}_{j},\bm{x}_{j})\xrightarrow{GH}(X_{\infty},\tilde{d}_{\infty},\bm{x}_{\infty}).
  2. (2)

    Rescaling of the solutions:

    Let ΞΊj>0\kappa_{j}>0 be a sequence of rescaling factors which will be determined later, such that

    (6.81) v~j≑κjβ‹…vj.\tilde{v}_{j}\equiv\kappa_{j}\cdot v_{j}.
  3. (3)

    Rescaling of the weight functions:

    Denote by ρ~j,Ξ΄,Ξ½,ΞΌ(k+Ξ±)\tilde{\rho}_{j,\delta,\nu,\mu}^{(k+\alpha)} and ρ~∞,Ξ΄,Ξ½,ΞΌ(k+Ξ±)\tilde{\rho}_{\infty,\delta,\nu,\mu}^{(k+\alpha)} the weight functions on the rescaled sequence (β„³j,g~j,𝒙j)(\mathcal{M}_{j},\tilde{g}_{j},\bm{x}_{j}) and the rescaled limit (X∞,g~∞,π’™βˆž)(X_{\infty},\tilde{g}_{\infty},\bm{x}_{\infty}) respectively. So we rescale the weight function ρj,Ξ΄,Ξ½,ΞΌ(k+Ξ±)\rho_{j,\delta,\nu,\mu}^{(k+\alpha)} by

    (6.82) ρ~j,Ξ΄,Ξ½,ΞΌ(k+Ξ±)=Ο„j⋅ρj,Ξ΄,Ξ½,ΞΌ(k+Ξ±).\tilde{\rho}_{j,\delta,\nu,\mu}^{(k+\alpha)}=\tau_{j}\cdot\rho_{j,\delta,\nu,\mu}^{(k+\alpha)}.

    Notice that the rescaling factor Ο„j\tau_{j} depends on kk and Ξ±\alpha.

In the following, we study the convergence of the renormalized functions v~jβˆˆπ”„\tilde{v}_{j}\in\mathfrak{A}, with respect to the rescaled metrics g~j\tilde{g}_{j}, in each region according to the subdivision given in Section 4.3. The main goal is to show v~βˆžβ‰‘0\tilde{v}_{\infty}\equiv 0 on the rescaled limit X∞X_{\infty} which gives the desired contradiction.

We will produce the desired contradiction in each region of 𝐈𝟏\bf{I}_{1}, 𝐈𝟐\bf{I}_{2}, πˆπŸ‘\bf{I}_{3} on β„³j\mathcal{M}_{j}. Before the detailed contradiction arguments, let us determine the rescaling factors in the following way. First, the scaling invariance requires

(6.83) Ο„jβ‹…ΞΊjΞ»jk+Ξ±=1.\frac{\tau_{j}\cdot\kappa_{j}}{\lambda_{j}^{k+\alpha}}=1.

Now we need to combing the regularity scale analysis in Proposition 4.18 and the choice of the weight function in Definition 4.19. So Ξ»j\lambda_{j}, Ο„j\tau_{j} and ΞΊj\kappa_{j} are determined as follows, which depends on if |z⁑(𝒙j)||z(\bm{x}_{j})| is uniformly bounded: First, if |z⁑(𝒙j)||z(\bm{x}_{j})| is uniformly bounded (corresponding to Region 𝐈𝟏\bf{I}_{1}, 𝐈𝟐\bf{I}_{2} and Case (a) of Region πˆπŸ‘\bf{I}_{3}), we choose

(6.84) {Ξ»j=𝔰jβˆ’1Ο„j=(𝔰jβˆ’1)Ξ½+k+Ξ±β‹…Tjβˆ’ΞΌΞΊj=(𝔰jβˆ’1)βˆ’Ξ½β‹…TjΞΌ.\displaystyle\begin{cases}\lambda_{j}=\mathfrak{s}_{j}^{-1}\\ \tau_{j}=(\mathfrak{s}_{j}^{-1})^{\nu+k+\alpha}\cdot T_{j}^{-\mu}\\ \kappa_{j}=(\mathfrak{s}_{j}^{-1})^{-\nu}\cdot T_{j}^{\mu}.\end{cases}

Next, if |z⁑(𝒙j)|β†’+∞|z(\bm{x}_{j})|\to+\infty (corresponding to Case (b) and Case (c) of Region πˆπŸ‘\bf{I}_{3}), we choose

(6.85) {Ξ»j=𝔰jβˆ’1Ο„j=(𝔰jβˆ’1)Ξ½+k+Ξ±β‹…eβˆ’Tjβ‹…Tjβˆ’ΞΌΞΊj=(𝔰jβˆ’1)βˆ’Ξ½β‹…eTjβ‹…TjΞΌ.\displaystyle\begin{cases}\lambda_{j}=\mathfrak{s}_{j}^{-1}\\ \tau_{j}=(\mathfrak{s}_{j}^{-1})^{\nu+k+\alpha}\cdot e^{-T_{j}}\cdot T_{j}^{-\mu}\\ \kappa_{j}=(\mathfrak{s}_{j}^{-1})^{-\nu}\cdot e^{T_{j}}\cdot T_{j}^{\mu}.\end{cases}

In this case, we need to rescale the zz-coordinate in the meanwhile so that the exponential term shows up in the rescaling factors.

Region 𝐈𝟏\bf{I}_{1} (The deepest bubble):

In this case, we consider that the reference points 𝒙j\bm{x}_{j} are in Region 𝐈𝟏\bf{I}_{1}. According to the discussions in Section 4.3, for any 0<Ξ³<10<\gamma<1, (β„³j,g~j,𝒙j)(\mathcal{M}_{j},\tilde{g}_{j},\bm{x}_{j}) converges to the following Riemann product in the C2,Ξ³C^{2,\gamma}-topology,

(6.86) (β„³j,g~j,𝒙j)β†’C2,Ξ³(β„‚T​N2Γ—β„‚nβˆ’2,g~∞,π’™βˆž),(\mathcal{M}_{j},\tilde{g}_{j},\bm{x}_{j})\xrightarrow{C^{2,\gamma}}(\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2},\tilde{g}_{\infty},\bm{x}_{\infty}),

where g~βˆžβ‰‘gT​NβŠ•gβ„‚nβˆ’2\tilde{g}_{\infty}\equiv g_{TN}\oplus g_{\mathbb{C}^{n-2}} is the product metric of the Taub-NUT metric gT​Ng_{TN} and the Euclidean metric gβ„‚nβˆ’2g_{\mathbb{C}^{n-2}}. Moreover, the rescaled weight function will converge to

(6.87) ρ~∞,Ξ΄,Ξ½,ΞΌ(k+Ξ±)​(𝒙)={1,π’™βˆˆT1​(Ξ£0),(dg~βˆžβ€‹(𝒙,Ξ£0))Ξ½+k+Ξ±,π’™βˆˆ(β„‚T​N2Γ—β„‚nβˆ’2)βˆ–T1​(Ξ£0),\displaystyle\tilde{\rho}_{\infty,\delta,\nu,\mu}^{(k+\alpha)}(\bm{x})=\begin{cases}1,&\bm{x}\in T_{1}(\Sigma_{0}),\\ (d_{\tilde{g}_{\infty}}(\bm{x},\Sigma_{0}))^{\nu+k+\alpha},&\bm{x}\in(\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2})\setminus T_{1}(\Sigma_{0}),\end{cases}

where Ξ£0≑{p∞}Γ—β„‚nβˆ’2βŠ‚β„‚T​N2Γ—β„‚nβˆ’2\Sigma_{0}\equiv\{p_{\infty}\}\times\mathbb{C}^{n-2}\subset\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2} for some pβˆžβˆˆβ„‚T​N2p_{\infty}\in\mathbb{C}_{TN}^{2}, is the Gromov-Hausdorff limit of the lifted divisor π’«β‰‘Ο€βˆ’1​(P)βŠ‚β„³j\mathcal{P}\equiv\pi^{-1}(P)\subset\mathcal{M}_{j} with respect to the rescaled metrics g~j\tilde{g}_{j} such that and

(6.88) T1​(Ξ£0)≑{π’™βˆˆβ„‚T​N2Γ—β„‚nβˆ’2|dg~βˆžβ€‹(𝒙,Ξ£0)≀1}.T_{1}(\Sigma_{0})\equiv\{\bm{x}\in\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2}|d_{\tilde{g}_{\infty}}(\bm{x},\Sigma_{0})\leq 1\}.

It is straightforward that, the rescaled functions v~j\tilde{v}_{j} converge to v~∞\tilde{v}_{\infty} in the C2,Ξ±β€²C^{2,\alpha^{\prime}}-topology for each 0<Ξ±β€²<Ξ±0<\alpha^{\prime}<\alpha such that the following properties hold,

  1. (1)

    β€–βˆ‡v~βˆžβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„‚T​N2Γ—β„‚nβˆ’2,g~∞)+β€–βˆ‡2v~βˆžβ€–CΞ΄,Ξ½+2,ΞΌ0​(β„‚T​N2Γ—β„‚nβˆ’2,g~∞)=1\|\nabla\tilde{v}_{\infty}\|_{C_{\delta,\nu+1,\mu}^{0}(\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2},\tilde{g}_{\infty})}+\|\nabla^{2}\tilde{v}_{\infty}\|_{C_{\delta,\nu+2,\mu}^{0}(\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2},\tilde{g}_{\infty})}=1,

  2. (2)

    v~βˆžβ€‹(π’™βˆž)=0\tilde{v}_{\infty}(\bm{x}_{\infty})=0,

  3. (3)

    Ξ”g~βˆžβ€‹v~βˆžβ‰‘0\Delta_{\tilde{g}_{\infty}}\tilde{v}_{\infty}\equiv 0 on β„‚T​N2Γ—β„‚nβˆ’2\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2}.

We will prove that v~βˆžβ‰‘0\tilde{v}_{\infty}\equiv 0 on β„‚T​N2Γ—β„‚nβˆ’2\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2}.

To start with, we will show that v~∞\tilde{v}_{\infty} is constant on the Euclidean factor β„‚nβˆ’2\mathbb{C}^{n-2}. Indeed, we write 𝒙≑(𝒙′,𝒙′′)βˆˆβ„‚T​N2Γ—β„‚nβˆ’2\bm{x}\equiv(\bm{x}^{\prime},\bm{x}^{\prime\prime})\in\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2}, so it suffices to prove that for every 1≀k≀2​nβˆ’41\leq k\leq 2n-4, we have

(6.89) |βˆ‡kv~∞|≑0​on​ℂnβˆ’2,|\nabla_{k}\tilde{v}_{\infty}|\equiv 0\ \text{on}\ \mathbb{C}^{n-2},

where the partial derivative βˆ‡kv~βˆžβ€‹(𝒙)β‰‘βˆ‚v~βˆžβˆ‚xk′′​(𝒙′,𝒙′′)\nabla_{k}\tilde{v}_{\infty}(\bm{x})\equiv\frac{\partial\tilde{v}_{\infty}}{\partial x_{k}^{\prime\prime}}(\bm{x}^{\prime},\bm{x}^{\prime\prime}) is taken in the directions of β„‚nβˆ’2\mathbb{C}^{n-2}. Now for every 1≀k≀2​nβˆ’41\leq k\leq 2n-4,

(6.90) Ξ”g~βˆžβ€‹(βˆ‡kv~∞)=Ξ”β„‚T​N2​(βˆ‡kv~∞)+Ξ”β„‚nβˆ’2​(βˆ‡kv~∞).\Delta_{\tilde{g}_{\infty}}(\nabla_{k}\tilde{v}_{\infty})=\Delta_{\mathbb{C}_{TN}^{2}}(\nabla_{k}\tilde{v}_{\infty})+\Delta_{\mathbb{C}^{n-2}}(\nabla_{k}\tilde{v}_{\infty}).

Notice that g~∞=gT​NβŠ•gβ„‚nβˆ’2\tilde{g}_{\infty}=g_{TN}\oplus g_{\mathbb{C}^{n-2}} is a product metric and βˆ‡k\nabla_{k} in effect acts on the Euclidean factor β„‚nβˆ’2\mathbb{C}^{n-2}, so βˆ‡k\nabla_{k} commutes with both Ξ”β„‚T​N2\Delta_{\mathbb{C}_{TN}^{2}} and Ξ”β„‚nβˆ’2\Delta_{\mathbb{C}^{n-2}}. Therefore,

(6.91) Ξ”g~βˆžβ€‹(βˆ‡kv~∞)=βˆ‡k(Ξ”β„‚T​N2​v~∞+Ξ”β„‚nβˆ’2​v~∞)=0.\displaystyle\Delta_{\tilde{g}_{\infty}}(\nabla_{k}\tilde{v}_{\infty})=\nabla_{k}(\Delta_{\mathbb{C}_{TN}^{2}}\tilde{v}_{\infty}+\Delta_{\mathbb{C}^{n-2}}\tilde{v}_{\infty})=0.

The weighted bound implies the estimates

(6.92) {|βˆ‡kv~βˆžβ€‹(𝒙)|≀1,dg~βˆžβ€‹(𝒙,Ξ£0)≀1,|βˆ‡kv~βˆžβ€‹(𝒙)|≀dg~βˆžβ€‹(𝒙,Ξ£0)βˆ’(Ξ½+1),dg~βˆžβ€‹(𝒙,Ξ£0)β‰₯1.\displaystyle\begin{cases}|\nabla_{k}\tilde{v}_{\infty}(\bm{x})|\leq 1,&d_{\tilde{g}_{\infty}}(\bm{x},\Sigma_{0})\leq 1,\\ |\nabla_{k}\tilde{v}_{\infty}(\bm{x})|\leq d_{\tilde{g}_{\infty}}(\bm{x},\Sigma_{0})^{-(\nu+1)},&d_{\tilde{g}_{\infty}}(\bm{x},\Sigma_{0})\geq 1.\end{cases}

Since we have assumed ν∈(βˆ’1,0)\nu\in(-1,0), so it is straightforward

(6.93) βˆ’(Ξ½+1)∈(βˆ’1,0).-(\nu+1)\in(-1,0).

The above implies that |βˆ‡kv~∞|≀1|\nabla_{k}\tilde{v}_{\infty}|\leq 1 on β„‚T​N2Γ—β„‚nβˆ’2\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2}. Applying Cheng-Yau’s gradient estimate to the harmonic function βˆ‡kv~∞\nabla_{k}\tilde{v}_{\infty} on the Ricci-flat manifold β„‚T​N2Γ—β„‚nβˆ’2\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2}, we conclude that βˆ‡kv~∞\nabla_{k}\tilde{v}_{\infty} is constant on β„‚T​N2Γ—β„‚nβˆ’2\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2}. By (6.92), βˆ‡kv~βˆžβ‰‘0\nabla_{k}\tilde{v}_{\infty}\equiv 0 for every 1≀k≀2​nβˆ’41\leq k\leq 2n-4. Therefore, v~∞\tilde{v}_{\infty} is constant on the Euclidean factor β„‚nβˆ’2\mathbb{C}^{n-2}.

By the above argument, the limiting function v~∞\tilde{v}_{\infty} can be viewed as a harmonic function on the Ricci-flat Taub-NUT space (β„‚T​N2,gT​N)(\mathbb{C}_{TN}^{2},g_{TN}). Now applying Bochner’s formula,

(6.94) 12​ΔgT​N​|βˆ‡gT​Nv~∞|2=|βˆ‡gT​N2v~∞|2β‰₯0.\frac{1}{2}\Delta_{g_{TN}}|\nabla_{g_{TN}}\tilde{v}_{\infty}|^{2}=|\nabla_{g_{TN}}^{2}\tilde{v}_{\infty}|^{2}\geq 0.

Since v~∞\tilde{v}_{\infty} satisfies the weighted bound

(6.95) β€–βˆ‡gT​Nv~βˆžβ€–CΞ΄,Ξ½+1,ΞΌ0​(β„‚T​N2)+β€–βˆ‡gT​N2v~βˆžβ€–CΞ΄,Ξ½+2,ΞΌ0​(β„‚T​N2)=1,\|\nabla_{g_{TN}}\tilde{v}_{\infty}\|_{C_{\delta,\nu+1,\mu}^{0}(\mathbb{C}_{TN}^{2})}+\|\nabla_{g_{TN}}^{2}\tilde{v}_{\infty}\|_{C_{\delta,\nu+2,\mu}^{0}(\mathbb{C}_{TN}^{2})}=1,

so we have for any π’™βˆˆβ„‚T​N2βˆ–B1​(π’™βˆž)\bm{x}\in\mathbb{C}_{TN}^{2}\setminus B_{1}(\bm{x}_{\infty}),

(6.96) |βˆ‡gT​Nv~βˆžβ€‹(𝒙)|≀dgT​N​(𝒙,π’™βˆž)βˆ’(Ξ½+1).|\nabla_{g_{TN}}\tilde{v}_{\infty}(\bm{x})|\leq d_{g_{TN}}(\bm{x},\bm{x}_{\infty})^{-(\nu+1)}.

By assumption ν∈(βˆ’1,0)\nu\in(-1,0), then |βˆ‡gT​Nv~∞|≑0|\nabla_{g_{TN}}\tilde{v}_{\infty}|\equiv 0 on β„‚T​N2\mathbb{C}_{TN}^{2} and hence v~∞\tilde{v}_{\infty} is constant on β„‚T​N2\mathbb{C}_{TN}^{2}. Notice that v~βˆžβ€‹(π’™βˆž)=0\tilde{v}_{\infty}(\bm{x}_{\infty})=0, so we conclude that v~βˆžβ€‹(π’™βˆž)≑0\tilde{v}_{\infty}(\bm{x}_{\infty})\equiv 0.

Region 𝐈𝟐\bf{I}_{2} (bubble transformations):

Now we separate the proof in 33 cases:

  1. (a)

    There is some Οƒ0>0\sigma_{0}>0 such that

    (6.97) Ξ»jβ‹…Tjβˆ’12β‰₯Οƒ0.\lambda_{j}\cdot T_{j}^{-\frac{1}{2}}\geq\sigma_{0}.
  2. (b)

    Assume that rjr_{j} satisfies the following condition holds,

    (6.98) Ξ»jβ‹…Tjβˆ’12β†’0,Ξ»jβ‹…Tj12β†’βˆž.\lambda_{j}\cdot T_{j}^{-\frac{1}{2}}\to 0,\ \lambda_{j}\cdot T_{j}^{\frac{1}{2}}\to\infty.
  3. (c)

    Assume that there is some C0>0C_{0}>0 such that Ξ»jβ‹…Tj12≀C0\lambda_{j}\cdot T_{j}^{\frac{1}{2}}\leq C_{0}.

Case (a):

In this case, the rescaled limit is the Riemann product β„‚T​N,Οƒ2Γ—β„‚nβˆ’2\mathbb{C}_{TN,\sigma}^{2}\times\mathbb{C}^{n-2}, where β„‚T​N,Οƒ2\mathbb{C}_{TN,\sigma}^{2} is the Taub-NUT space and the length of the circle fiber at infinity equals Οƒβˆˆ[Οƒ0,1]\sigma\in[\sigma_{0},1]. The remainder of the proof is the same as that in Region 𝐈𝟏\bf{I}_{1}, so we omit it.

Case (b):

In this case, the rescaled spaces (β„³j,g~j,𝒙j)(\mathcal{M}_{j},\tilde{g}_{j},\bm{x}_{j}) converge to the product Euclidean space (ℝ3Γ—β„‚nβˆ’2,g0,π’™βˆž)(\mathbb{R}^{3}\times\mathbb{C}^{n-2},g_{0},\bm{x}_{\infty}) in the pointed Gromov-Hausdorff topology, i.e.,

(6.99) (β„³j,g~j,𝒙j)β†’G​H(ℝ3Γ—β„‚nβˆ’2,g0,π’™βˆž),(\mathcal{M}_{j},\tilde{g}_{j},\bm{x}_{j})\xrightarrow{GH}(\mathbb{R}^{3}\times\mathbb{C}^{n-2},g_{0},\bm{x}_{\infty}),

where the metric g0g_{0} is the standard Euclidean metric on ℝ3Γ—β„‚nβˆ’2\mathbb{R}^{3}\times\mathbb{C}^{n-2}. In this rescaled limit, the limiting reference point π’™βˆž\bm{x}_{\infty} satisfies dg0​(π’™βˆž,Ξ£03)=1d_{g_{0}}(\bm{x}_{\infty},\Sigma_{0^{3}})=1 and Ξ£03≑{03}Γ—β„‚nβˆ’2βŠ‚β„3Γ—β„‚nβˆ’2\Sigma_{0^{3}}\equiv\{0^{3}\}\times\mathbb{C}^{n-2}\subset\mathbb{R}^{3}\times\mathbb{C}^{n-2} is the singular slice. Moreover, the convergence keeps curvatures uniformly bounded away from the singular slice Ξ£03\Sigma_{0^{3}}. By passing to the local universal covers, in fact one can show that, away from Ξ£03βŠ‚β„3Γ—β„‚nβˆ’2\Sigma_{0^{3}}\subset\mathbb{R}^{3}\times\mathbb{C}^{n-2}, the rescaled contradicting functions v~j\tilde{v}_{j} converge to v~∞\tilde{v}_{\infty} in the C2,Ξ±β€²C^{2,\alpha^{\prime}}-topology for each 0<Ξ±β€²<Ξ±<10<\alpha^{\prime}<\alpha<1, such that the following properties hold,

  1. (1)

    β€–βˆ‡v~βˆžβ€–CΞ΄,Ξ½+1,ΞΌ0​(ℝ3Γ—β„‚nβˆ’2)+β€–βˆ‡2v~βˆžβ€–CΞ΄,Ξ½+2,ΞΌ0​(ℝ3Γ—β„‚nβˆ’2)=1\|\nabla\tilde{v}_{\infty}\|_{C_{\delta,\nu+1,\mu}^{0}(\mathbb{R}^{3}\times\mathbb{C}^{n-2})}+\|\nabla^{2}\tilde{v}_{\infty}\|_{C_{\delta,\nu+2,\mu}^{0}(\mathbb{R}^{3}\times\mathbb{C}^{n-2})}=1,

  2. (2)

    v~βˆžβ€‹(π’™βˆž)=0\tilde{v}_{\infty}(\bm{x}_{\infty})=0,

  3. (3)

    Ξ”g~βˆžβ€‹v~βˆžβ‰‘0\Delta_{\tilde{g}_{\infty}}\tilde{v}_{\infty}\equiv 0 in (ℝ3Γ—β„‚nβˆ’2)βˆ–Ξ£03(\mathbb{R}^{3}\times\mathbb{C}^{n-2})\setminus\Sigma_{0^{3}},

where the limiting weight function is

(6.100) ρ∞,Ξ΄,Ξ½,ΞΌ(k+Ξ±)​(𝒙)=(dg0​(𝒙,Ξ£03))Ξ½+k+Ξ±,π’™βˆˆβ„3Γ—β„‚nβˆ’2.\rho_{\infty,\delta,\nu,\mu}^{(k+\alpha)}(\bm{x})=(d_{g_{0}}(\bm{x},\Sigma_{0^{3}}))^{\nu+k+\alpha},\ \bm{x}\in\mathbb{R}^{3}\times\mathbb{C}^{n-2}.

Our goal is to show that v~βˆžβ‰‘0\tilde{v}_{\infty}\equiv 0 on ℝ3Γ—β„‚nβˆ’2\mathbb{R}^{3}\times\mathbb{C}^{n-2}, which consists of the following ingredients:

First, we will prove that v~∞\tilde{v}_{\infty} in fact globally harmonic in ℝ3Γ—β„‚nβˆ’2\mathbb{R}^{3}\times\mathbb{C}^{n-2}. To show the singular slice Ξ£03\Sigma_{0^{3}} is removable, for each q∈Σ03q\in\Sigma_{0^{3}}, we take a unit ball B1​(q)βŠ‚Ξ£03B_{1}(q)\subset\Sigma_{0^{3}}, and for any r∈(0,1)r\in(0,1), we choose the tubular neighborhood Tr​(B1​(q))βŠ‚β„3Γ—β„‚nβˆ’2T_{r}(B_{1}(q))\subset\mathbb{R}^{3}\times\mathbb{C}^{n-2}. Notice that βˆ‡v~∞\nabla\tilde{v}_{\infty} satisfies the uniform estimate

(6.101) β€–βˆ‡v~βˆžβ€–CΞ΄,Ξ½+1,ΞΌ0​(ℝ3Γ—β„‚nβˆ’2)≀1,\|\nabla\tilde{v}_{\infty}\|_{C_{\delta,\nu+1,\mu}^{0}(\mathbb{R}^{3}\times\mathbb{C}^{n-2})}\leq 1,

integrating the above weighted bound, then for any π’™βˆˆTr​(B1​(q))βˆ–B1​(q)\bm{x}\in T_{r}(B_{1}(q))\setminus B_{1}(q),

(6.102) |v~βˆžβ€‹(𝒙)|≀Cβ‹…d​(𝒙,B1​(q))βˆ’(Ξ½).|\tilde{v}_{\infty}(\bm{x})|\leq C\cdot d(\bm{x},B_{1}(q))^{-(\nu)}.

By Lemma 6.5, B1​(q)B_{1}(q) is a removable singular set in Tr​(B1​(q))T_{r}(B_{1}(q)) and hence v~∞\tilde{v}_{\infty} is harmonic in Tr​(B1​(q))T_{r}(B_{1}(q)).

Next, we will show that v~∞\tilde{v}_{\infty} is constant in β„‚nβˆ’2\mathbb{C}^{n-2}. It is straightforward that for each 1≀k≀2​nβˆ’41\leq k\leq 2n-4, the partial derivative βˆ‡kv~βˆžβ‰‘βˆ‚βˆ‚xk′′​v~βˆžβ€‹(𝒙′,𝒙′′)\nabla_{k}\tilde{v}_{\infty}\equiv\frac{\partial}{\partial x_{k}^{\prime\prime}}\tilde{v}_{\infty}(\bm{x}^{\prime},\bm{x}^{\prime\prime}) satisfies

(6.103) Ξ”g0​(βˆ‡kv~∞)=0​in​ℝ3Γ—β„‚nβˆ’2.\Delta_{g_{0}}(\nabla_{k}\tilde{v}_{\infty})=0\ \text{in}\ \mathbb{R}^{3}\times\mathbb{C}^{n-2}.

The weighted condition implies that βˆ‡kv~∞\nabla_{k}\tilde{v}_{\infty} satisfies the uniform estimate,

(6.104) |βˆ‡kv~∞|≀d​(𝒙,Ξ£03)βˆ’(Ξ½+1),βˆ€π’™βˆˆβ„3Γ—β„‚nβˆ’2.|\nabla_{k}\tilde{v}_{\infty}|\leq d(\bm{x},\Sigma_{0^{3}})^{-(\nu+1)},\forall\bm{x}\in\mathbb{R}^{3}\times\mathbb{C}^{n-2}.

Since we have assumed ν∈(βˆ’1,0)\nu\in(-1,0), Lemma 6.6 implies that |βˆ‡kv~∞|≑0|\nabla_{k}\tilde{v}_{\infty}|\equiv 0 on ℝ3Γ—β„‚nβˆ’2\mathbb{R}^{3}\times\mathbb{C}^{n-2} and hence v~∞\tilde{v}_{\infty} is constant in β„‚nβˆ’2\mathbb{C}^{n-2}. Therefore, v~∞\tilde{v}_{\infty} can be viewed as a harmonic function in the Euclidean space (ℝ3,gℝ3)(\mathbb{R}^{3},g_{\mathbb{R}^{3}}). By assumption, v~∞\tilde{v}_{\infty} satisfies

(6.105) |v~βˆžβ€‹(𝒙)|≀dgℝ3​(𝒙,03)βˆ’Ξ½.|\tilde{v}_{\infty}(\bm{x})|\leq d_{g_{\mathbb{R}^{3}}}(\bm{x},0^{3})^{-\nu}.

Since ν∈(βˆ’1,0)\nu\in(-1,0), applying the standard Liouville theorem for sublinear growth harmonic functions on a Euclidean space, we conclude that v~∞\tilde{v}_{\infty} is a constant. The last step is to use the renormalization v~βˆžβ€‹(π’™βˆž)=0\tilde{v}_{\infty}(\bm{x}_{\infty})=0, then v~βˆžβ‰‘0\tilde{v}_{\infty}\equiv 0.

Case (c):

The rescaled limit is the cylinder (Q,gc)≑(D×ℝ,gDβŠ•d​z2)(Q,g_{c})\equiv(D\times\mathbb{R},g_{D}\oplus dz^{2}), where (D,gD)(D,g_{D}) is a closed Calabi-Yau manifold. The limiting solutions v~∞\tilde{v}_{\infty} satisfies

  1. (1)

    β€–βˆ‡v~βˆžβ€–CΞ΄,Ξ½+1,ΞΌ0​(Q)+β€–βˆ‡2v~βˆžβ€–CΞ΄,Ξ½+2,ΞΌ0​(Q)=1\|\nabla\tilde{v}_{\infty}\|_{C_{\delta,\nu+1,\mu}^{0}(Q)}+\|\nabla^{2}\tilde{v}_{\infty}\|_{C_{\delta,\nu+2,\mu}^{0}(Q)}=1,

  2. (2)

    v~βˆžβ€‹(π’™βˆž)=0\tilde{v}_{\infty}(\bm{x}_{\infty})=0,

  3. (3)

    Ξ”g~βˆžβ€‹v~βˆžβ‰‘0\Delta_{\tilde{g}_{\infty}}\tilde{v}_{\infty}\equiv 0 in Qβˆ–PQ\setminus P,

where the limiting weight function is

(6.106) ρ~∞,Ξ΄,Ξ½,ΞΌ(k+Ξ±)​(𝒙)={eΞ΄β‹…z⁑(𝒙)⋅𝔯​(𝒙)Ξ½+k+Ξ±,z⁑(𝒙)>0eβˆ’Ξ΄β‹…z(𝒙)⋅𝔯(𝒙)Ξ½+k+Ξ±,z⁑(𝒙)≀0.\displaystyle\tilde{\rho}_{\infty,\delta,\nu,\mu}^{(k+\alpha)}(\bm{x})=\begin{cases}e^{\delta\cdot z(\bm{x})}\cdot\mathfrak{r}(\bm{x})^{\nu+k+\alpha},&z(\bm{x})>0\\ e^{-\delta\cdot z(\bm{x})}\cdot\mathfrak{r}(\bm{x})^{\nu+k+\alpha},&z(\bm{x})\leq 0.\end{cases}

Similar to Case (b), first we need to extend the limiting function v~∞\tilde{v}_{\infty} across the singular set PP. Integrating βˆ‡v~∞\nabla\tilde{v}_{\infty} around PP, we have that v~∞\tilde{v}_{\infty} satisfies the growth estimate

(6.107) |v~βˆžβ€‹(𝒙)|≀Cβ‹…dgc​(𝒙,P)βˆ’Ξ½.|\tilde{v}_{\infty}(\bm{x})|\leq C\cdot d_{g_{c}}(\bm{x},P)^{-\nu}.

Since we have assumed ν∈(βˆ’1,0)\nu\in(-1,0), so Lemma 6.5 implies that the singular set PP is removable. Now we have obtained that v~∞\tilde{v}_{\infty} is harmonic on QQ and satisfies

(6.108) |v~∞(𝒙)|≀Ceβˆ’Ξ΄β‹…|z(𝒙)|,|\tilde{v}_{\infty}(\bm{x})|\leq Ce^{-\delta\cdot|z(\bm{x})|},

for |z⁑(𝒙)||z(\bm{x})| large. Therefore, v~βˆžβ‰‘0\tilde{v}_{\infty}\equiv 0 on QQ which completes the proof of Case (c).

Region πˆπŸ‘\bf{I}_{3} (the cylindrical bubble and the boundary behavior):

In this region, the rescaling factors of the metrics gjg_{j} are chosen such that the rescaled Gromov-Hausdorff limit is the cylinder Q≑D×ℝQ\equiv D\times\mathbb{R}. Let ΞΆj≑z⁑(𝒙j)\zeta_{j}\equiv z(\bm{x}_{j}), then there are two different cases to analyze which depends on if the convergence keeps curvatures uniformly bounded.

  1. (a)

    Assume that there is some ΞΆ0>0\zeta_{0}>0 such that |zj|≀΢0|z_{j}|\leq\zeta_{0}.

  2. (b)

    Assume that zjz_{j} satisfies

    (6.109) |ΞΆj|β†’βˆž,Tjnβˆ’2nLTj​(zj)β†’0.|\zeta_{j}|\to\infty,\ \frac{T_{j}^{\frac{n-2}{n}}}{L_{T_{j}}(z_{j})}\to 0.
  3. (c)

    Assume that zjz_{j} satisfies

    (6.110) c0≀Tjnβˆ’2nLTj​(zj)≀1.\displaystyle c_{0}\leq\frac{T_{j}^{\frac{n-2}{n}}}{L_{T_{j}}(z_{j})}\leq 1.

Case (a):

So the rescaled spaces (β„³j,g~j,𝒙j)(\mathcal{M}_{j},\tilde{g}_{j},\bm{x}_{j}) converge to the cylinder (Q,gc)=(D2​n×ℝ,gD2​nβŠ•d​z2)(Q,g_{c})=(D^{2n}\times\mathbb{R},g_{D^{2n}}\oplus dz^{2}) and the sequence has uniformly bounded geometry away from Qβˆ–π’«Q\setminus\mathcal{P}. Moreover, the weight function in the rescaled limit space is

(6.111) ρ~∞,Ξ΄,Ξ½,ΞΌ(k+Ξ±)​(𝒙)={eΞ΄β‹…z⁑(𝒙)⋅𝔯​(𝒙)Ξ½+k+Ξ±,z⁑(𝒙)>0eβˆ’Ξ΄β‹…z(𝒙)⋅𝔯(𝒙)Ξ½+k+Ξ±,z⁑(𝒙)≀0.\displaystyle\tilde{\rho}_{\infty,\delta,\nu,\mu}^{(k+\alpha)}(\bm{x})=\begin{cases}e^{\delta\cdot z(\bm{x})}\cdot\mathfrak{r}(\bm{x})^{\nu+k+\alpha},&z(\bm{x})>0\\ e^{-\delta\cdot z(\bm{x})}\cdot\mathfrak{r}(\bm{x})^{\nu+k+\alpha},&z(\bm{x})\leq 0.\end{cases}

The rest of the proof is the same as Case (c) in Region II.

Case (b) in Region πˆπŸ‘\bf{I}_{3}

In this case, the reference point 𝒙j\bm{x}_{j} satisfies

(6.112) |z⁑(𝒙j)|β†’βˆž,Tjnβˆ’2nLTj​(zj)β†’0.|z(\bm{x}_{j})|\to\infty,\quad\frac{T_{j}^{\frac{n-2}{n}}}{L_{T_{j}}(z_{j})}\to 0.

In addition, we also need to perform the coordinate change centered at the reference point 𝒙j\bm{x}_{j},

(6.113) z⁑(𝒙)=zj+(TjLTj​(zj))nβˆ’22​w​(𝒙).z(\bm{x})=z_{j}+\Big(\frac{T_{j}}{L_{T_{j}}(z_{j})}\Big)^{\frac{n-2}{2}}w(\bm{x}).

In the following, we only consider the case zjβ‰ͺ0z_{j}\ll 0. It is shown in Section 4.3 that the rescaled limit is isometric to a cylinder Q=D×ℝQ=D\times\mathbb{R} with a product metric

(6.114) gQ=gD+d​w2.g_{Q}=g_{D}+dw^{2}.

Moreover, as Tjβ†’+∞T_{j}\to+\infty, the rescaled weight function limits to

(6.115) ρ~∞,Ξ΄,Ξ½,ΞΌ(k+Ξ±)(𝒙)=eβˆ’Ξ΄β‹…nβ‹…kβˆ’2β‹…w(𝒙).\tilde{\rho}_{\infty,\delta,\nu,\mu}^{(k+\alpha)}(\bm{x})=e^{-\frac{\delta\cdot n\cdot k_{-}}{2}\cdot w(\bm{x})}.

Now the growth condition implies that the limiting function v~∞\tilde{v}_{\infty} satisfies

(6.116) {Ξ”Q​v~βˆžβ€‹(𝒙)=0,βˆ€π’™βˆˆQ,|v~βˆžβ€‹(𝒙)|≀eΞ΄β‹…nβ‹…kβˆ’2β‹…w⁑(𝒙),wβˆˆβ„.\displaystyle\begin{cases}\Delta_{Q}\tilde{v}_{\infty}(\bm{x})=0,&\forall\bm{x}\in Q,\\ |\tilde{v}_{\infty}(\bm{x})|\leq e^{\frac{\delta\cdot n\cdot k_{-}}{2}\cdot w(\bm{x})},&w\in\mathbb{R}.\end{cases}

By the choice of the parameter Ξ΄\delta in (6.12),

(6.117) Ξ΄β‹…nβ‹…kβˆ’2<Ξ»D2.\frac{\delta\cdot n\cdot k_{-}}{2}<\frac{\sqrt{\lambda_{D}}}{2}.

Applying Lemma 6.7, for every π’™βˆˆQ\bm{x}\in Q,

(6.118) v~βˆžβ€‹(𝒙)=0.\tilde{v}_{\infty}(\bm{x})=0.

So the proof of Case (b) is done.

Case (c) in Region πˆπŸ‘\bf{I}_{3}

In this case, the reference point 𝒙j\bm{x}_{j} is close to the boundary such that Neumann boundary condition plays a crucial role. Precisely, the scale condition is given by the following: there is some c0>0c_{0}>0 such that

(6.119) c0≀Tjnβˆ’2nLTj​(zj)≀1.\displaystyle c_{0}\leq\frac{T_{j}^{\frac{n-2}{n}}}{L_{T_{j}}(z_{j})}\leq 1.

We can assume that zjβ‰ͺ0z_{j}\ll 0 and passing to a subsequence, there is some constant 𝔠0∈[c0,1]\mathfrak{c}_{0}\in[c_{0},1] such that

(6.120) Tjnβˆ’2nLTj​(zj)→𝔠0.\frac{T_{j}^{\frac{n-2}{n}}}{L_{T_{j}}(z_{j})}\to\mathfrak{c}_{0}.

For the convenience of the computations, we will perform the coordinate change centered at the boundary slice, that is,

(6.121) z⁑(𝒙)=Tβˆ’+(TjLTj​(zj))nβˆ’22​w​(𝒙).z(\bm{x})=T_{-}+\Big(\frac{T_{j}}{L_{T_{j}}(z_{j})}\Big)^{\frac{n-2}{2}}w(\bm{x}).

We have computed in Section 4.3 that the limit of the rescaled spaces (β„³T,g~j,𝒙j)(\mathcal{M}_{T},\tilde{g}_{j},\bm{x}_{j}) is the Calabi model space (π’žβˆ’n,gπ’žβˆ’n,π’™βˆž)(\mathcal{C}^{n}_{-},g_{\mathcal{C}^{n}_{-}},\bm{x}_{\infty}). Moreover, the limiting weight function is

(6.122) ρ~∞,Ξ΄,Ξ½,ΞΌ(k+Ξ±)(𝒙)=eβˆ’Ξ΄β‹…π” 0n2β‹…Pn2(w)β‹…(Pn2(w))Ξ½+k+Ξ±2,\tilde{\rho}_{\infty,\delta,\nu,\mu}^{(k+\alpha)}(\bm{x})=e^{-\delta\cdot\mathfrak{c}_{0}^{\frac{n}{2}}\cdot P_{{\frac{n}{2}}}(w)}\cdot(P_{\frac{n}{2}}(w))^{\frac{\nu+k+\alpha}{2}},

where

(6.123) Pn2​(w)≑(1+kβˆ’β€‹π” 0n2​w)n2.P_{{\frac{n}{2}}}(w)\equiv(1+k_{-}\mathfrak{c}_{0}^{\frac{n}{2}}w)^{\frac{n}{2}}.

Since 𝔠0∈[c0,1]\mathfrak{c}_{0}\in[c_{0},1], so the limiting function v~∞\tilde{v}_{\infty} satisfies

(6.124) {Ξ”gπ’žβˆ’n​v~∞=0,π’™βˆˆπ’žβˆ’n,|v~βˆžβ€‹(𝒙)|≀eΞ΄β‹…(kβˆ’)n2β‹…wn2β‹…Pn2​(w)βˆ’Ξ½2,w⁑(𝒙)≫1,βˆ‚v~βˆžβˆ‚w=0,w⁑(𝒙)=w0.\displaystyle\begin{cases}\Delta_{g_{\mathcal{C}_{-}^{n}}}\tilde{v}_{\infty}=0,&\bm{x}\in\mathcal{C}_{-}^{n},\\ |\tilde{v}_{\infty}(\bm{x})|\leq e^{\delta\cdot(k_{-})^{\frac{n}{2}}\cdot w^{\frac{n}{2}}}\cdot P_{\frac{n}{2}}(w)^{-\frac{\nu}{2}},&w(\bm{x})\gg 1,\\ \frac{\partial\tilde{v}_{\infty}}{\partial w}=0,&w(\bm{x})=w_{0}.\end{cases}

In the following, we will prove that v~∞\tilde{v}_{\infty} is vanishing everywhere in the Calabi space π’žβˆ’n\mathcal{C}_{-}^{n} such that the contradiction arises.

To see this, recall that the incomplete Calabi model space (π’žβˆ’n,gπ’žβˆ’)(\mathcal{C}_{-}^{n},g_{\mathcal{C}_{-}}) is diffeomorphic to the topological product [w0,+∞)Γ—Y2​nβˆ’1[w_{0},+\infty)\times Y^{2n-1}, where Y2​nβˆ’1≑{ρ=ρ0}Y^{2n-1}\equiv\{\rho=\rho_{0}\} is with respect to the boundary slice in the Calabi model (see Section 5 for detailed discussions on it). The above structure leads to a natural coordinate representation 𝒙=(w,π’š)βˆˆπ’žβˆ’n\bm{x}=(w,\bm{y})\in\mathcal{C}_{-}^{n} for each point in the Calabi model space such that the boundary of π’žβˆ’n\mathcal{C}_{-}^{n} is given by {w=w0}\{w=w_{0}\}, where the coordinate ww is the natural moment map coordinate.

Denote by Ξ£Y2​nβˆ’1={Ξ›k}k=0∞\Sigma_{Y^{2n-1}}=\{\Lambda_{k}\}_{k=0}^{\infty} the spectrum of the fiber Y2​nβˆ’1Y^{2n-1} with respect to the induced Riemannian metric. Let {Ο†k}k=0∞\{\varphi_{k}\}_{k=0}^{\infty} be the orthonormal basis with respect to the L2L^{2}-inner product on Y2​nβˆ’1Y^{2n-1}, such that for each kβˆˆβ„•k\in\mathbb{N},

(6.125) βˆ’Ξ”Y2​nβˆ’1​φk=Ξ»kβ‹…Ο†k.\displaystyle-\Delta_{Y^{2n-1}}\varphi_{k}=\lambda_{k}\cdot\varphi_{k}.

If δ>0\delta>0 is chosen sufficiently small, applying Proposition 5.14, then v~∞\tilde{v}_{\infty} has the expansion

(6.126) v~βˆžβ€‹(w,π’š)=ΞΊβ‹…w+β„“+βˆ‘k=1∞ckβ‹…π’Ÿk​(w)β‹…Ο†k​(π’š),\tilde{v}_{\infty}(w,\bm{y})=\kappa\cdot w+\ell+\sum\limits_{k=1}^{\infty}c_{k}\cdot\mathcal{D}_{k}(w)\cdot\varphi_{k}(\bm{y}),

where the function π’Ÿk​(w)\mathcal{D}_{k}(w) has some definite exponential decaying rate (see Lemma 5.4 and Lemma 5.7 for the accurate rates).

Now we apply the Neumann condition to show that ΞΊ=0\kappa=0 and ck=0c_{k}=0 for all kβˆˆβ„•k\in\mathbb{N}. In fact,

(6.127) βˆ‚v~βˆžβ€‹(w,π’š)βˆ‚w=ΞΊ+βˆ‘k=1∞ckβ‹…π’Ÿk′​(w)β‹…Ο†k​(π’š).\frac{\partial\tilde{v}_{\infty}(w,\bm{y})}{\partial w}=\kappa+\sum\limits_{k=1}^{\infty}c_{k}\cdot\mathcal{D}_{k}^{\prime}(w)\cdot\varphi_{k}(\bm{y}).

Integrating (6.127) over the boundary slice {w=w0}\{w=w_{0}\},

(6.128) ΞΊβ‹…Volgπ’žβˆ’n⁑(Y2​nβˆ’1)=∫Y2​nβˆ’1βˆ‚v~βˆžβ€‹(w,π’š)βˆ‚w|w=w0=0,\kappa\cdot\Vol_{g_{\mathcal{C}_{-}^{n}}}(Y^{2n-1})=\int_{Y^{2n-1}}\frac{\partial\tilde{v}_{\infty}(w,\bm{y})}{\partial w}\Big|_{w=w_{0}}=0,

which implies

(6.129) ΞΊ=0.\kappa=0.

Next, for each fixed kβˆˆβ„€+k\in\mathbb{Z}_{+}, multiplying Ο†k\varphi_{k} on the both sides of (6.127) and integrating over Y2​nβˆ’1Y^{2n-1},

(6.130) ckβ‹…π’Ÿk′​(w)=∫Y2​nβˆ’1Ο†k​(π’š)β‹…βˆ‚v~βˆžβ€‹(w,π’š)βˆ‚w|w=w0=0.c_{k}\cdot\mathcal{D}_{k}^{\prime}(w)=\int_{Y^{2n-1}}\varphi_{k}(\bm{y})\cdot\frac{\partial\tilde{v}_{\infty}(w,\bm{y})}{\partial w}\Big|_{w=w_{0}}=0.

The conclusion ck=0c_{k}=0 follows from the claim

(6.131) π’Ÿk′​(w)<0,βˆ€wβ‰₯w0.\mathcal{D}_{k}^{\prime}(w)<0,\forall\ w\geq w_{0}.

Now we just need to prove the claim. In fact, since π’Ÿk′​(w)\mathcal{D}_{k}^{\prime}(w) satisfies the equation

(6.132) π’Ÿk′′​(w)=wnβˆ’2​(jk2​n24β‹…wn+n​λk)β€‹π’Ÿk​(w)\mathcal{D}_{k}^{\prime\prime}(w)=w^{n-2}(\frac{j_{k}^{2}n^{2}}{4}\cdot w^{n}+n\lambda_{k})\mathcal{D}_{k}(w)

and hence

(6.133) π’Ÿk′′​(w)>0.\mathcal{D}_{k}^{\prime\prime}(w)>0.

Notice that π’Ÿk​(w)\mathcal{D}_{k}(w) has an exponential decaying rate. This tells us that π’Ÿk′′​(w)>0\mathcal{D}_{k}^{\prime\prime}(w)>0 and bounded as wβ†’+∞w\to+\infty. Therefore, π’Ÿk′​(w)\mathcal{D}_{k}^{\prime}(w) is increasing and uniformly continuous for w>0w>0. Since π’Ÿk​(w)β†’0\mathcal{D}_{k}(w)\to 0, we conclude that limwβ†’+βˆžπ’Ÿk′​(w)=0\lim\limits_{w\to+\infty}\mathcal{D}_{k}^{\prime}(w)=0. Therefore, π’Ÿk​(w)<0\mathcal{D}_{k}(w)<0 for any wβ‰₯w0w\geq w_{0}.

Lastly, v~∞\tilde{v}_{\infty} satisfies the renormalization condition v~βˆžβ€‹(π’™βˆž)=0\tilde{v}_{\infty}(\bm{x}_{\infty})=0, immediately, β„“=0\ell=0. Therefore,

(6.134) v~βˆžβ‰‘0onβ€‹π’žβˆ’n.\tilde{v}_{\infty}\equiv 0\quad\text{on}\ \mathcal{C}_{-}^{n}.

The proof is done.

∎

Combining all the above estimates, we are ready to complete the proof of Theorem 6.3.

Proof of Theorem 6.3.

It suffices to verify each condition for β„±\mathscr{F} in Lemma 6.1. Proposition 6.8 and Proposition 6.4 show that β„±\mathscr{F} satisfies Item (1) and Item (2a). In our context, CL>0C_{L}>0 and CN>0C_{N}>0 are uniform constants. r0>0r_{0}>0 can be chosen as any fixed constant in (0,12​CL​CN)(0,\frac{1}{2C_{L}C_{N}}). To verify Item (2b) in Lemma 6.1, we just need to use (6.21). In fact, we have assumed Ξ½+Ξ±<0\nu+\alpha<0, then

(6.135) ‖ℱ⁑(𝟎)‖𝔖2≀Cβ‹…TΞ½+Ξ±β‰ͺr04​CL,\|\mathscr{F}(\bm{0})\|_{\mathfrak{S}_{2}}\leq C\cdot T^{\nu+\alpha}\ll\frac{r_{0}}{4C_{L}},

as TT is sufficiently large. This completes the proof.

∎

6.4. Geometric singularity and normalized limit measure

The goal of this subsection is to understand the measured Gromov-Hausdorff limits of the sequence of incomplete Calabi-Yau metrics (β„³T,Ο‰T,C​Y)(\mathcal{M}_{T},\omega_{T,CY}) (scaled to fixed diameter) constructed in Theorem 6.3. As can be easily seen, the results are parallel to the statements in Theorem 1.1, and in Section 7 we shall not reproduce the arguments from here.

To begin with, we recall the notion of measured Gromov-Hausdorff convergence. We refer the readers to [CC97] for the general theory about this.

Definition 6.11 (Measured Gromov-Hausdorff convergence).

Let (Mjm,gj,pj)(M_{j}^{m},g_{j},p_{j}) be a sequence of Riemannian manifolds with Ricgjβ‰₯βˆ’(mβˆ’1)\Ric_{g_{j}}\geq-(m-1) such that

(6.136) (Mjm,gj,pj)β†’G​H(X∞,d∞,p∞)(M_{j}^{m},g_{j},p_{j})\xrightarrow{GH}(X_{\infty},d_{\infty},p_{\infty})

for some metric space (X∞,d∞,p∞)(X_{\infty},d_{\infty},p_{\infty}), then by passing to a subsequence, the renormalized measures

(6.137) d​ν¯j≑dvolgjVolgj⁑(B1​(pj))d\underline{\nu}_{j}\equiv\frac{\dvol_{g_{j}}}{\Vol_{g_{j}}(B_{1}(p_{j}))}

converge to a Radon measure dβ€‹Ξ½Β―βˆžd\underline{\nu}_{\infty} on X∞X_{\infty} which is called the renormalized limit measure. The Gromov-Hausdorff convergence together with the convergence of the renormalzied measures is called the measured Gromov-Hausdorff convergence.

In the general context of collapsed sequences with Ricci curvature bounded from below, dβ€‹Ξ½Β―βˆžd\underline{\nu}_{\infty} behaves quite differently from the Hausdorff measures on X∞X_{\infty} induced by the limiting metric d∞d_{\infty}. In our specific context, dβ€‹Ξ½Β―βˆžd\underline{\nu}_{\infty} has an explicit form and it effectively reveals the geometric singularity information in the collapsing spaces.

Now return to our context. We are interesting in the measured Gromov-Hausdorff limits of (β„³T,Ο‰T,d​ν¯T)(\mathcal{M}_{T},\omega_{T},d\underline{\nu}_{T}), where d​ν¯T=1n!​ωTnd\underline{\nu}_{T}=\frac{1}{n!}\omega_{T}^{n} is the volume measure of the metric Ο‰T\omega_{T}. Using the error estimate in Proposition 4.23, the convergence is in fact dominated by large scale geometries of the neck metric (β„³T,Ο‰T)(\mathcal{M}_{T},\omega_{T}) constructed in Section 4.1. So we shall only perform the calculation using the metrics Ο‰T\omega_{T}, and the latter are fairly explicit by construction.

Gromov-Hausdorff limit:

By construction and direct calculation one sees that gTg_{T} in large scale is approximated by the 11 dimensional metric tensor T(2βˆ’n)​(n+1)n​LT​(z)nβˆ’1​d​z2T^{\frac{(2-n)(n+1)}{n}}L_{T}(z)^{n-1}dz^{2}. In particular, the diameter is of order Tn+1nT^{\frac{n+1}{n}}. This suggests rescaling the metric gTg_{T} by Tβˆ’2​(n+1)nT^{-\frac{2(n+1)}{n}} in order to obtain bounded diameter. Indeed, upon the change of variable z=Tβ‹…ΞΎz=T\cdot\xi, we see Tβˆ’2​(n+1)n​gTT^{-\frac{2(n+1)}{n}}g_{T} converges to the one dimensional metric (1+kβˆ“β€‹ΞΎ)nβˆ’1​d​ξ2(1+k_{\mp}\xi)^{n-1}d\xi^{2}, ξ∈[βˆ’kβˆ’βˆ’1,βˆ’k+βˆ’1]\xi\in[-k_{-}^{-1},-k_{+}^{-1}] in the Gromov-Hausdorff sense.

The above limit can be transformed into the standard metric on the unit interval (𝕀,d​v2)(\mathbb{I},dv^{2}) via a constant rescaling and the following coordinate change

(6.138) {1+k+(1kβˆ’βˆ’1k+)v=(1+k+ΞΎ)n+12,ΞΎ>0;1+kβˆ’(1kβˆ’βˆ’1k+)v=(1+kβˆ’ΞΎ)n+12,ΞΎ<0.\begin{cases}1+k_{+}(\frac{1}{k_{-}}-\frac{1}{k_{+}})v=(1+k_{+}\xi)^{\frac{n+1}{2}},\ \ \xi>0;\\ 1+k_{-}(\frac{1}{k_{-}}-\frac{1}{k_{+}})v=(1+k_{-}\xi)^{\frac{n+1}{2}},\ \ \xi<0.\end{cases}

Renormalized limit measure:

Again we first calculate by definition

(6.139) Vol​(β„³a≀z≀b,Ο‰T)=∫abd​z​T2βˆ’n(nβˆ’1)!β€‹βˆ«DΟ‰~​(z)nβˆ’1.\text{Vol}(\mathcal{M}_{a\leq z\leq b},\omega_{T})=\int_{a}^{b}dz\frac{T^{2-n}}{(n-1)!}\int_{D}\tilde{\omega}(z)^{n-1}.

Upon the change of variable z=Tβ‹…ΞΎz=T\cdot\xi, this we get

(6.140) Vol​(β„³a≀ξ≀b,Ο‰T)=T2β€‹βˆ«abdβ€‹ΞΎβ€‹βˆ«D1(nβˆ’1)!​(1+k±​ξ)nβˆ’1​ωDnβˆ’1.\text{Vol}(\mathcal{M}_{a\leq\xi\leq b},\omega_{T})=T^{2}\int_{a}^{b}d\xi\int_{D}\frac{1}{(n-1)!}(1+k_{\pm}\xi)^{n-1}\omega_{D}^{n-1}.

So up to constant, the renormalized limit measure has density function given by (1+Β±ΞΎ)nβˆ’1​d​ξ(1+\pm\xi)^{n-1}d\xi. Changing to the vv-variable this becomes (again up to constant multiplication)

(6.141) dβ€‹Ξ½Β―βˆž={(vβˆ’k++1kβˆ’βˆ’k+)nβˆ’1n+1​d​v,v∈[k+kβˆ’βˆ’k+,0];(vβˆ’kβˆ’+1kβˆ’βˆ’k+)nβˆ’1n+1​d​v,v∈[0,kβˆ’kβˆ’βˆ’k+].d\underline{\nu}_{\infty}=\begin{cases}(\frac{v}{-k_{+}}+\frac{1}{k_{-}-k_{+}})^{\frac{n-1}{n+1}}dv,\ \ v\in[\frac{k_{+}}{k_{-}-k_{+}},0];\\ (\frac{v}{-k_{-}}+\frac{1}{k_{-}-k_{+}})^{\frac{n-1}{n+1}}dv,\ \ v\in[0,\frac{k_{-}}{k_{-}-k_{+}}].\end{cases}

Fibration structure:

There is an obvious fibration of β„³T\mathcal{M}_{T} over [Tβˆ’,T+][T_{-},T_{+}] using the coordinate function zz. Composing with above coordinate changes, we obtain a fibration

(6.142) β„±T:β„³T→𝕀;𝒙↦v⁑(𝒙).\mathcal{F}_{T}:\mathcal{M}_{T}\rightarrow\mathbb{I};\bm{x}\mapsto v(\bm{x}).

It is clear that for any vβ‰ 0v\neq 0, β„±Tβˆ’1​(v)\mathcal{F}_{T}^{-1}(v) is an S1S^{1} bundle over DD, whose first Chern class is given by c1​(LΒ±)c_{1}(L_{\pm}) depending on the sign of vv, and β„±Tβˆ’1​(0)\mathcal{F}_{T}^{-1}(0) is an singular S1S^{1} fibration over DD, with vanishing circles along HH.

Bubble classification:

From our analysis in Section 4.3, it is clear that suitable rescalings around the vanishing circles in β„±Tβˆ’1​(0)\mathcal{F}_{T}^{-1}(0) are given by the product space β„‚T​N2Γ—β„‚nβˆ’2\mathbb{C}_{TN}^{2}\times\mathbb{C}^{n-2}. Also suitable rescalings around the ends z=TΒ±z=T_{\pm} gives the incomplete Calabi model spaces.

We close this section by giving the following remarks regarding the regularity of the renormalized limit measure.

Remark 6.11.1.

It can be seen from the above formulae that the limiting density function π’±βˆž=dβ€‹Ξ½Β―βˆžd​v\mathscr{V}_{\infty}=\frac{d\underline{\nu}_{\infty}}{dv} is a Lipschitz function on 𝕀\mathbb{I} and it is smooth everywhere in the interior of 𝕀\mathbb{I} except at v=0v=0. On the other hand, the singular fiber of β„±\mathcal{F} precisely appears at t=0t=0. So in our context, the singularity of the renormalized limit measure dβ€‹Ξ½Β―βˆžd\underline{\nu}_{\infty} effectively characterizes the singularity behavior of the collapsing geometry.

Remark 6.11.2.

By Cheeger-Colding (see [CC00], theorem 4.6), in the regular set β„›\mathcal{R} of a general Ricci-limit space, the density function π’±βˆž\mathscr{V}_{\infty} of the renormalized limit measure always exists and is HΓΆlder continuous. Our example tells us that, in general, one cannot expect the regularity of π’±βˆž\mathscr{V}_{\infty} to be differentiable in β„›\mathcal{R} (even though β„›\mathcal{R} is a smooth Riemannian manifold). We thank Shouhei Honda for pointing this out.

Remark 6.11.3.

If we use rescale the metrics further around the point v=0v=0 such that the sequence of spaces collapse to the complete real line ℝ\mathbb{R}, then dβ€‹Ξ½Β―βˆžd\underline{\nu}_{\infty} coincides with the standard Lebesgue measure. In particular, the singularity at v=0v=0 disappears. This fact can be quickly seen by scaling-up the coordinates vv. This is compatible with the general theory of Ricci-limit spaces. That is, due to Cheeger-Colding, the renormalized limit measure always splits off the Lebesgue measure of ℝ\mathbb{R} if the limit space isometrically splits off ℝ\mathbb{R} (see proposition 1.35 in [CC97] for more details).

Original mathematics by the credited authors. Source-backed reader collection; mathematical self-containment is not assessed.