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LeanPool.CIVAxisymmetric.Prerequisites.Gkt.TopBoundedness

From interior smallness below the top slice to boundedness at the origin #

Three closing facts for the Gustafson–Kang–Tsai criterion used at the end of the proof of lem:aniso:closure: the finite halving recursion used to iterate the pressure decay; the passage from bounds on the interior cylinders Q_r(0, s), s ∈ (-σ, 0), to the Theorem A integrand on the backward cylinder B_r × (-r², 0) (monotone convergence in the top time, with the force term controlled by a pointwise bound); and the conclusion BoundedNearOrigin from smallness of that integrand, by the top-boundary form of CKN's Theorem A and continuity of u inside Q.

theorem CIV.gkt_le_half_pow_of_forall_lt {a : ℕ → ℝ} {b : ℝ} {N : ℕ} (hb : 0 ≤ b) (hrec : ∀ n < N, a (n + 1) ≤ 1 / 2 * a n + b) :
a N ≤ (1 / 2) ^ N * a 0 + 2 * b

A finite halving recursion a_{n+1} ≤ a_n / 2 + b for n < N gives a_N ≤ 2^{-N} a_0 + 2b.

theorem CIV.gkt_topCylinder_small_of_interior {q : ℝ} {u : CKN.Foundation.Parabolic.ParabolicPoint → CKN.Foundation.Parabolic.Vec3} {Du : CKN.Foundation.Parabolic.ParabolicPoint → Fin 3 → CKN.Foundation.Parabolic.Vec3} {p : CKN.Foundation.Parabolic.ParabolicPoint → ℝ} {f : CKN.Foundation.Parabolic.ParabolicPoint → CKN.Foundation.Parabolic.Vec3} (hsol : CKN.IsSuitableWeakSolution (CKN.Foundation.Parabolic.vec3Ball 0 1) (Set.Ioo (-1) 0) q u Du p f) (henergy : GlobalEnergyClass u Du p) {Mf : ℝ} (hMf0 : 0 ≤ Mf) (hMbound : ∀ z ∈ unitCylinder, CKN.Foundation.Parabolic.vec3EuclideanNorm (f z) ≤ Mf) {r σ τ : ℝ} (hτ : 0 ≤ τ) (hr : 0 < r) (hr2 : r ≤ 1 / 2) (hσ : 0 < σ) (hσr : σ ≤ r ^ 2) (hsmall : ∀ s ∈ Set.Ioo (-σ) 0, ∫⁻ (z : CKN.Foundation.Parabolic.ParabolicPoint) in CKN.Foundation.Parabolic.parabolicCylinder 0 s r, ENNReal.ofReal (CKN.Foundation.Parabolic.vec3EuclideanNorm (u z)) ^ 3 ≤ ENNReal.ofReal (τ * r ^ 2) ∧ ∫⁻ (z : CKN.Foundation.Parabolic.ParabolicPoint) in CKN.Foundation.Parabolic.parabolicCylinder 0 s r, ENNReal.ofReal |p z| ^ (3 / 2) ≤ ENNReal.ofReal (τ * r ^ 2)) :

If the velocity and pressure integrals over Q_r(0, s) are at most τ r² for every s ∈ (-σ, 0), σ ≤ r², then the Theorem A integrand over the backward cylinder B_r × (-r², 0) is at most (2τ + (4π/3) M_f^q r^{3q}) r², where M_f bounds the force on Q.

The top-boundary Theorem A in the form used here: there is ε₀ > 0, depending only on q, such that smallness ≤ ε₀ r² of the Theorem A integrand on one backward cylinder B_r × (-r², 0), r ≤ 1/2, makes (0, 0) a regular point, for a velocity continuous inside Q.