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Weak rectangular Newtonian velocity and pressure

Physical scope

Conditional no-slip weak velocity and normalized distribution pressure on a finite rectangular vessel, with constant density, positive constant viscosity, and zero force. Pressure is only a spacetime distribution; no L2 estimate, corner regularity, or pointwise wall traction is claimed.

Statement

Let Ω=∏i=13(ai,bi)⊂R3 be a finite open rectangle in Cartesian coordinates measured in metres, with ai<bi, and write U=(0,∞)×Ω⊂R4 with coordinates (t,x1,x2,x3). For an open O⊆Rn, set D(O)=Cc∞(O;C) and, for each compact K⊂O, set DK(O)={ψ∈D(O):supp⁡ψ⊆K} with Fréchet seminorms pm(ψ)=max⁡∣α∣≤msup⁡x∈K∣∂αψ(x)∣, m∈N0. Give D(O) its locally convex LF topology, the finest locally convex topology making every inclusion DK(O)→D(O) continuous; real and finite-dimensional vector test-function spaces carry the corresponding real and componentwise topologies. Let D′(O) be the vector space of continuous complex-linear functionals on D(O), with bilinear pairing ⟨F,ψ⟩=F(ψ); a spacetime distribution on U is an element of D′(U). A locally integrable field f is identified componentwise with the distribution ψ↦∫Ufψ dt dx. For F∈D′(O) and a multi-index α∈N0n, define ⟨∂αF,ψ⟩=(−1)∣α∣⟨F,∂αψ⟩ for every ψ∈D(O). Derivatives of vector or matrix distributions are taken componentwise; for scalar F∈D′(U), ∇xF=(∂xiF)i=13, for a matrix distribution A, (div⁡A)i=∑j=13∂xjAij for i=1,2,3, and Δ acts componentwise as ∑j=13∂xj2.

Define Dσ(Ω)={a∈Cc∞(Ω;R3):div⁡a=0}, where for smooth fields div⁡a=∑i=13∂xiai, let H be its closure in L2(Ω;R3), and let V be its closure in H01(Ω;R3), where H01 is the H1 closure of compactly supported smooth vector fields and H1 uses square-integrable fields and first weak derivatives. This convention does not identify V with all divergence-free members of H01 on an arbitrary open set and makes no pointwise trace assertion. Let ρ0>0 in kg m−3, μ>0 in Pa s, ν=μ/ρ0>0, and u0∈H be an initial velocity in m s−1. Assume AC and Countable Choice. In addition, assume the following rectangular test-divergence inverse: for D0(Ω)={h∈Cc∞(Ω;R):∫Ωh=0} with its subspace LF topology, a continuous linear map R:D0(Ω)→Cc∞(Ω;R3) with the componentwise LF topology satisfies div⁡(Rh)=h; for each compact input support there is one compact output support, and every fixed-support restriction is continuous for the test-function seminorms above.

Then there are a weak velocity u∈Cw([0,∞);H)∩L∞(0,∞;H)∩Lloc2(0,∞;V) and a real kinematic-pressure distribution π∈D′(U), meaning it takes real values on real-valued tests, with units m2 s−2. Here Cw means continuity of every fixed H-pairing, and the time-dependent spaces use strongly measurable Bochner maps on finite intervals. The velocity has u(0)=u0 and strong H trace at zero, and for every compactly time-supported C1 curve ϕ:[0,∞)→V it satisfies

∫0∞ ⁣[(u,∂tϕ)L2+(u⊗u,∇ϕ)L2−ν(∇u,∇ϕ)L2]dt+(u0,ϕ(0))L2=0.

All spatial pairings use unnormalized Lebesgue measure, with (u⊗u)ij=uiuj, (u⊗u):∇ϕ=∑i,juiuj∂jϕi, and ∇u:∇ϕ=∑i,j∂jui∂jϕi. For every t≥0 it satisfies

∥u(t)∥22+2ν∫0t∥∇u(s)∥22ds≤∥u0∥22,

and there is a full-measure set S⊂(0,∞) such that for every s∈S∪{0} and every t≥s,

∥u(t)∥22+2ν∫st∥∇u(τ)∥22dτ≤∥u(s)∥22.

Fix one real scalar test function θ∈Cc∞(Ω;R) with ∫Ωθ=1. The following spacetime equation is an equality in D′(U)3 under the stated distributional-derivative convention, and this fixed normalization is

∂tu+div⁡(u⊗u)+∇π=νΔu, ⟨π,a(t)θ(x)⟩=0

for every a∈Cc∞((0,∞);C). Such a θ exists because a product of normalized smooth compactly supported interval bumps belongs to Cc∞(Ω) and has integral one. The physical pressure distribution p=ρ0π has units Pa, is unique under this fixed scaled normalization, and satisfies

ρ0∂tu+ρ0div⁡(u⊗u)+∇p=μΔu

as a spacetime distribution. The SI kinetic energy E(t)=ρ02∫Ω∣u(t,x)∣2dx obeys E(t)+μ∫0t∫Ω∣∇u(s,x)∣2dx ds≤E(0). This conditional result asserts no pressure in L2, corner regularity, or pointwise boundary traction.

Facts & Assumptions

Given: The no-slip model, a bounded finite rectangle, u0∈H, AC, Countable Choice, and the stated right inverse R.

[A1]

Bounded no-slip Newtonian vessel model: ρ0,μ>0 are constant, the force is zero, no-slip means membership in V, and the weak model is tested on solenoidal V-valued curves.

[F1]

Bounded no-slip solenoidal closure spaces: H is the L2 closure and V the H01 closure of compactly supported smooth divergence-free fields; no larger solenoidal space or trace identification is included.

[F2]

Global bounded no-slip Leray–Hopf existence: for bounded open Ω, AC, ν>0, and u0∈H, the supplier Statement gives a global weak velocity with the variational identity and initial/restart energy inequalities.

[F3]

Rectangular evolving distributional pressure: for a finite rectangle and the bounded weak velocity, the proposition constructs a spacetime pressure distribution with one fixed mean-zero-test normalization, conditional on the stated continuous linear right inverse R on mean-zero tests.

[F4]

Rectangular continuous divergence inverse on mean-zero tests: for every finite rectangle, the current item proves a continuous linear R:D0(Ω)→Cc∞(Ω;R3) with div⁡(Rh)=h, compact-support enlargement, and fixed-support seminorm control.

[A2]

The Axiom of Choice: every family of nonempty sets has a choice function; AC is explicit in the bounded weak-existence Statement.

[A3]

The Axiom of Countable Choice (ACω): every countable family of nonempty sets has a choice function; it is used in the bounded weak-existence proof.

Proof

Given: The rectangle, physical parameters and model, closure spaces, AC, Countable Choice, the bounded weak-existence result [F2], the pressure proposition [F3], and the actual divergence inverse [F4].

1.1givenA1F1F2A2A3algebra

For each side interval set mi=(ai+bi)/2, di=(bi−ai)/4>0, and ri(xi)=(xi−mi)/di. Define gi(xi)=exp⁡(−1/(1−ri(xi)2)) when ∣ri(xi)∣<1 and gi=0 otherwise. Its support is the compact interval [mi−di,mi+di]⊂(ai,bi). Each repeated derivative inside that support is a finite sum of a polynomial in ri times a negative power of 1−ri2 times the exponential; since y−Ne−1/y→0 as y↓0 for every N, all derivatives vanish at the support endpoints and gi∈Cc∞((ai,bi)). Positivity and compact support give Ii=∫aibigi dxi∈(0,∞). Put ηi=gi/Ii and θ(x)=η1(x1)η2(x2)η3(x3); then θ∈Cc∞(Ω) and Fubini gives ∫Ωθ=1. Set ν=μ/ρ0>0. The domain, initial datum, closure spaces, AC, and Countable Choice match [F2], so choose its global weak velocity u with the stated initial and restart energy inequalities. To match the stress model, first take compactly supported smooth solenoidal u,ϕ. Then 2D(u):∇ϕ=∇u:∇ϕ+∂jui∂iϕj; integration by parts makes the last term −∫ui∂i(div⁡ϕ)=0. The pressure term also vanishes because div⁡ϕ=0. The bilinear forms are continuous in V, so density extends this identity to the closure-space weak velocity. Hence [F2] is exactly the weak velocity input for [A1].

2.1givenF1F2F3F4step 1.1

The rectangle is within the domain of [F3], and its exact conditional right-inverse hypothesis is supplied by [F4]. Apply the proposition to this weak velocity to obtain π, its fixed-θ normalization, and the spacetime distributional equation.

3.1F2F3step 2.1algebra∎

Define p=ρ0π. Multiplication by the positive constant ρ0 preserves distributional equality and the normalization; substituting ρ0ν=μ gives the physical equation in the Statement. The same scaling preserves uniqueness under normalization and converts the velocity energy inequality to SI units. No step supplies an L2 or corner estimate.

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