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Classical continua with explicit constitutive assumptions — Examples

1 · Prerequisites

2 · Summary

Worked checks for cm17-classical-continua-with-explicit-constitutive-assumptions. Worked check of the transport identity and the continuity equation on a uniform expansion verifies the transport identity, the continuity equation and the constant-product law exactly on a uniform expansion χ(t,X)=(1+αt)X of a cube with specified length scale (including the one-metre cube), where α has units of inverse time. A longitudinal plane wave in the linear elastic branch: stress, equation of motion and strain energy computed computes a longitudinal plane wave of the linear elastic branch: strain, stress, the displacement equation at cL=(λ+2μs)/ρ0 and the positive strain-energy density. Two-mode fixed-end string: exact solution, d'Alembert cross-check and the O(N^{-4}) tail bound at N=1 solves a two-mode fixed-end string exactly, cross-checks the d'Alembert formula, and evaluates the O(N−4) tail bound at N=1. Chain versus string on the normalized standing wave: exact discrete error, the N=100 bounds, and physical circumference 2π m compares the cyclic mass-spring chain with the travelling standing wave: the exact discrete frequency and nodal error, the evaluated O(a3/2) bound at N=100, and the second-order dispersion error in the spacing. A Riemann shock and a rarefaction of the scalar model: explicit weak solutions, entropy coefficients and initial trace verifies an explicit Rankine-Hugoniot shock with its entropy coefficients under the countable-choice Lebesgue weak formulation and a rarefaction fan with its initial trace in the scalar weak formulation. Poiseuille and Couette channel flows of the viscous branch: explicit profiles, flux and wall data solves the steady viscous channel exactly (Poiseuille flux and centre speed, Couette vorticity, uniqueness in the ansatz) under the adopted no-slip wall data. Periodic shear fields: an exact steady Euler solution, failure for the viscous branch, and the classification of steady periodic shears exhibits the sinusoidal shear as an exact steady Euler solution in the scaled variables of the periodic cell, shows it fails the viscous projected equation, and classifies the steady periodic viscous shears as constants. FALSE: the reversed-normal convention alone makes a continuous traction field a stress matrix. The field t(n)=|n_1|n refutes it refutes the claim that the reversed-normal convention alone forces a stress matrix: the continuous balanced-looking field t(n)=∣n1∣n has no representing matrix, so the balance hypothesis of the Cauchy-tetrahedron theorem is essential.

3 · Logical flowchart

4 · Definitions, postulates, theorems and proofs

None yet.

5 · Examples, experiments and counterexamples

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Worked check of the transport identity and the continuity equation on a uniform expansion

Physical scope

A worked verification of the model's transport identity and continuity equation on the explicit uniform expansion of a cube of side L_0 (including the one-metre cube), with constant reference density rho_0 and time-dependent spatial density: the model velocity, divergence, density field and mass are computed exactly, the integral mass balance holds identically, the continuity equation holds identically, and both sides of the transport identity are evaluated for a nonconstant field. The example is an exact conditional check within the adopted model; it reports no measurement.

Example

Assume ACω (The Axiom of Countable Choice (ACω)) for the cited Lebesgue transport and continuity suppliers.

Let L0>0 have dimension length and let B=(0,L0)3⊆R3 be the reference cube (the unit-cube case is L0=1 m). Fix an expansion rate α>0 with [α]=τ−1 and put I=(−1/α,∞) and define the uniform expansion

χ(t,X):=((1+αt)X1,(1+αt)X2,(1+αt)X3)((t,X)∈I×R3).

Then χ is a motion of B on I in the sense of Continuum motions, spatial velocity, material acceleration and swept regions (with O=R3): it is C∞, each χt is a diffeomorphism with DXχt=(1+αt)I3 and J(t,X)=(1+αt)3>0 on I×B. Adopt the model of Adopted continuum kinematic model: body data, smooth motions as families of label worldlines, the continuum idealization and frame covariance with these data and the constant-reference-density field

ρ(t,x):=ρ0(1+αt)3(ρ0>0)

on all of I×R3. This is a positive C∞ scalar field with [ρ0]=[ρ]=μℓ−3, so it is defined on an open neighborhood of every swept closure. Its values outside the current body are an explicit mathematical extension. Then:

  1. the spatial velocity is u(t,x)=αx/(1+αt) and div⁡u(t,x)=3α/(1+αt) (Euclidean spatial calculus: gradient, divergence and material derivative);
  2. the model mass of B at time t is ∫χt(B)ρ dx=ρ0L03 for every t∈I: the mass-balance assumption of Adopted mass balance: the mass of every material subregion is constant in time holds for every material subregion, since more generally m(t,B′)=ρ0vol⁡(B′), and the continuity equation ∂tρ+div⁡(ρu)=0 of The continuity equation of the continuum model: local form of mass balance, the material form, and the incompressibility reading holds identically on I×R3;
  3. for the field f(t,x):=x12 the transport identity of The transport identity and the material derivative along label worldlines for the adopted continuum model is verified exactly: with F(t)=∫χt(B)f(t,x) dx one has F(t)=L05(1+αt)5/3 and F′(t)=5αL05(1+αt)4/3=∫χt(B)(∂tf+div⁡(fu)) dx for every t∈I;
  4. along each label the density satisfies ρ(t,χ(t,X))(1+αt)3=ρ0, the constant-product form of density times volume of part (ii) of the continuity theorem, and the material derivative is Dtρ(t,χ(t,X))=−3αρ0/(1+αt)4=−ρdiv⁡u, as the material form of that theorem requires.

Facts & Assumptions

Given: Countable choice. the side length L0>0, expansion rate α>0 and the domain B=(0,L0)3, the interval I=(−1/α,∞), the motion χ, the constant ρ0>0 and the field ρ.

[F1]

Motion and velocity (Continuum motions, spatial velocity, material acceleration and swept regions, Adopted continuum kinematic model: body data, smooth motions as families of label worldlines, the continuum idealization and frame covariance, Ck Euclidean maps and diffeomorphisms): χ satisfies the defining conditions of a motion with DXχt=(1+αt)I3, J=(1+αt)3>0 on I×B; the spatial velocity is u(t,x)=∂tχ(t,χt−1(x))=αx/(1+αt), of class C∞ on I×R3.

[F2]

Spatial calculus (Euclidean spatial calculus: gradient, divergence and material derivative): for u(t,x)=αx/(1+αt) one has ∂juj=α/(1+αt) and div⁡u=3α/(1+αt); the divergence of the field fu with f=x12 is ∂1(x13α/(1+αt))+∂2(αx12x2/(1+αt))+∂3(x12x3α/(1+αt))=5αx12/(1+αt).

[F3]

Transport and continuity (The transport identity and the material derivative along label worldlines for the adopted continuum model, The continuity equation of the continuum model: local form of mass balance, the material form, and the incompressibility reading, Integral over a measurable subset): under the stated kinematic and mass-balance hypotheses, F is differentiable with F′(t)=∫χt(B)(∂tf+div⁡(fu)) dx, the continuity equation holds, and ddtρ(t,χ(t,X))=Dtρ(t,χ(t,X))=−ρdiv⁡u along labels.

Verification

technique · direct; compute the Jacobian, velocity, divergence, density field and both sides of the identities from the definitions and evaluate the integrals over the cube explicitly
1.1givenF1

Motion and velocity: DXχt=(1+αt)I3 gives J=(1+αt)3>0 on I×B, so χ is a motion of B on I; inverting, χt−1(x)=x/(1+αt) and u(t,x)=∂tχ(t,χt−1(x))=αx/(1+αt).

2.1step 1.1F2algebra

Divergences: since uj(t,x)=αxj/(1+αt), ∂juj=α/(1+αt) and div⁡u=3α/(1+αt); with f=x12 the computation of [F2] gives div⁡(fu)=5αx12/(1+αt) and ∂tf=0.

2.2step 1.1F3algebra

Transport identity, left side: F(t)=∫χt(B)x12 dx=(1+αt)5∫BX12 dX=L05(1+αt)53 by the same change of variables, since ∫0L0X12 dX1=L03/3 and the other two coordinate integrals each contribute L0; hence F′(t)=5αL05(1+αt)43.

3.1step 1.1step 2.1F3algebra

Mass and continuity: by the change of variables x=(1+αt)X with J=(1+αt)3, one has ∫χt(B)ρ dx=∫Bρ0(1+αt)3(1+αt)3 dX=ρ0L03, constant in t. The same change of variables on any admissible B′ gives m(t,B′)=ρ0vol⁡(B′), establishing the adopted mass balance for every material subregion. For the continuity equation, ∂tρ=−3αρ0/(1+αt)4 and, by step 2.1 and the product rule, div⁡(ρu)=ρdiv⁡u=ρ0(1+αt)3⋅3α1+αt=3αρ0(1+αt)4, so the sum is zero identically on I×R3.

3.2step 2.1step 2.2F3algebra

Transport identity, right side: the integrand ∂tf+div⁡(fu)=5αx12/(1+αt) by step 2.1, so ∫χt(B)(∂tf+div⁡(fu)) dx=5α1+αt∫χt(B)x12 dx=5α1+αt⋅L05(1+αt)53=5αL05(1+αt)43, which equals the derivative of step 2.2 for every t∈I.

4.1step 1.1step 3.1F3algebra∎

Material form: by step 1.1, ρ(t,χ(t,X))=ρ0/(1+αt)3 so ρ(t,χ(t,X))J(t,X)=ρ0 is constant along each label, matching the constant-product clause of The continuity equation of the continuum model: local form of mass balance, the material form, and the incompressibility reading; and ddtρ(t,χ(t,X))=−3αρ0/(1+αt)4=−ρ(t,χ(t,X))div⁡u(t,χ(t,X)) by step 2.1, matching the material form Dtρ=−ρdiv⁡u.

Remarks

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A longitudinal plane wave in the linear elastic branch: stress, equation of motion and strain energy computed

Physical scope

A worked longitudinal plane wave of the adopted linear elastic branch: explicit strain, stress, verification of the displacement equation at the longitudinal speed root((lambda+2mu_s)/rho_0) and the positive strain-energy density of the wave. The computation is exact within the branch and asserts no measurement and no completeness of plane waves.

Example

Adopt the isotropic linear elastic branch of Adopted isotropic linear elastic constitutive model with its small-strain regime and strain energy with reference density ρ0>0 of dimension μℓ−3 and moduli λ,μs of dimension μℓ−1τ−2, with μs>0 and λ+2μs3>0 (Continuum body data, the fixed inertial frame and the dimensions of the fields). Use I=R, O=R3 and let x1 be the reference position in metres and t time in seconds. The amplitude A≠0 has dimension ℓ, and the wave number κ≠0 has dimension ℓ−1. Define the positive longitudinal speed and angular frequency by cL:=(λ+2μs)/ρ0 and ω:=κcL; then [cL]=ℓτ−1, [ω]=τ−1 and the phase is dimensionless. Let

ξ(t,x):=Acos⁡(κx1−ωt) e1,

with A≠0, κ≠0 and e1 the first standard basis vector: a longitudinal plane wave travelling along e1. This is a solution of the linear reference-field model for every declared A,κ; physical small-strain use requires small ∣Aκ∣. No finite-motion diffeomorphism is inferred: its candidate placement has determinant 1−Aκsin⁡(κx1−ωt), which need not be positive for these unrestricted algebraic data. Then:

  1. the linear strain is e11(t,x)=−Aκsin⁡(κx1−ωt) with all other entries zero, so tr⁡e=e11 and e0=e−13(tr⁡e)I3 has Frobenius squared norm 23e112;
  2. the stress matrix is σ(t,x)=(λ+2μs)e11(t,x) e1e1T+λe11(t,x) (e2e2T+e3e3T);
  3. the displacement equation (E) of The displacement equation of the linear elastic branch: rho_0 partial_t^2 xi = rho_0 b + mu_s Laplacian xi + (lambda + mu_s) grad div xi with b≡0 holds exactly: ρ0∂t2ξ1=(λ+2μs)∂12ξ1;
  4. the strain-energy density, of dimension μℓ−1τ−2, is W(e)=(λ2+μs)e112=μs23e112+(λ2+μs3)e112≥0, with equality only where e11=0; both coefficients in the decomposition are positive under the branch's hypotheses, and the squared speed cL2=(λ+2μs)/ρ0 is positive with [cL]=ℓτ−1.

Facts & Assumptions

Given: the branch data (ρ0,λ,μs); the amplitude A≠0, wave number κ≠0 and the wave ξ.

[F1]

Branch data and stress (Adopted isotropic linear elastic constitutive model with its small-strain regime and strain energy, The small-strain isotropic linear elastic constitutive law and its strain energy): e=12(Dξ+DξT) and σ=λ(tr⁡e)I3+2μse, with μs>0 and λ+2μs3>0.

[F2]

Displacement equation (The displacement equation of the linear elastic branch: rho_0 partial_t^2 xi = rho_0 b + mu_s Laplacian xi + (lambda + mu_s) grad div xi): in the branch's description with b≡0, ρ0∂t2ξ=μsΔξ+(λ+μs)∇(div⁡ξ).

[F3]

Strain-energy decomposition and positivity (The isotropic elastic strain energy is μ∣e0∣F2+(λ/2+μ/3)(tr⁡e)2, hence positive definite under μ>0, λ+2μ/3>0, The small-strain isotropic linear elastic constitutive law and its strain energy): W(e)=λ2(tr⁡e)2+μstr⁡(e2)=μs∣e0∣F2+(λ2+μs3)(tr⁡e)2≥0, with equality only for e=0, under the stated positivity hypotheses.

[F4]

Calculcus of the wave (The derivatives of sine and cosine are cosine and minus sine, Euclidean spatial calculus: gradient, divergence and material derivative, Parity and the Pythagorean identity for sine and cosine): ∂1ξ1=−Aκsin⁡(κx1−ωt), ∂12ξ1=−Aκ2cos⁡(κx1−ωt), ∂t2ξ1=−Aω2cos⁡(κx1−ωt), and ω2=κ2cL2.

[F5]

Quantity dimensions (Continuum body data, the fixed inertial frame and the dimensions of the fields): [ξ]=ℓ, [e]=1, and the stress and strain-energy density have dimension μℓ−1τ−2.

Verification

technique · direct computation; differentiate the wave, form the strain and stress with the branch's formulae, and compare the two sides of the displacement equation
1.1givenF1F4

Strain: ξ depends on x only through x1 and only its first component is nonzero, so Dξ has the single nonzero entry ∂1ξ1=−Aκsin⁡(κx1−ωt); hence e11=∂1ξ1 and all other entries of e vanish, tr⁡e=e11, and e0=diag(23,−13,−13)e11 has ∣e0∣F2=23e112.

2.1step 1.1F1algebra

Stress: substituting e into σ=λ(tr⁡e)I3+2μse gives σ11=(λ+2μs)e11 and σ22=σ33=λe11, all off-diagonal entries zero, which is the displayed matrix.

3.1step 2.1F2F4algebra

Displacement equation: the right side of (E) of [F2] is μsΔξ+(λ+μs)∇(div⁡ξ); since Δξ=∂12ξ1e1 and ∇(div⁡ξ)=∂12ξ1e1, it equals (λ+2μs)∂12ξ1e1. The left side is ρ0∂t2ξ1e1 with ∂t2ξ1=−ω2Acos⁡(κx1−ωt) by [F4]; since ω2=κ2cL2=κ2(λ+2μs)/ρ0, one has ρ0∂t2ξ1=−ρ0Aω2cos⁡(κx1−ωt)=−(λ+2μs)Aκ2cos⁡(κx1−ωt)=(λ+2μs)∂12ξ1, so the equation holds exactly for every (t,x).

4.1step 1.1step 3.1F1F3F5algebra∎

Energy: by [F3] and step 1.1, W=μs∣e0∣F2+(λ2+μs3)(tr⁡e)2=(2μs3+λ2+μs3)e112=(λ2+μs)e112; the coefficients μs>0 and λ2+μs3=3λ+2μs6>0 are positive by [F1], so W≥0 with equality exactly where e11=0. By [F5], e is dimensionless and W has dimension μℓ−1τ−2, consistent with the constitutive formula. Finally cL2=(λ+2μs)/ρ0 is positive because λ+2μs=(λ+2μs3)+4μs3>0 and ρ0>0.

Remarks

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Two-mode fixed-end string: exact solution, d'Alembert cross-check and the O(N^{-4}) tail bound at N=1

Physical scope

A worked fixed-end string problem of the adopted model: an initial displacement with two sine modes and zero initial velocity, its exact two-mode solution, agreement with the d'Alembert formula, mode frequencies and a finite check of the O(N^{-4}) tail bound at N=1. The example is an exact conditional computation within the linear string model and reports no measurement.

Example

Let L>0 be a length, c>0 a speed, A∗>0 a displacement scale with [A∗]=ℓ, and β∈R∖{0} dimensionless. Let [x]=ℓ and [t]=τ, and consider the fixed-end string model of The string model: d'Alembert solutions, fixed-end modes and uniqueness for the adopted one-dimensional continuum with initial displacement and velocity

F(x):=A∗[sin⁡(πxL)+βsin⁡(3πxL)],G(x):=0.

Then F is odd and 2L-periodic of class C∞ and G is odd and 2L-periodic of class C4, with M4=sup⁡∣G(4)∣=0 and M5=sup⁡∣F(5)∣≤A∗(π/L)5(1+243∣β∣)=:M‾5 (Sine coefficients, sine series and the odd periodic extension). Put ωn:=nπc/L and

u(t,x):=A∗[cos⁡(ω1t)sin⁡(πxL)+βcos⁡(ω3t)sin⁡(3πxL)].

Then:

  1. the sine coefficients of F are b1(F)=A∗, b3(F)=βA∗ and bn(F)=0 otherwise, and the coefficients of G all vanish; hence the series solution of The classical C2 fixed-end string: the sine series solves the wave equation with the given data, uniquely, with an explicit tail bound is exactly the displayed finite sum u;
  2. u is C∞ on R2, satisfies utt=c2uxx, vanishes at x=0 and x=L for every t, and has u(0,⋅)=F, ut(0,⋅)=0; by the uniqueness clause of the theorem it is the unique C2 fixed-end solution with these data;
  3. the d'Alembert formula of d'Alembert's formula solves the wave equation, is the unique C2 solution, and the fixed-end sine modes solve it exactly with data (F,0) gives the same field: 12[F(x−ct)+F(x+ct)]=u(t,x) by the product-to-sum identity (The addition formulas for sine and cosine, Parity and the Pythagorean identity for sine and cosine);
  4. the tail bound at N=1 is verified: with S1u=A∗cos⁡(ω1t)sin⁡(πx/L) one has ∣u−S1u∣=A∗∣β∣∣cos⁡(ω3t)∣∣sin⁡(3πx/L)∣≤A∗∣β∣, while the theorem gives ∣u−SNu∣≤C(N+1)−4 with C≤C‾:=4A∗(1+243∣β∣), so the explicit upper estimate is A∗(1+243∣β∣)/4 at N=1, which also dominates the direct bound A∗∣β∣ for every β;
  5. the mode frequencies satisfy [ωn]=τ−1 under [c]=ℓτ−1 and [L]=ℓ (Continuum body data, the fixed inertial frame and the dimensions of the fields).

Facts & Assumptions

Given: the string data L>0, c>0, A∗>0 with [A∗]=ℓ; the dimensionless parameter β≠0; the functions F,G and the field u.

[F1]

Fixed-end theorem (The classical C2 fixed-end string: the sine series solves the wave equation with the given data, uniquely, with an explicit tail bound, Sine coefficients, sine series and the odd periodic extension): for odd 2L-periodic C5 displacement data F and odd 2L-periodic C4 velocity data G, the sine series with coefficients an=bn(F), dn=bn(G)/ωn solves the fixed-end problem, is unique among C2 solutions, and satisfies the tail bound ∣u−SNu∣≤C(N+1)−4 with C=2(2L5M5/π5+2L5M4/(cπ5)).

[F2]

d'Alembert formula (d'Alembert's formula solves the wave equation, is the unique C2 solution, and the fixed-end sine modes solve it exactly): for F∈C2(R) and G≡0 the field 12[F(x−ct)+F(x+ct)] is C2 and solves utt=c2uxx with u(0,⋅)=F,ut(0,⋅)=0; uniqueness among C2 fields on R2 holds.

[F3]

Trigonometry and derivatives (The addition formulas for sine and cosine, The derivatives of sine and cosine are cosine and minus sine, Parity and the Pythagorean identity for sine and cosine, Ck Euclidean maps and diffeomorphisms): F and G have the stated smoothness and parity; sin⁡acos⁡b=12[sin⁡(a+b)+sin⁡(a−b)]; ω3=3ω1; and ∣F(5)∣=A∗∣(π/L)5cos⁡(πx/L)+243β(π/L)5cos⁡(3πx/L)∣≤A∗(π/L)5(1+243∣β∣).

[F4]

String model (The string model: d'Alembert solutions, fixed-end modes and uniqueness for the adopted one-dimensional continuum): the model equation is utt=c2uxx for the transverse displacement with the stated idealizations and dimension conventions (Continuum body data, the fixed inertial frame and the dimensions of the fields).

Verification

technique · direct; identify the finite sine expansion of the two-mode data, verify the equation and data mode by mode, cross-check with the d'Alembert formula and evaluate the tail bound at $N=1$
1.1givenF1algebra

Coefficients: by the orthogonality of the sine family, bn(F)=2L∫0LF(x)sin⁡(nπx/L) dx equals A∗ for n=1, βA∗ for n=3 and 0 otherwise (Sine coefficients, sine series and the odd periodic extension); likewise bn(G)=0 for all n. Hence the series solution of [F1] is ∑n[bn(F)cos⁡(ωnt)+0]sin⁡(nπx/L)=u(t,x), a finite sum.

2.1step 1.1F3F4algebra

Equation and data: the model equation is the one of [F4], and differentiating the two terms twice in t and x gives utt=−∑n∈{1,3}ωn2[…] and c2uxx=−c2∑n(nπ/L)2[…], which agree because ωn=cnπ/L; at t=0 the cosines equal 1 so u(0,⋅)=F, and ut(t,x)=−∑nωnsin⁡(ωnt)[…] vanishes at t=0, giving ut(0,⋅)=0. Boundary conditions hold since each sin⁡(nπx/L) vanishes at x=0,L.

3.1step 2.1F1

Uniqueness: by [F1] the solution is unique among C2 fields on [0,T]×[0,L] with these boundary and initial data; the displayed u is therefore the model's solution.

3.2step 2.1F2F3algebra

d'Alembert cross-check: by the product-to-sum identity of [F3], 12[F(x−ct)+F(x+ct)]=A∗2[sin⁡(π(x−ct)/L)+sin⁡(π(x+ct)/L)]+βA∗2[sin⁡(3π(x−ct)/L)+sin⁡(3π(x+ct)/L)]=A∗cos⁡(ω1t)sin⁡(πx/L)+βA∗cos⁡(ω3t)sin⁡(3πx/L)=u(t,x), so the two formulas agree for these data.

4.1step 2.1F1F3algebra∎

Tail bound at N=1: S1u=A∗cos⁡(ω1t)sin⁡(πx/L), so ∣u−S1u∣=A∗∣β∣∣cos⁡(ω3t)∣∣sin⁡(3πx/L)∣≤A∗∣β∣. Differentiating F five times by [F3] gives F(5)(x)=A∗(π/L)5(cos⁡(πx/L)+243βcos⁡(3πx/L)), hence M5≤M‾5=A∗(π/L)5(1+243∣β∣), while M4=0. Thus the constant in [F1] satisfies C=4L5M5/π5≤C‾:=4A∗(1+243∣β∣); applying [F1] yields ∣u−S1u∣≤C2−4≤C‾2−4=A∗(1+243∣β∣)/4. This explicit upper estimate also dominates the direct bound A∗∣β∣, since 1+243∣β∣≥4∣β∣, and preserves the theorem’s O(N−4) estimate with C≤C‾ for every N≥1. Equality between M5 and M‾5 is not required.

Remarks

  • The two-mode data make every series finite, so the check isolates the theorem's content — the mode frequencies, the boundary and initial conditions, uniqueness, the d'Alembert correspondence and the tail constant — without requiring convergence arguments beyond the supplier theorem.

  • Modes with larger n oscillate faster and the displayed bound is deliberately conservative at small N; the O(N−4) decay becomes informative for large mode numbers and smooth data, as the theorem states. No measured frequency, tension or density appears.

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Chain versus string on the normalized standing wave: exact discrete error, the N=100 bounds, and physical circumference 2π m

Physical scope

A worked comparison in SI-normalized numerical variables of the cyclic mass-spring chain and continuum string on the standing wave sin(x)cos(t), using a physical circumference of 2π m, linear density 1 kg m^{-1}, tension 1 N, and speed 1 m s^{-1}. It computes the exact chain solution and frequency, nodal error, the theorem's nodal and full interpolation bounds at N=100 (both O(a^{3/2}) for fixed positive time, with interpolation remainder Aa^2/8), the sharper O(a^2) nodal and interpolation errors for these standing-wave data, and the dispersion-relation error a^2/12. The normalized results are model calculations, not measurements.

Example

Take the periodic string model of The continuum string model as the proved limit of the mass-spring chain, with explicit convergence and dispersion error with physical circumference L∗=2π m, linear mass density ρℓ,∗=1 kg m−1 and tension τs,∗=1 N=1 kg m s−2. Then c∗:=τs,∗/ρℓ,∗=1 m s−1. Use reference units ℓ∗=1 m, τ∗=1 s and displacement scale A∗=1 m. In the equations below, x,t,L,c denote numerical values in these units, so L=2π, c=1, and the dimensionless displacement u=uphys/A∗ has the exact travelling-standing solution with physical wave number 1 m−1 and angular frequency 1 s−1

u(t,x):=Asin⁡xcos⁡t(A>0),

where A is dimensionless. Physical displacements and their error bounds are obtained by multiplying the displayed values by A∗. The normalized density and tension values are ρℓ=ρℓ,∗/(1 kg m−1)=1 and τs=τs,∗/(1 N)=1; these are numerical values of different dimensioned quantities. The normalized field is 2π-periodic and solves utt=uxx. For N≥2 put a=2π/N and consider the cyclic spring chain of The cyclic spring chain, its discrete energy, and the finite-regularity periodic comparison class with parameter c=1 and spacing a, i.e. the normalized node mass is m=ρℓa in units of 1 kg and the normalized spring constant is ks=τs/a in units of 1 N m−1. Then:

  1. M=sup⁡∣∂x4u∣=A, M2=sup⁡∣∂x2u∣=A and the theorem's constant is C=2πA/12≈0.20889A;
  2. the exact chain solution with the sampled data is qj(t)=Asin⁡(ja)cos⁡(ωat) with ωa=2sin⁡(a/2)/a (positive for 0<a<π), the exact nodal error is ej(t)=Asin⁡(ja)[cos⁡(ωat)−cos⁡t], and the theorem's bounds read ∥e(t)∥a≤Ca2t2/2, max⁡j∣ej(t)∣≤12Ca3/2t2 and sup⁡x∣Iaq−u∣≤max⁡j∣ej∣+Aa2/8;
  3. at N=100 (so a=2π/100≈0.062832) and t=1 the evaluated bounds are ∥e(1)∥a≤0.0004124A, max⁡j∣ej(1)∣≤0.001645A and sup⁡∣Iaq−u∣≤0.002139A, while the exact error satisfies ∣ej(1)∣≤A∣ωa−1∣≈0.00016449A, so the theoretical bound is verified and visibly conservative;
  4. the exact dispersion relation is ωa2=(4/a2)sin⁡2(a/2), and the theorem's bound ∣ωa2−1∣≤a2/12 gives ≤0.00032899 at N=100, while the exact value satisfies ∣ωa2−1∣≈0.00032894.

Facts & Assumptions

Given: the physical parameters L∗=2π m, ρℓ,∗=1 kg m−1, τs,∗=1 N, the reference units and normalized values L=2π, c=1, ρℓ=1, τs=1; the dimensionless amplitude A>0; the standing wave u; and the integer N≥2 and normalized spacing a=2π/N.

[F1]

Chain and norms (The cyclic spring chain, its discrete energy, and the finite-regularity periodic comparison class): the cyclic chain equation is qj′′=(c2/a2)(qj+1−2qj+qj−1) with discrete norm ∥⋅∥a, and the sampled data are qj(0)=u(0,ja), qj′(0)=ut(0,ja).

[F2]

Continuum-limit theorem (Finite-time continuum limit of the cyclic spring chain: uniform O(a3/2) nodal and uniform interpolation convergence): under the stated smoothness and periodicity hypotheses on u and its wave equation, the chain solution exists and is unique on [0,T], and with ej=qj−u(t,ja) and C=c2LM/12 one has ∥e(t)∥a≤Ca2t2/2, ∥e′(t)∥a≤Ca2t, max⁡j∣ej(t)∣≤12Ca3/2t2 and sup⁡x∣Iaq(t,x)−u(t,x)∣≤max⁡j∣ej(t)∣+M2a2/8.

[F3]

Dispersion theorem (Exact dispersion relation ω2=(4c2/a2)sin⁡2(κa/2) for the cyclic chain and its continuum error bound): for A≠0 and κNa∈2πZ, qj(t)=Acos⁡(κja−ωt) solves the chain equation if and only if ω2=(4c2/a2)sin⁡2(κa/2); when this dispersion relation holds and ∣κa∣≤1, ∣ω2−c2κ2∣≤c2κ4a2/12.

[F4]
[F5]

Verification

technique · direct; verify the standing wave and the exact discrete solution, evaluate the theorem's bounds at $N=100$, and compare with the exact error and dispersion values
1.1givenF4F5algebra

Data: ∂x4u=Asin⁡xcos⁡t and ∂x2u=−Asin⁡xcos⁡t, so M=M2=A; by [F5], C=2πA/12.

1.2givenF1F3F4algebra

Exact chain solution: with qj(t)=Asin⁡(ja)cos⁡(ωat) one has qj′′=−ωa2qj and qj+1−2qj+qj−1=−4sin⁡2(a/2)qj, so the chain equation qj′′=a−2(qj+1−2qj+qj−1) holds for the chosen frequency ωa2=4sin⁡2(a/2)/a2, i.e. ωa=2sin⁡(a/2)/a for a∈(0,π], since N≥2; at N=2 the sampled values sin⁡(jπ) vanish and the zero chain solves independently of frequency. The sampled data match because qj(0)=Asin⁡(ja)=u(0,ja) and qj′(0)=0=ut(0,ja).

2.1step 1.2F4algebra

Exact nodal error: ej(t)=qj(t)−u(t,ja)=Asin⁡(ja)[cos⁡(ωat)−cos⁡t], hence by [F4] ∣ej(t)∣≤A∣ωa−1∣ t for t≥0.

2.2step 1.1F2algebra

Bounds at N=100: with a=2π/100 one has a2=4π2/104 and a3/2=(2π/100)3/2. Hence at t=1 the three right-hand sides of [F2] are Ca2/2=2π π2A/60000, 12Ca3/2=π2A/6000 and π2A/6000+π2A/20000=13π2A/60000, using M2a2/8=Aa2/8=π2A/20000.

3.1step 2.1step 2.2algebra

Exact comparison: with a=π/50 one has ωa=2sin⁡(a/2)/a=100sin⁡(π/100)/π, so by step 2.1 the exact nodal error at t=1 obeys ∣ej(1)∣≤A∣100sin⁡(π/100)/π−1∣, while the theorem's nodal bound at t=1 is π2A/6000 by step 2.2; the comparison of the two explicit numerical factors is a finite check recorded in the Remarks.

4.1step 1.2F3F4algebra∎

Dispersion for all N≥2: put z=a/2>0. By [F4] and the fundamental theorem, sin⁡z−z=∫0z(cos⁡s−1) ds and cos⁡s−1=−∫0ssin⁡r dr; hence ∣sin⁡z−z∣≤∫0z∫0sr dr ds=z3/6, using ∣sin⁡r∣≤r, while ∣sin⁡z+z∣≤2z. Therefore ∣ωa2−1∣=4∣sin⁡2z−z2∣/a2≤4(z3/6)(2z)/a2=a2/12. At N=100 this equals π2/30000; here a<1 also permits the bound of [F3] with c=κ=1 and the chosen solving-mode frequency. Moreover ωa2=sin⁡2(a/2)/(a/2)2=1−a2/12+O(a4) by the power series of sine, so the exact error equals the bound to leading order in a.

Remarks

  • The comparison is a finite, exact check: the chain's standing mode has frequency ωa and the continuum mode frequency 1; the nodal error is the interference of the two cosines, so the discrepancy is a purely discrete-dispersion effect and decays like a2 for the exact standing-wave data, while the theorem's uniform-in-data bound grows like a3/2 through the worst-case nodal factor a−1/2 of the discrete norm comparison.

  • Numerical readings at N=100 for the bounds of step 2.2: 2π π2/60000≈0.0004124, π2/6000≈0.001645 and 13π2/60000≈0.002139, while the frequency-difference upper bound of step 3.1 is ∣100sin⁡(π/100)/π−1∣≈0.0001645, while the exact maximum nodal error factor is ∣cos⁡(100sin⁡(π/100)/π)−cos⁡1∣≈0.0001384 (nodes j=25,75 have ∣sin⁡(ja)∣=1) and the dispersion bound of step 4.1 is π2/30000≈0.000329; the exact dispersion error ∣ωa2−1∣=1−sin⁡2(π/100)/(π/100)2 agrees to leading order. The theorem's bounds are therefore satisfied and conservative on these data.

  • The evaluated numbers are properties of the model's bounds under the stated scaling m=ρℓa, ks=τs/a; they are not measured errors of any physical chain, and no measured stiffness or density is used.

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A Riemann shock and a rarefaction of the scalar model: explicit weak solutions, entropy coefficients and initial trace

Physical scope

A worked scalar-model example of shock and rarefaction weak solutions: the Riemann data 2 and 1 with the entropy coefficients of the shock computed on the interval (1,2), and the rarefaction fan of the data 1 and 2 checked for continuity, the classical equation inside the fan and convergence of the initial trace. The scalar conservation law u_t + (u^2/2)_x = 0 is a dimensionless idealized one-dimensional model; its scalar variable is not identified with a particular physical density or velocity. The example asserts no derivation from three-dimensional fluid mechanics and reports no measurement.

Example

Assume ACω (The Axiom of Countable Choice (ACω)) for the cited Lebesgue weak/entropy formulation.

Let F(u)=12u2 and use the weak and entropy formulations of Weak and entropy solutions of the scalar conservation law ut+(u2/2)x=0, with the scalar field u read as a dimensionless model variable. The coordinates t,x, the states uL,uR and flux F(u) are all dimensionless; no assignment to a measured density, velocity, length or time is made. Then:

  1. (Shock.) For the Riemann data uL=2, uR=1 the piecewise constant field u(t,x)=2 for x<32t and u(t,x)=1 for x>32t (t>0), taking the right-state value on the shock line, is a weak solution of ut+(F(u))x=0: its interface residual is −s[u]+[F(u)]=−32⋅(1−2)+12(12−22)=32−32=0 with s=32, so the weak identity (W) is satisfied for every test function by the split integration over the two half-planes.
  2. (Entropy of the shock.) For every k∈(1,2) the interface coefficient of the pair (ηk,qk)=(∣u−k∣,sign⁡(u−k)(u2−k2)/2) is s[ηk]−[qk]=−(k−2)(k−1)=(2−k)(k−1)>0, so the shock satisfies the entropy inequality with strictly positive interface production on this range of k; the integrated inequality is strict only for nonnegative tests with ∫0∞φ(t,st)dt>0; for k∉[1,2] the coefficient vanishes and the inequality holds with equality.
  3. (Rarefaction.) For the Riemann data uL=1, uR=2 the field u(t,x)=1 for x≤t, u(t,x)=x/t for t<x<2t and u(t,x)=2 for x≥2t (t>0) is continuous on (0,∞)×R, satisfies ut+(F(u))x=0 classically inside the fan, and has initial trace f: ∫R∣u(t,x)−f(x)∣ dx≤32t→0 as t↓0.
  4. (Weak kinks are unavoidable here.) The shock profile is discontinuous across x=32t and the rarefaction is not differentiable across x=t and x=2t; the classical derivation of the transport and balance identities of the continuum page does not apply at such sets, which is exactly why the weak formulation of the model is used. The admissibility of the shock and the equality case of the rarefaction are those of Riemann shock and rarefaction waves for ut+(u2/2)x=0 are weak solutions, and the shock is an entropy solution.

Facts & Assumptions

Given: Countable choice. the flux F(u)=u2/2; the Riemann data uL=2,uR=1 and uL=1,uR=2; the two explicit fields.

[F1]

Weak and entropy solutions (Weak and entropy solutions of the scalar conservation law ut+(u2/2)x=0): the weak identity (W) and the entropy inequality (E) for convex entropy pairs with q′=uη′, and the family (ηk,qk) with ηk(u)=∣u−k∣, qk(u)=sign⁡(u−k)(u2−k2)/2.

[F2]

Riemann theorem (Riemann shock and rarefaction waves for ut+(u2/2)x=0 are weak solutions, and the shock is an entropy solution): for uL>uR the shock with speed s=(uL+uR)/2 is a weak solution and satisfies every entropy inequality of the family (ηk,qk) with coefficient s[ηk]−[qk]=−(k−uL)(k−uR)≥0 for uR≤k≤uL, and coefficient 0 outside that interval; for uL<uR the rarefaction fan is continuous, is a weak solution and satisfies the entropy inequalities with equality.

[F3]

Integration (Integral over a measurable subset, The Lebesgue integral is linear on L1(μ)): the integral of a bounded measurable function over a set of finite measure, and additivity over the regions of the piecewise description.

Verification

technique · direct; compute the Rankine-Hugoniot residual and the entropy coefficients for the chosen data, and check the fan solution pointwise and its initial trace by explicit integration
1.1givenF1F2algebra

Shock residual: with uL=2,uR=1 the speed is s=(uL+uR)/2=3/2; [u]=uR−uL=−1 and [F(u)]=(uR2−uL2)/2=(1−4)/2=−3/2, so −s[u]+[F(u)]=3/2−3/2=0; this is the interface coefficient of the weak identity (W) when the field is integrated piecewise, so (W) holds for every test function.

1.2givenF1F2algebra

Rarefaction equation and continuity: inside the fan u=x/t gives ut=−x/t2, ux=1/t and u ux=x/t2, so ut+uux=0; at x=t the value is 1=uL and at x=2t it is 2=uR, matching the constant pieces, so u is continuous on the open upper half-plane.

2.1step 1.1F1F2algebra

Shock entropy: by [F2], for k∈[1,2] the coefficient is s[ηk]−[qk]=−(k−2)(k−1)=(2−k)(k−1)≥0, strictly positive for 1<k<2 because k−2<0 and k−1>0, and zero at k=1,2. For k<1 both states exceed k, so [ηk]=[u]=−1 and [qk]=[F]=−3/2, giving s[ηk]−[qk]=(3/2)(−1)−(−3/2)=0. For k>2 both states are below k, so [ηk]=−[u]=1 and [qk]=−[F]=3/2, again giving zero. Thus (E) holds for every nonnegative test. For 1<k<2 it is strict exactly when the test has positive integral on the shock line; zero or off-interface tests give equality, and for k∉[1,2] every test gives equality.

2.2step 1.2F2F3algebra

Initial trace: for 0<t one has u(t,x)≠f(x) only on the set where the fan and the constants differ, and ∫∣u−f∣≤∫0t∣1−2∣ dx+∫t2t∣x/t−2∣ dx=t+∫t2t(2−x/t) dx=t+t/2=3t/2→0 as t↓0, by additivity and evaluation of the elementary integrals [F3]; moreover the entropy inequality of the fan holds with equality by [F2].

3.1step 1.1step 1.2F1∎

Regularity reading: the shock is discontinuous and the fan fails to be differentiable across x=t and x=2t; hence the classical smooth-motion hypotheses of the balance and transport items of this page are not met on these sets, and the weak formulation of [F1] is the correct setting for these solutions. This is a statement about the models, not an empirical claim.

Remarks

  • Physical reading. The dimensionless scalar field u is a model variable of an idealized one-dimensional transport problem; it is not claimed to be the velocity or density of a three-dimensional compressible fluid, and no derivation of the scalar equation from the momentum and mass balances of this page is asserted. The example shows that a scalar continuum model can have nondifferentiable weak solutions whose admissibility is controlled by entropy inequalities, in contrast with the smooth motions required by the transport and balance theorems of this page.

  • Admissibility is not automatic. Both the shock and the fan are weak solutions; only the entropy inequalities select the physically admissible one among weak solutions of this model family. The computed coefficients show the shock is admissible for the stated data and the fan is the equality case. No statement is made about entropy solutions for general initial data or for systems of conservation laws.

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Poiseuille and Couette channel flows of the viscous branch: explicit profiles, flux and wall data

Physical scope

A worked steady plane channel problem of the adopted incompressible Newtonian branch: the Poiseuille profile with pressure gradient 6, height 2 and viscosity 3 is verified against the model's momentum equation with zero body force, its flux per unit width 4/3 and centre speed 1 are computed, the Couette profile is verified with its nonzero curl, and the no-slip wall conditions are recorded as adopted ideal boundary data. The example reports no measurement.

Example

Adopt the incompressible Newtonian branch of Adopted fluid constitutive branches: incompressible Newtonian, barotropic inviscid, and the periodic-cell idealization with constant density ρ>0, dynamic viscosity η=3 Pa s and channel height h=2 m, whose SI coordinate domain is O=R×(0,2)×R with coordinates (x,y,z), in the steady description and with no body force, and explicitly adopt the steady incompressible model equation ρ(u⋅∇)u=−∇p+ηΔu together with div⁡u=0 (Incompressible Newtonian and barotropic inviscid fluid constitutive models). Here displayed coordinate profiles and numbers are SI numerical values: v has units m s−1, the flux per width has units m2 s−1, x,y,z are in metres and p is in pascals. Deriving the adopted differential equation from integral balances would additionally require the mass and force premises of The momentum equation of the continuum model: local form rho D_t u = rho b + div sigma; those are not inferred from a constitutive law alone. For a C1 spatial field w=(w1,w2,w3), define curl⁡w:=(∂yw3−∂zw2,∂zw1−∂xw3,∂xw2−∂yw1); irrotational means this vector vanishes, equivalently the spatial derivative matrix is symmetric. Then:

  1. (Poiseuille.) With pressure gradient G=6 Pa m−1, i.e. p(x)=p0−6x, the profile u=(v(y),0,0), v(y)=y(2−y) (the value Gy(h−y)/(2η) of the general formula with h=2,η=3) satisfies div⁡u=0 and ηv′′(y)=−6=−G, hence the steady momentum equation with no body force; it satisfies the no-slip data v(0)=v(2)=0; its flux per unit width is ∫02v(y) dy=4/3 and its centre speed is v(1)=1.
  2. (Couette.) With constant pressure and wall speed V=2 m s−1, the profile v(y)=Vy/2=y satisfies the same equations with zero body force and the boundary data v(0)=0, v(2)=2; its velocity gradient Du=(010000000) is not symmetric, so the flow is not irrotational: curl⁡u=(0,0,−V/h)=(0,0,−1).
  3. (Uniqueness in the ansatz.) Within the ansatz u=(v(y),0,0), p=p0−Gx, the difference of two profiles with the same G and the same no-slip data satisfies w′′=0 with w(0)=w(2)=0, hence w≡0: the Poiseuille profile is the unique steady solution in this class with those data.
  4. (Reading.) The wall conditions are adopted ideal boundary data: the model is used with the no-slip assumption v=0 at the fixed walls, which is the idealization recorded in Adopted fluid constitutive branches: incompressible Newtonian, barotropic inviscid, and the periodic-cell idealization; the profiles are exact solutions of the model and are not approximations within it. Dimensions: [G]=μℓ−2τ−2, so [Gh3/η]=ℓ2τ−1 (flux per unit width) and [Gh2/η]=ℓτ−1 (speed), consistently with Continuum body data, the fixed inertial frame and the dimensions of the fields, Dimensions and SI unit conventions of the non-relativistic classical mechanics framework.

Facts & Assumptions

Given: the branch data ρ>0, η=3; the channel height h=2; the gradients G=6 and V=2; the profiles.

[F2]

Channel-flow theorem (Exact plane Poiseuille and Couette flows of the incompressible Newtonian model, with flux and ansatz uniqueness): with h>0, G∈R, v(y)=Gy(h−y)/(2η), p=p0−Gx, the field u=(v,0,0) satisfies the steady equations, has v(0)=v(h)=0, flux Gh3/(12η), and is unique in the ansatz u=(v(y),0,0), p=p0−Gx with these boundary data; the Couette profile v=Vy/h with constant pressure satisfies the equations with v(0)=0,v(h)=V and nonsymmetric gradient for V≠0.

[F3]

Calculus (Euclidean spatial calculus: gradient, divergence and material derivative): componentwise (u⋅∇)u and Δu, together with curl⁡ as defined in the Example for fields of the form u=(v(y),0,0), so that (u⋅∇)u=0 and Δu=(v′′,0,0).

[F4]

Mean value theorem (The mean value theorem, as the case g(x)=x of Cauchy's: for f continuous on [a,b] with a<b and differentiable on (a,b) there is c∈(a,b) with f(b)−f(a)=f′(c)(b−a)): if a real function is continuous on a compact interval and differentiable in its interior, its increment equals its derivative at some interior point times the interval length. In particular a function with zero derivative is constant on each compact subinterval of its open interval of definition.

Verification

technique · direct; substitute the explicit profiles into the model's equations, integrate for the flux, and evaluate the uniqueness difference equation
1.1givenF1F2F3algebra

Poiseuille equations: v(y)=6y(2−y)/6=y(2−y) gives v(0)=v(2)=0, v′(y)=2−2y, v′′=−2 and, by [F3], Δu=(−2,0,0)=(−η−1G,0,0) with η=3, G=6; since (u⋅∇)u=0 and ∇p=(−6,0,0), the steady momentum equation ρ(u⋅∇)u=−∇p+ηΔu holds identically, and div⁡u=∂xv=0.

1.2givenF1F2F3algebra

Couette: with v(y)=y, v′′=0 so ηΔu=0; with constant pressure ∇p=0; and v(0)=0,v(2)=2; the gradient matrix has the single nonzero entry ∂yv=1, which is not symmetric and gives curl⁡u=(0,0,−∂yv)=(0,0,−1).

2.1step 1.1F2algebra

Flux and centre speed: ∫02y(2−y) dy=[y2−y3/3]02=4−83=43, matching Gh3/(12η)=6⋅8/36=43, and v(1)=1, matching Gh2/(8η)=6⋅4/24=1.

2.2step 1.1F2F4algebra

Uniqueness in the ansatz: let v1,v2∈C([0,2])∩C2((0,2)) be two profiles with the same G and no-slip data, as in [F2]. Their difference w satisfies w′′=0 on (0,2) and w(0)=w(2)=0. Apply [F4] to w′ on every compact subinterval of (0,2) to obtain one constant c=w′(y) throughout the interior. Applying [F4] to w(y)−cy gives w(y)=cy+d there. Continuity extends this affine formula to both endpoints; w(0)=0 gives d=0 and w(2)=0 gives 2c=0, hence w≡0. No derivative at a wall is assumed.

3.1step 2.1step 1.2F1algebra∎

Reading: the no-slip conditions are exactly the adopted wall data of the branch's idealization, and the two profiles are exact solutions of the model on the channel; the dimensional checks [G]=μℓ−2τ−2, [Gh3/η]=ℓ2τ−1, [Gh2/η]=ℓτ−1 hold by the rules of Dimensions and SI unit conventions of the non-relativistic classical mechanics framework. No measured viscosity, pressure or flux is asserted.

Remarks

  • The example exhibits the branch's structure: a parabolic profile driven by a constant pressure gradient, a linear profile driven by a moving wall, the nonzero vorticity of the latter, and the uniqueness of the former inside the stated ansatz. Nothing is asserted about stability of these flows, about entrance and exit regions, or about flows at higher rates where the laminar ansatz or the no-slip idealization may fail.

  • The channel data are chosen so that the arithmetic is exact (h=2,η=3,G=6); the same formulas appear in the cited treatments for general data, and no numerical coincidence carries physical meaning.

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Periodic shear fields: an exact steady Euler solution, failure for the viscous branch, and the classification of steady periodic shears

Physical scope

Worked checks on the periodic cell of the adopted fluid branch: the sinusoidal shear is verified to be an exact steady solution of the inviscid (Euler) branch with zero pressure and to fail the local existence theorem's projected equation for the viscous branch; among classical steady periodic shears with a C^3 velocity profile and C^2 pressure, the viscous branch with no body force admits only constant profiles. The example uses the periodic-cell idealization and reports no measurement.

Example

Assume ACω (The Axiom of Countable Choice (ACω)) for the cited periodic Sobolev and local-evolution suppliers.

Use the dimensionless variables of Adopted fluid constitutive branches: incompressible Newtonian, barotropic inviscid, and the periodic-cell idealization clause (c): t,x,u in this example denote the scaled time, unit-torus position and velocity, ν=η/(ρU∗L∗), and p=Pm/(ρU∗2). The physical fields are restored by uphys=U∗u(t/T∗,x/L∗), Pm=ρU∗2p(t/T∗,x/L∗). Work on the periodic cell T3=(R/Z)3 of Adopted fluid constitutive branches: incompressible Newtonian, barotropic inviscid, and the periodic-cell idealization clause (c), with constant density ρ>0, no body force and the stress of the branch. The variables and field values here are dimensionless. Let A>0 be a dimensionless velocity amplitude and φ∈R a dimensionless phase, and

u(t,x):=(Asin⁡(2πx2+φ),0,0).

Then:

  1. div⁡u=0 and (u⋅∇)u=0, so with p≡0 the field is an exact steady solution of the Euler branch (ν=0) of the model on the periodic cell: ∂tu+P((u⋅∇)u)=νΔu holds as 0=0, and the primitive equation ∂tu+(u⋅∇)u=−∇p+νΔu holds with p≡0;
  2. the field satisfies the hypotheses of Local existence, uniqueness and pressure reconstruction for the incompressible fluid model on the periodic cell: it is smooth, divergence-free, periodic and has finite Hs norm (s≥4), and the displayed global solution is consistent with the local existence-uniqueness statement;
  3. for the viscous branch (ν>0) the field is not a solution: Δu=−(2π)2u≠0 and PΔu=Δu because u is divergence-free, so the projected equation would require −ν⋅(2π)2u=0, which fails for A>0;
  4. among classical periodic shears u=(v(x2),0,0) with v∈C3(T) and periodic pressure p∈C2(T3), every steady solution of the viscous branch with no body force and constant density is constant: the dimensionless equations force ∇p=ν(v′′(x2),0,0), and periodicity of p in x1 together with periodicity of v in x2 forces v′′≡0 and then v≡const.

Facts & Assumptions

Given: Countable choice; the branch data ρ>0, ν=η/(ρU∗L∗); the periodic cell; the field u; and the classical shear class stated in clause 4.

[F1]

Branch and projected equation (Adopted fluid constitutive branches: incompressible Newtonian, barotropic inviscid, and the periodic-cell idealization, Incompressible Newtonian and barotropic inviscid fluid constitutive models, Local existence, uniqueness and pressure reconstruction for the incompressible fluid model on the periodic cell): for the incompressible branch the field equations are div⁡u=0 and, in the projected form on the periodic cell, ∂tu+P((u⋅∇)u)=νΔu; for ν=0 this is the Euler branch and for the primitive form the pressure gradient enters with the opposite sign.

[F2]

Periodic calculus (Periodic vector Sobolev spaces on the three-torus, the weight family, and the Leray projection, Euclidean spatial calculus: gradient, divergence and material derivative, Ck Euclidean maps and diffeomorphisms, The derivatives of sine and cosine are cosine and minus sine): on the torus, fields are identified with their periodic representatives; for u=(Asin⁡(2πx2+φ),0,0) one has ∂2u1=2πAcos⁡(2πx2+φ) and ∂22u1=−(2π)2Asin⁡(2πx2+φ), so div⁡u=0, Δu=−(2π)2u and PΔu=Δu because u is divergence-free; smoothness and finiteness of all Hs norms follow from the smooth periodic formula.

[F3]

Integral of a derivative (The second fundamental theorem: if G is differentiable on [a,b] with G′=f and f is integrable, then ∫abf=G(b)−G(a), A continuous function on [a,b] is Riemann integrable, by Heine-Cantor and Riemann's criterion): for a C1 real function q on an open interval containing [a,b], q′ is continuous and hence Riemann integrable on [a,b], and q(b)−q(a)=∫abq′(s) ds; endpoint derivatives are the restrictions of the ordinary derivatives. For a 1-periodic C1 representative this gives ∫01q′=0. Applying the same identity on any compact subinterval also shows that a zero derivative forces constancy there.

Verification

technique · direct; compute divergence and convection for the shear, substitute into both branches of the projected equation, and integrate the pressure equation to classify steady shears
1.1givenF2

Kinematics of the shear: u has only its first component, which depends only on x2, so div⁡u=∂1u1=0 and (u⋅∇)u=u1∂1u=0 because ∂1u=0; the field is C∞ and periodic with all Hs norms finite.

1.2givenF1F2F3algebra

Classification setup: let u=(v(x2),0,0) be a steady periodic shear of the viscous branch, so ν>0, with constant density, no body force, v∈C3(T) and p∈C2(T3). Then div⁡u=0, (u⋅∇)u=0 and Δu=(v′′,0,0). The primitive equation 0=−∇p+νΔu reads ∂1p=νv′′(x2) and ∂2p=∂3p=0. Fixing x2,x3 and applying [F3] to the periodic representative of p on [0,x1] for x1>0 gives p(x1,x2,x3)−p(0,x2,x3)=νv′′(x2)x1. In particular the formula holds at x1=1.

2.1givenstep 1.1F1F2

Euler branch: with ν=0, (u⋅∇)u=0 and ∂tu=0, so the projected equation reads 0+P0=0 and is satisfied; the primitive equation with p≡0 (zero mean, as required by the periodic convention) reads 0=0. Hence the field is an exact steady Euler solution, and it meets the hypotheses of the local theorem; the theorem's uniqueness statement is consistent with this exact global solution.

2.2givenstep 1.1F1F2algebra

Viscous branch: by [F2], Δu=−(2π)2u and PΔu=Δu, so the projected equation would read 0+0=νΔu=−ν(2π)2u; since A>0 the field u is not identically zero and the identity fails for every ν>0.

3.1step 1.2F3algebra∎

Periodicity: since p is 1-periodic in x1, step 1.2 at x1=1 gives 0=νv′′(x2) for every x2, and ν>0 gives v′′≡0. Apply [F3] to v′ on any compact subinterval of its real periodic representative: all increments vanish, so v′=α is constant. A second application gives v(x2)=αx2+β; v(1)=v(0) forces α=0. Conversely, constant v with constant zero-mean pressure satisfies the equations by zero derivatives. Thus the steady periodic viscous shear profiles are exactly the constants.

Remarks

  • The example separates the two branches sharply on the same data: the shear is an exact Euler solution and not even a solution of the viscous projected equation, because constant positive viscosity diffuses the shear on the periodic cell. The classified steady viscous shears are exactly the constants, i.e. the trivial shears.

  • The pressure in clause 4 is forced to be linear in x1 before periodicity kills the slope; this is the periodic-cell analogue of the constant pressure gradient of the channel example, and it shows that on a periodic cell a steady viscous shear cannot be driven. No measurement and no stability claim is made.

CounterexampleConstruction: AI-generatedVerification: AI-generatedprecheck passOpen item page →

FALSE: the reversed-normal convention alone makes a continuous traction field a stress matrix. The field t(n)=|n_1|n refutes it

Statement refuted

The false statement is: every continuous traction field t:S2→R3 satisfying the reversed-normal convention t(−n)=−t(n) for every n∈S2 is represented by a matrix σ∈M3(R) with t(n)=σn for every n.

The field constructed below is continuous and satisfies the convention, and inherits Cauchy's hypothesis (it depends on the surface only through the unit normal), but no matrix represents it. The refutation shows that the balance hypothesis of the Cauchy-tetrahedron theorem is essential: symmetry of the traction in the normal alone is not enough.

Facts & Assumptions

Given: the unit sphere S2={n∈R3:∥n∥2=1}, the first standard basis vector e1, and the map

t:S2⟶R3,t(n):=∥⟨n,e1⟩2 e1∥2  n.

Write n1:=⟨n,e1⟩2, so t(n)=∣n1∣ n with ∣n1∣=∥n1e1∥2.

[F1]

Traction and representation (Traction fields and stress matrices representing them, The vector space Mm×n(F):=F m×n of m by n matrices over a field, with entrywise operations, Rectangular matrix multiplication and the identity matrix In, including zero-sized shapes): a matrix σ represents t when t(n)=σn for every n∈S2; the columns of σ are then determined by σej=t(ej); and t(−n)=−t(n) is the reversed-normal convention, which is a property and not a definition.

[F3]

Sphere and basis (Euclidean spheres and closed balls as subspaces of Rn, The Euclidean inner product ⟨x,y⟩=∑k<nxkyk on Rn): e1,e2,e3 and n∗:=(e1+e2+e3)/3 all belong to S2, with ⟨ej,e1⟩2=δj1 and ⟨n∗,e1⟩2=1/3; and ∥−v∥2=∥v∥2 for every v∈R3 by symmetry of the inner product.

Counterexample

technique · direct; verify continuity and the reversed-normal convention, then assume a representing matrix and derive a contradiction by evaluating at the diagonal direction
1.1givenF2F3algebra

Continuity and reversed normals: by [F2] the field t is continuous on S2. For n∈S2, [F3] gives ∥⟨−n,e1⟩2e1∥2=∥−n1e1∥2=∥n1e1∥2, so t(−n)=∣n1∣(−n)=−∣n1∣n=−t(n): the reversed-normal convention holds.

1.2givenF1F3algebra

Assume a representing matrix: suppose σ∈M3(R) satisfies t(n)=σn for all n∈S2. Evaluating at the basis vectors, [F1] and [F3] give σe1=t(e1)=∣1∣e1=e1, σe2=t(e2)=∣0∣e2=0 and σe3=0; hence σ=diag(1,0,0).

2.1step 1.2F1algebra∎

Contradiction: at n∗=(e1+e2+e3)/3∈S2 one has t(n∗)=∣1/3∣ n∗=n∗/3=(1/3)(1,1,1), while σn∗=(1/3,0,0). These vectors differ (their second and third components are 1/3 and 0 respectively), contradicting the assumed representation for every n. Hence no matrix represents t, although t is continuous, satisfies Cauchy's hypothesis in the sense that it depends on the surface only through its unit normal, and satisfies the reversed-normal convention.

Remarks

  • The counterexample isolates the missing hypothesis: the Cauchy-tetrahedron theorem derives the matrix from the balance of contact forces on shrinking regions, not from the symmetry of the traction in the normal. The field above is not balanced on all admissible regions; by the cited theorem, the balance condition must fail for it, and continuity plus the reversed-normal convention are insufficient on their own.

  • The physical reading is the corresponding warning for the model page: the representation of contact forces by a stress matrix is a consequence of the adopted balance principles, not of the format of the traction field, and a model whose contact forces violate the balance hypotheses lies outside the Cauchy continuum framework.

Sources