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Rigid observer calculus and objective strain rate

Statement

Let I⊆R be a nonempty open interval. For r=1,2, Cr means that all coordinate partial derivatives through total order r exist and are continuous. Let U⊆R3 be open and let χ∈C2(I×U,R3) be such that every slice χt:U→χt(U) is a bijection with C2 inverse and J(t,a):=det⁡Daχ(t,a)>0, where Daχ is the matrix of reference-coordinate partial derivatives. Write H(t,a):=(t,χ(t,a)) and Ω:={(t,x):t∈I, x∈χt(U)}. The map H is injective and its derivative is block triangular with determinant J>0, so the inverse function theorem gives local C1 inverses; injectivity makes them agree on overlaps. Hence Ω is open and the joint inverse A(t,x):=χt−1(x) is C1. Define u(t,x):=∂tχ(t,A(t,x)), which is C1. For any C1 vector field f on Ω, let Dxf be its matrix of spatial coordinate partial derivatives and define Dtf:=∂tf+(Dxf)u. Set L:=Dxu, D:=(L+LT)/2, W:=(L−LT)/2, θ:=tr⁡L, and am:=Dtu. Here tr⁡M:=∑iMii for a square matrix M, I3 denotes the 3×3 identity matrix, and

SO(3):={Q∈R3×3:QTQ=I3, det⁡Q=1}.

Let Q∈C2(I,SO(3)) and c∈C2(I,R3), hold time fixed, and change spatial coordinates by x∗=Q(t)x+c(t). This map preserves Euclidean distances and orientation because QTQ=I3 and det⁡Q=1; the coordinate change does not assert that the observer is inertial. Set χ∗(t,a):=Q(t)χ(t,a)+c(t) and Ω∗:={(t,x∗):t∈I, x∗=χ∗(t,a) for some a∈U}. Define the transformed velocity, material derivative, rate tensors and acceleration from χ∗ by the same formulas on Ω∗; in particular, Dt∗f=∂tf+(Dx∗f)u∗ and am∗:=Dt∗u∗. For corresponding points x=χ(t,a) and x∗=χ∗(t,a), the transformed fields satisfy

u∗(t,x∗)=Q′(t)x+Q(t)u(t,x)+c′(t),L∗(t,x∗)=Q(t)L(t,x)Q(t)T+Q′(t)Q(t)T,

D∗(t,x∗)=Q(t)D(t,x)Q(t)T,W∗(t,x∗)=Q(t)W(t,x)Q(t)T+Q′(t)Q(t)T,θ∗(t,x∗)=θ(t,x).

Thus D transforms objectively, meaning its transformed tensor components obey D∗=QDQT under every such Q,c; W acquires the observer spin Q′QT and is not objective under general time-dependent rotations. If am:=Dtu is the material acceleration, then

am∗(t,x∗)=Q(t)am(t,x)+2Q′(t)u(t,x)+Q′′(t)x+c′′(t).

When Q′=0 and c′′=0, the acceleration formula reduces to am∗=Qam. These are mathematical kinematic identities and assert no force law or balance equation.

Facts & Assumptions

Given: The motion, the C2 maps Q,c, and the spatial transformation in the statement.

[F1]

The Euclidean inverse function theorem: a C1 map on an open subset of Rn, n≥1, with invertible derivative at a point has a local C1 inverse there. The fields u,Dt,L,D,W,θ in this lemma are defined in its statement; no reference body or distinguished time is required.

[F2]

The chain rule for total derivatives: D(g∘f)(a)=Dg(f(a))∘Df(a): derivatives of composable totally differentiable Euclidean maps multiply in the stated order.

Proof

1.1givenF1F2algebra

The given C2 map H(t,a)=(t,χ(t,a)) is injective on the open set I×U and has invertible derivative, since its block-triangular derivative has determinant J>0. By [F1] its local C1 inverses patch by injectivity, so its image Ω is open and its inverse label A is C1. The event map (t,x)↦(t,Q(t)x+c(t)) has the C2 inverse (t,x∗)↦(t,Q(t)T(x∗−c(t))). Thus Ω∗ is open and A∗(t,x∗)=A(t,Q(t)T(x∗−c(t))) is C1 by [F2]; both induced velocities are C1. For fixed a, differentiate χ∗=Qχ+c in time and use the given velocity definitions to obtain u∗(t,x∗)=Q′x+Qu+c′ at x=χ(t,a).

2.1givenF2step 1.1algebra

Along the material curve x(t)=χ(t,a), the given definitions and [F2] give ddtu(t,χ(t,a))=∂tu+(Dxu)∂tχ=Dtu(t,χ(t,a))=am(t,x).

2.2F2step 1.1algebra

Since x=QT(x∗−c), its spatial derivative at fixed t is Dx∗x=QT. Apply [F2] to the x∗ derivative of the velocity formula in step 1.1 to get L∗=(Q′+QL)QT=QLQT+Q′QT.

3.1givenF2step 1.1step 2.1algebra

By the given transformed-field definitions and [F2], am∗(t,x∗(t))=ddtu∗(t,χ∗(t,a))=d2dt2χ∗(t,a)=d2x∗dt2. Differentiate x∗(t)=Q(t)x(t)+c(t) twice; the product rule gives d2x∗dt2=Q′′x+2Q′u+Qd2xdt2+c′′. Substituting step 2.1 gives the displayed transformation law for am∗.

4.1step 2.2algebra∎

Differentiating QQT=I3 gives Q′QT+Q(Q′)T=0, so Ω:=Q′QT is skew-symmetric. Taking the symmetric and skew-symmetric parts of step 2.2 yields D∗=QDQT and W∗=QWQT+Ω. The finite-sum trace identity gives tr⁡(QLQT)=tr⁡L, while a skew-symmetric matrix has zero diagonal, hence tr⁡Ω=0 and θ∗=θ.

Depends on

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