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Total momentum, kinetic-energy splitting and centre-of-mass angular momentum of a rigid-material motion

Physical scope

Conditional inertial identities of the rigid-material model branch of Adoption of the rigid-material model branch: reference mass distribution, rigid placements, orientation and scope along a C2 motion in one inertial frame: the total momentum equals the total mass times the centre-of-mass velocity; the kinetic energy splits into the centre-of-mass term and the rotational term 12ωTIω; and the angular momentum about the centre of mass equals RIω. The statements are identities for the model's measure, motion and inertia data, under the countable-choice assumption used only for the finiteness of the integrals. No conservation law, no force law and no measured value is asserted.

Statement

Assume the Axiom of Countable Choice ACω (The Axiom of Countable Choice (ACω)), used only to make the integrals below finite. Adopt the model and notation of Adoption of the rigid-material model branch: reference mass distribution, rigid placements, orientation and scope: a reference mass distribution ν with total mass m and centred reference coordinates, a fixed inertial frame, and a motion x(t,ρ)=c(t)+R(t)ρ with configuration path (c,R) of class C2 on the time window I0, body angular velocity ω (Body and spatial angular velocity of a rigid-material motion, and the material velocity field) and body inertia matrix I (Inertia matrix, spatial inertia tensor, inertia tensor about a point and moment of inertia about an axis of a rigid-material model). Define the total momentum, kinetic energy and angular momentum about the centre of mass of the model along the motion by the componentwise integrals P(t):=∫∂tx(t,ρ) dν(ρ),K(t):=12∫∥∂tx(t,ρ)∥22 dν(ρ), Lc(t):=∫(x(t,ρ)−c(t))×(∂tx(t,ρ)−c′(t)) dν(ρ), with dimensions μℓτ−1, μℓ2τ−2 and μℓ2τ−1 (Dimensions and SI unit conventions of the non-relativistic classical mechanics framework). Then for every t∈I0:

  1. the three integrands are ν-integrable, so P(t), K(t) and Lc(t) are a well-defined finite vector and finite real numbers;
  2. P(t)=m c′(t);
  3. K(t)=12m∥c′(t)∥22+12ω(t)TIω(t);
  4. Lc(t)=R(t) I ω(t).

The identities hold for every C2 configuration path; no equation of motion, force law or conservation statement is used or asserted.

Facts & Assumptions

Given: The model data of Adoption of the rigid-material model branch: reference mass distribution, rigid placements, orientation and scope, one inertial frame, a C2 motion x(t,ρ)=c(t)+R(t)ρ, its body angular velocity ω, its body inertia matrix I, and a time t∈I0.

[L1]

The mathematical supplier (Kinetic energy and angular momentum of a rigid placement: K=12m∥c′∥22+12ωTIω and Lc=RIω): under ACω, for a centred mass distribution ν with total mass m and inertia matrix I, an interval J with at least two points, differentiable c:J→R3 and R:J→SO(3) and the rigid placement x(t,ρ)=c(t)+R(t)ρ with body angular velocity ω, the identities ∂tx(t,ρ)=c′(t)+R(t)(ω(t)×ρ), the integrability of ∥∂tx∥22 and of the angular-momentum integrand, and the identities of clauses 2 and 3 hold; the integral definitions of K and Lc there are the ones displayed in the statement.

[L2]

The model's definitions (Body and spatial angular velocity of a rigid-material motion, and the material velocity field, Inertia matrix, spatial inertia tensor, inertia tensor about a point and moment of inertia about an axis of a rigid-material model): ω is the unique vector with RTR′=[ω]× and ωs=Rω; I=I(ν) is the body inertia matrix; ∫ρ dν=0 and m=ν(R3).

[L3]

Integrability and integral rules (Finiteness of the moments of a bounded finite Borel measure on R3, Mass distributions on R3: total mass, first moment and inertia matrix, The Lebesgue integral is linear on L1(μ), Integral over a measurable subset, Integrable real and complex functions, and their integrals, The nonnegative Lebesgue integral, The integral of a nonnegative simple function): the coordinate functions ρ↦ρj are ν-integrable and bounded on the support; the constant function satisfies ∫1 dν=m; integrals of real integrable functions are linear, and vector integrals are componentwise.

Proof

technique · direct; the rotational identities are the cited mathematical supplier, and the total-momentum identity is the centring of the reference mass distribution together with linearity of the integral
1.1givenL1L2

The hypotheses of [L1] are met with the interval I0 and the differentiable maps c and R: the measure ν is a centred mass distribution with total mass m by [L2], I0 is nondegenerate by Adoption of the rigid-material model branch: reference mass distribution, rigid placements, orientation and scope clause (ii), and C2 implies differentiability. Clause 1 of [L1] gives ∂tx(t,ρ)=c′(t)+R(t)(ω(t)×ρ) for every ρ, and the ν-integrability of the kinetic-energy integrand and of the angular-momentum integrand.

2.1step 1.1L2L3

The momentum integrand is a finite sum of the constant functions ρ↦cj′(t) and the linear functions ρ↦(R(t)(ω(t)×ρ))j, which are finite real linear combinations of the coordinate functions ρ↦ρl; these are ν-integrable and bounded on the support by [L3], so the momentum integrand is ν-integrable by linearity of the integral [L3]. Together with step 1.1 this proves clause 1.

2.2step 1.1L1

Kinetic energy: clause 2 of [L1] gives, for the same placement data, K(t)=12∫∥∂tx(t,ρ)∥22 dν(ρ)=12m∥c′(t)∥22+12ω(t)TIω(t), which is clause 3.

3.1step 2.1L2L3algebra

Total momentum: by step 1.1, linearity of the integral and the componentwise reading of vector integrals [L3], P(t)=∫(c′(t)+R(t)(ω(t)×ρ)) dν(ρ)=c′(t)∫1 dν+R(t)∫(ω(t)×ρ) dν(ρ). The first integral is m by [L3]. The second integral is zero componentwise: for example its first component is ω2(t)∫ρ3 dν−ω3(t)∫ρ2 dν=0, and its second and third components are the cyclic analogues, since ∫ρ dν=0 by [L2] and each finite linear combination commutes with integration by [L3]. Hence P(t)=mc′(t), which is clause 2.

4.1step 1.1L1∎

Angular momentum: clause 3 of [L1] gives Lc(t)=∫(x(t,ρ)−c(t))×(∂tx(t,ρ)−c′(t)) dν(ρ)=R(t)Iω(t), which is clause 4.

Remarks

  • Instantaneous identities. The three displayed identities are identities at each time for the stated motion; they do not say that either term of the kinetic splitting is conserved, and no equation of motion for (c,R) enters. The terms are the model's translational kinetic energy 12m∥c′∥22 and rotational kinetic energy 12ωTIω.

  • Frame dependence of the two terms. The centre-of-mass velocity c′ and hence the translational term depend on the inertial frame; the rotational term 12ωTIω is built from the body angular velocity and the body inertia matrix and is therefore unchanged by a change of inertial frame. The precise transformation laws are proved in Behaviour of the rigid-material configuration, angular velocity, inertia data and inertial quantities under a change of inertial frame on this page.

  • The countable-choice hypothesis. ACω is used only to make the integrals finite through [L1] and [L3]; the algebraic identities themselves are choice-free once the integrals exist. A consumer that needs the identities under weak hypotheses must carry this assumption.

  • Degenerate shapes remain allowed. The identities hold for every mass distribution of the branch, including those supported on a line; in that case Iω is not injective in ω, so the angular momentum does not determine the body angular velocity, as the companion page's counterexample exhibits.

Depends on

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