Stress theory for classical fields
Raz Kupferman, Elihu Olami, Reuven Segev

TL;DR
This paper develops a geometric framework for classical field theories and continuum mechanics, representing configurations as sections of fiber bundles and stresses as generalized force objects within this setting.
Contribution
It introduces a unified geometric approach to classical fields and continuum mechanics, including a representation theorem for stresses and analysis of constitutive relations.
Findings
Existence of a stress object representing forces, though non-unique
Configuration space modeled as an infinite-dimensional manifold
Role of constitutive relations analyzed within the geometric framework
Abstract
Classical field theories together with the Lagrangian and Eulerian approaches to continuum mechanics are embraced under a geometric setting of a fiber bundle. The base manifold can be either the body manifold of continuum mechanics, space manifold, or space-time. Differentiable sections of the fiber bundle represent configurations of the system and the configuration space containing them is given the structure of an infinite dimensional manifold. Elements of the cotangent bundle of the configuration space are interpreted as generalized forces and a representation theorem implies that there exist a stress object representing forces, non-uniquely. The properties of stresses are studies as well as the role of constitutive relations in the present general setting.
| Objects | Elements of | Notation |
| Points in the field (base manifold) | ||
| Values of a field | ||
| Configurations | ||
| Virtual velocities | ||
| Velocities at | ||
| Generalized forces | ||
| Forces at | ||
| Body force densities | ||
| Body force density field at | ||
| Surface force densities | ||
| Surface force density field at | ||
| Deformation jets | ||
| Velocity jets | ||
| Velocity jets at | ||
| Variational stresses | ||
| Variational stresses at | ||
| Variational stress densities | ||
| Variational stress density fields at | ||
| Traction stress densities | ||
| Traction stress density fields at | ||
| Loadings | ||
| Body loading densities | ||
| Surface loading densities | ||
| Loading potentials | ||
| Body loading potential densities | ||
| Boundary loading potential densities | ||
| Constitutive relations | ||
| Constitutive densities | ||
| Elastic energy | ||
| Elastic energy density |
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Stress Theory for Classical Fields
Raz Kupferman∗, Elihu Olami∗
∗Einstein Institute of Mathematics, The Hebrew University of Jerusalem Jerusalem, 9190401, Israel
and
Reuven Segev*∗∗*
*∗∗*Department of Mechanical Engineering, Ben-Gurion University of the Negev, Beer-Sheva 84105, Israel
Abstract.
Classical field theories together with the Lagrangian and Eulerian approaches to continuum mechanics are embraced under a geometric setting of a fiber bundle. The base manifold can be either the body manifold of continuum mechanics, space manifold, or space-time. Differentiable sections of the fiber bundle represent configurations of the system and the configuration space containing them is given the structure of an infinite dimensional manifold. Elements of the cotangent bundle of the configuration space are interpreted as generalized forces and a representation theorem implies that there exist a stress object representing forces, non-uniquely. The properties of stresses are studies as well as the role of constitutive relations in the present general setting.
MSC codes: 74A10, 53Z05, 74A60
Contents
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5.4 The traction stress induced by a variational stress density
-
5.5 The exterior jet of a differentiable traction stress density
-
6.4 The differential form of the continuum mechanics equations
1. Introduction
Physical theories for which the states are represented by sections of a fiber bundle are predominant in both classical field theories of theoretical physics and studies of the material structure of bodies in continuum mechanics. This paper is concerned with the corresponding stress theory.
For about half a century now, classical fields are modeled mathematically in the theoretical physics literature as sections of fiber bundles over space-time. Since the pioneering works on modern formulations of classical field theories, for example, [Tra67, Kom68, Kom69, Śniatycki70, Her70, Kru71], a generic field is viewed as a section of a fiber bundle for a -dimensional space-time . The field equations are obtained by considering stationary values of an action integral
[TABLE]
where the Lagrangian function is a fiber preserving mapping of -jets into the bundle of -alternating multilinear forms over . (See, for example, [KT79, dR85, BSF88, EEMLRR96, Ram01, GIMM03, GMS09, Fra12].) The variational analysis of the action integral yields terms that may be interpreted as the components of the stress tensor.
Nontrivial fiber bundles appeared in continuum mechanics originally in works considering dislocations, and material uniformity and homogeneity. (See, [BBS55, Kon55, Nol67, Wan67, Blo79, EE07].) The modern formulations of these theories usually consider sections of the principal bundle of frames, or moving frames, over the body manifold as a mathematical model for the distributions of material directions. Since the sections are defined over the body manifold, no reference should be made to the physical space and its conceivable Euclidean structure.
Formulation of continuum mechanics using sections of a general fiber bundle has an additional advantage. While a major portion of studies in continuum mechanics use the Lagrangian approach in which material points serve as fundamental objects, the Eulerian viewpoint may be advantageous for studies of chemically reacting matter and growing bodies. The Lagrangian and Eulerian viewpoints are unified when continuum theories are modeled on fiber bundles. For the Lagrangian formulation, one simply considers the trivial bundle in which is the manifold representing the ambient physical space. In the Eulerian picture, is interpreted as the space manifold or a region therein.
Modern studies of the mathematical structure of stress theory in continuum mechanics may be traced back to [Nol59] and subsequently [GW67, GM75, Sil85, Sil91, Sil08], for example. The relevance of the notion of stress to field theories led to contributions from the physics community, for example, [KT79, p. 168], which, in some cases, applied ideas originating in the continuum mechanics research (see [Heh76, KT79, HM86, HN91, HMMN95, GH97, p. 168]).
The stress object emerges in field theories as the vertical derivative of the Lagrangian function. Yet, the studies of the stress object and the field equations it should satisfy are relevant in the more general situation where a Lagrangian mapping is not readily available. In the continuum theory of dislocations, for example, it is hard to expect that the motion of dislocations will be governed by a potential.
Thus, this paper considers the stress object and the equations governing it for fields represented as sections of a general fiber bundle. Extending the terminology in [TT60], and in view of the applications described above, we will use the terminology a classical field theory to refer to any such mechanical, or other physical, theory.
In our approach, the analysis of the stress field is put in a broader (global) context. Extending [Seg86], we consider a configuration space of sections which is an infinite dimensional manifold. Generalized forces are viewed as elements of the cotangent bundle of the configuration space and stresses emerge from a representation theorem for the force linear functionals. This “weak” approach allows for generalized, singular, stress fields, with corresponding distributional field equations. We give special attention to the case of smooth stress fields for which we write down the field equation in an explicit differential form. For example, a weak formulation of -form, [HT86, HT88], premetric, [HIO06], electrodynamics was shown in [Seg16] to follow from stress theory for fields represented by -forms in the case where the stress object has a particularly simple form. It should be mentioned that we study here the theory concerning the existence of stresses and the equations it satisfies; we do not study the analytic aspects of the field equations obtained after the constitutive relations are used, in tems of existence and uniqueness of solutions, appropriate function spaces, etc.
Following the introduction in Section 2 of the notation and terminology used pertaining to fiber bundles and their jet bundles, Section 3 is concerned with the infinite dimensional configuration space of sections. Generalized velocities and generalized forces are modeled as elements of the tangent and cotangent bundles of the configuration space, respectively. Particular attention is given to smooth forces, those given in terms of body forces and surface forces. Section 4 considers the analog of “local configurations” as in [TN65, pp. 51–52]. In the present general geometric setting, these are described by sections of the jet bundle. Next, local velocities and their relation to the jets of generalized velocity fields are discussed. Stresses are considered in Section 5. Variational stresses are defined as functionals conjugate to velocity jets. A representation theorem for generalized forces in terms of variational stresses relate the two type of objects through a general version of the principle of virtual power. While, in general, variational stresses are tensor-valued measures, smooth variational stresses, those represented by smooth tensor valued densities induce traction stresses. The traction stress object determines surface forces on oriented -submanifolds via a generalization of Cauchy’s formula. A differential operator generalizing the traditional divergence of the stress tensor is defined next, enabling one to write a generalized version of differential equations of equilibrium and boundary conditions. It is observed, that while in the classical formulation of stress theory, the stress tensor both acts on the rate of change of the deformation gradient to produce power and determines the traction on hypersurfaces, in the geometry of general manifolds, two objects, the variational stress and the traction stresses, are needed for these two roles. While the variational stress determines a unique traction stress, a traction stress field do not determine a unique variational stress. Next, in Section 6, loadings and constitutive relations are introduced leading to a formulation of the problem of stress analysis. Finally, a number of particular cases are presented in Section 7. In particular, the relation between stress theory and premetric -form electrodynamics is summarized.
2. Preliminaries and Notation
The fundamental geometric object considered in this work is that of a fiber bundle, the sections of which are identified with the configurations of a mechanical system or with classical fields. In this section we introduce the notation and terminology adopted throughout this paper.
A fiber bundle [Sau89] will be denoted by a triple , where is the total space, is the base manifold and is the projection. Let be a manifold. We denote by
[TABLE]
its tangent and cotangent bundles. The bundle of -alternating multilinear forms will be denoted by .
Let be a fiber bundle. For a section and a point , we denote by , rather than , the value of at . We also denote the fiber of at by .
Consider . The kernel of in is commonly denoted by , and is referred to as the vertical sub-bundle of . The set is the total space of two bundles: the vector bundle
[TABLE]
and the fiber bundle
[TABLE]
[TABLE]
The vertical bundle of is often denoted in the literature by rather than by . The notation may be ambiguous in instances where is the total space of multiple bundles; the notation makes explicit the projection with respect to which verticality is defined. On the other hand, the latter notation is often cumbersome, for example, when the projection is a composition of several projections, some of which restricted to sub-bundles. For improved readability we adopt the following notation scheme: for a fiber bundle , we denote its vertical bundle by in cases where is the total space of a single bundle, or, in the case of repeated projections, , in which case verticality is implied relative to the projection onto the manifold .
Consider two fiber bundles and over the same base manifold . Let be a fiber bundle morphism, i.e., . The restriction of the tangent map to defines a vertical bundle morphism,
[TABLE]
[TABLE]
Let be a fiber bundle and let be a differentiable mapping. One has the natural pullback bundle, with canonically identified with via the bundle morphism over , as in the diagram below. A section induces the section satisfying ; in other words, is identified with .
[TABLE]
The tangent map of , induces the differential of , satisfying .
[TABLE]
In particular, for two fiber bundles and over the same base manifold , and a fiber bundle morphism , we use
[TABLE]
to denote the vertical derivative of , i.e., the restriction of to ; this vertical derivative is sometimes denoted in the literature by .
Let and be fiber bundles over . Let and let be a fiber bundle morphism. Then, induces a fiber bundle morphism , defined by the equality .
[TABLE]
For a manifold , denotes the space of smooth real-valued functions on . For a fiber bundle , it is common to denote by the set of -sections . As in the case of the vertical bundle, we note that the space of -sections is often denoted in the literature by . Here too, we adopt the following notation scheme: for a fiber bundle , we denote its -sections by in cases where is the total space of a single bundle, or, in the case of repeated projections, , when the section is with respect to projection onto the manifold .
Consider two fiber bundles and and let be a fiber bundle morphism. Then induces a map between sections,
[TABLE]
This mapping is often denoted by , however, we will write explicitly either or just .
[TABLE]
Let be a fiber bundle and let . We say that two (local) sections are -equivalent at if . Equivalently, and are -equivalent if and only if they assume at the same values and the same first derivatives in some (hence, any) coordinate system. The -equivalence class at of a (local) section is denoted by . The first jet bundle of is the set
[TABLE]
In analogy with vertical bundles and sections, we adopt the following notation scheme: for a fiber bundle , we denote its jet bundle by in cases where is the total space of a single bundle, or, in the case of repeated projections, , when the sections are with respect to projection onto the manifold .
The first jet bundle of is associated with the following projections:
[TABLE]
Consider once again two fiber bundles and over the same base manifold . Let be a fiber bundle morphism. The first jet map of is a fiber bundle morphism
[TABLE]
defined by
[TABLE]
where for , is a local section of at .
[TABLE]
Let and be vector bundles over a manifold . We denote by
[TABLE]
the vector bundle over whose elements at are linear maps . Using to designate the set of vector bundle morphisms , it is observed that a vector bundle morphism can be identified with a section of ; thus, a vector bundle morphism may be viewed as a tensor field over . For a section of and a section , we have the section , defined by .
Let be a one-form and let be a mapping. Then, is a section of ; it is not a differential form. In contrast, we denote by the one-form over defined by
[TABLE]
for every .
Throughout this paper we adopt the following terms and notation:
3. Configurations, Velocities and Forces
3.1. The manifold of configurations
In the global approach to mechanics, a system is characterized by its configuration space.
The fundamental object in a classical field theory is a fiber bundle, in which the various fields assume their values. The -dimensional base manifold typically represents space-time in modern physical field theories and a body manifold in continuum mechanics. For , the -dimensional fiber represents the values that the field may assume at . Thus, a field theory is characterized by a particular fiber bundle.
Definition 1**.**
Let be a fiber bundle, where the base manifold is assumed to be compact, oriented and possibly having a boundary. Consider the Banach manifold [Pal68] of sections . The manifold of configurations, , is an open subset of .
Since is open in , it inherits its Banach manifold structure; moreover, for every , .
Comment 2**.**
A basic example of a manifold of configurations is the case where is a trivial bundle. In the Lagrangian approach to continuum mechanics, a body is modeled as a smooth, compact, -dimensional differentiable manifold, . The ambient space is modeled as a smooth -dimensional differentiable manifold without boundary, . The space of configurations is the space of -embeddings , which can be given the structure of a smooth Banach manifold [Pal68, Mic80]. We may also view such maps as sections, , where
[TABLE]
is a trivial bundle over .
A construction of the manifold consistent with the Whitney -topology [Mic80] can be found in Palais [Pal68]. The construction may be roughly described as follows. Let and let be the Banachable space of sections along . That is, satisfies for
[TABLE]
A local chart for in a neighborhood of is a map
[TABLE]
given by
[TABLE]
where is the exponential map on induced by some arbitrarily chosen spray, consistent with the fiber structure. Namely, for ,
[TABLE]
Strictly speaking, is only defined on a neighborhood of the zero section of . However, one can always reparametrize to be defined globally on . The above construction holds only for the case of a compact base manifold . See Remark 7 below for the case of non-compact bases.
Throughout this paper, we complement the covariant, coordinate-free formulation with its corresponding local coordinate representation. We will use a typical local coordinate system
[TABLE]
for the base manifold , and a local coordinate system
[TABLE]
for the fiber bundle . The components of for a given chart will be denoted with Greek indexes, e.g., ; the components of will be denoted with Roman indexes, e.g., . Note the abuse of notation where is both a function on and a function on ; this type of abuse will recur in several instances below.
The coordinate system is assumed to be adapted to the bundle structure: for every , i.e.,
[TABLE]
3.2. Generalized velocities
Definition 3**.**
The bundle tangent to the manifold of configurations is termed the bundle of generalized velocities, or the bundle of virtual displacements.
Following Lang [Lan72, p. 26], we define the tangent space of an infinite-dimensional manifold in the following way. Let and be two configurations, and let
[TABLE]
be coordinate systems at and , respectively, whose images overlap. We will keep the simple notation for the restriction to the overlap. Let
[TABLE]
The triples
[TABLE]
where and , are considered equivalent if
[TABLE]
The collection of all such equivalence classes for a fixed forms the vector space . Given an exponential map on , the canonical representative of an element of is of the form
[TABLE]
that is, the vector space of virtual velocities at can be identified with the space of velocity fields at ,
[TABLE]
A velocity field at , can be identified with a path in a canonical way,
[TABLE]
i.e.,
[TABLE]
The bundle of velocities is the union of the tangent spaces with the standard smooth structure. As a set, consists of sections of viewed as a fiber bundle over . The tangent space at consists of those sections whose projection onto coincides with . In the physics context, an element of is interpreted as a fiber-wise variation of .
[TABLE]
The local coordinate system on induces a smooth local frame for ,
[TABLE]
defined by the paths
[TABLE]
where is the standard basis of . The action of this frame on a function is
[TABLE]
Likewise, the local coordinate system induces a smooth local frame for ,
[TABLE]
defined by the paths
[TABLE]
In terms of derivations, for and ,
[TABLE]
Since the coordinate systems are adapted,
[TABLE]
The vertical bundle is spanned locally by the frame field ; a local coordinate system for is
[TABLE]
where
[TABLE]
A generalized velocity (or virtual displacement) field at has a local representation
[TABLE]
where .
We denote by and , the co-frames dual to , and . We have
[TABLE]
[TABLE]
and
[TABLE]
3.3. Generalized forces
Definition 4**.**
The bundle of forces is the vector bundle
[TABLE]
dual to the vector bundle of velocities. A generalized force at is an element
[TABLE]
That is, for every configuration , the vector space of forces at is the dual of the vector space of velocities at . The action of a force at on a velocity at yields a real number, , termed the virtual power, or virtual work that expends on .
By the isomorphism (3.1),
[TABLE]
Generally, forces may be represented by a collection of measures (see Subsection 5.1) and therefore cannot be assigned values at points. The remaining part of this section considers forces that can be represented by more regular fields.
Definition 5**.**
The bundle of body force densities is
[TABLE]
It is a vector bundle over , with projection which we denote by . For ,
[TABLE]
is the bundle of body force densities along ; it is a vector bundle over .
The bundle of surface force densities is
[TABLE]
It is a vector bundle over , with projection which we denote by . For , and ,
[TABLE]
is the bundle of surface force densities along ; it is a vector bundle over .
With these definitions, we can define the notion of a continuous force:
Definition 6**.**
A force at is termed continuous if there exists a body force density field along ,
[TABLE]
and a surface force density field along ,
[TABLE]
such that for every velocity at , the virtual power that expends on is given by
[TABLE]
Note that on the left-hand side of (3.5), is viewed as an element of , whereas on the right-hand side, is viewed as a velocity field at , i.e., an element of .
Remark 7** (Non-compact base manifolds).**
If the base manifold is not compact, the image of a section is never compact, hence, it is not possible to endow (or any other reasonable class of sections) with a Banach manifold structure (see discussion in the introduction of [PT01]). However, as shown in [Mic80] and [KM97] for smooth sections, the space of -sections can be given a structure of a smooth manifold modeled on a locally convex topological vector space. The tangent space at a configuration may be identified with the space of differentiable sections with compact supports, equipped with the inductive limit topology
[TABLE]
where runs through all compact sets in and has the topology of uniform convergence of all derivatives [KM97, Theorem 42.1]. Thus, generalized velocities are represented by sections of having compact supports so that forces may be viewed as tensor valued currents or generalized sections (see [GS77, Seg16]). An analogous construction can be applied to -sections.
4. Deformation Jets and Velocity Jets
4.1. The manifold of deformation jets
In this section, we consider what is termed in [Seg81] the local model—a notion of configuration that encodes also information about local deformations. In a first grade theory, this additional information is reflected by conceivable values of the first derivative of the configuration at the various points. These values of the derivatives need not be compatible with a particular configuration . For short, we refer to such fields as deformation jets (referred to in [Seg81], for the case of a trivial bundle, as local configurations after [TN65, pp. 51–52]). The natural geometric construct for encoding this information is the first jet bundle .
Definition 8**.**
The manifold of deformation jets which we denote by , is some open subset of —the space of -sections containing the image of . That is
[TABLE]
A deformation jet which is a jet extension of a configuration is termed compatible or holonomic.
The manifold structure of is analogous to the manifold structure of . Denote the vertical bundle of by
[TABLE]
[TABLE]
For , the modeling space for a chart in a neighborhood of is the Banachable space of sections along ; that is, in that neighborhood of is represented by an element satisfying
[TABLE]
[TABLE]
A local coordinate system for [Sau89, p. 96] is
[TABLE]
such that
[TABLE]
4.2. The bundle of velocity jets
The analog of a generalized velocity for the case of the bundle of deformation jets is defined as follows:
Definition 9**.**
The vector bundle tangent to the manifold of deformation jets will be termed the bundle of velocity jets. In [Seg81] it is referred to as the bundle of local virtual displacements (again, in the context of a trivial bundle).
The construction of is analogous to the construction of the bundle of velocities . In particular, for ,
[TABLE]
which is the space of sections along .
As a set, consists of sections of viewed as a fiber bundle over . The tangent space at consists of those sections whose projection onto coincides with . In the physics context, an element of is interpreted as a fiber-wise variation of .
For later use, we will need the following well-known isomorphism:
Proposition 10**.**
* is isomorphic to ,*
[TABLE]
We will denote the isomorphism by
[TABLE]
[TABLE]
Proof.
See [Pal68, Chapter 17] and [Sau89, Theorem 4.4.1]. ∎
Lemma 11**.**
Let be a holonomic deformation jet. Then, the isomorphism induces an isomorphism of vector bundles over ,
[TABLE]
Proof.
See Theorem 17.1 in [Pal68, p. 82]. ∎
A local coordinate system for is
[TABLE]
This local system of coordinates is adapted in the sense that for , where ,
[TABLE]
For
[TABLE]
we have
[TABLE]
Moreover,
[TABLE]
and
[TABLE]
A local coordinate system for is
[TABLE]
For a local section of ,
[TABLE]
[TABLE]
The isomorphism is represented by:
[TABLE]
In other words, The local representative of is given by
[TABLE]
Note that
[TABLE]
We denote by , and the corresponding co-frames:
[TABLE]
4.3. Compatibility and jet prolongation of velocity fields
Evidently, special attention should be given to configuration jets induced as jets of configurations. The analogous situation applies to generalized velocity fields. In this section, we consider compatible configuration jets and compatible velocity jets.
The jet prolongation mapping is an injection, where we omit the indication that needs to be restricted first from to . Its differential is a vector bundle morphism (see diagram below)
[TABLE]
mapping velocities at into velocity jets at ,
[TABLE]
[TABLE]
Since and , the differential of at can also be viewed as a linear map
[TABLE]
mapping velocity fields at into velocity jet fields at .
Proposition 12**.**
The differential of can be factored into the action of and a vector bundle morphism: for ,
[TABLE]
In other words, is represented by
[TABLE]
where the last isomorphism follows from Lemma 11.
Proof.
For , let be a path of configurations satisfying
[TABLE]
By the definition of the differential via its action on curves,
[TABLE]
We now view as a section , i.e., as a map
[TABLE]
Then,
[TABLE]
and
[TABLE]
∎
Since can be identified with , we will use the shorter notation rather than to denote the corresponding element of , and treat
[TABLE]
as a representative of .
Using local coordinate frames, a velocity field at may be represented locally in the form,
[TABLE]
where are differentiable functions defined on the domain of a chart. Its jet prolongation is the velocity jet field at , represented locally as
[TABLE]
5. Stresses
This section introduces the stress object as a tensor valued measure that represents a force functional, non-uniquely. Particular attention is given to stresses measures that are continuous relative to volume measures on the manifold .
5.1. Variational stresses
Definition 13**.**
The bundle dual to the bundle of velocity jets is termed the bundle of variational stresses. Given a deformation jet , an element is referred to as a variational stress at .
For every deformation jet , the vector space is the dual of the vector space of velocity jets at , . By the isomorphism (4.1),
[TABLE]
Let be given. The map
[TABLE]
is an embedding. It follows from the Hahn-Banach theorem that its dual,
[TABLE]
is surjective; to every force at , , there corresponds a (non-unique) variational stress at , , such that
[TABLE]
That is, for every ,
[TABLE]
Equation (5.3) is a generalization of the principle of virtual work in continuum mechanics, and Equation (5.2) is the corresponding generalization of the equilibrium equation.
It should be noted that the (generalized) equilibrium equation is merely a representation theorem; it is not a law of physics. Note also that the well-known static indeterminacy—the non-uniqueness of the stress representing a given force—is reflected by the non-injectivity of , which in turn, follows from the fact that is not surjective.
Let , hence . By the Riesz representation theorem, the space of continuous linear functionals on -sections,
[TABLE]
coincides with the space of Radon measures valued in the dual vector bundle . Locally, a variational stress is represented by a collection of Radon measures
[TABLE]
so that in case or are supported in the domain of a single chart,
[TABLE]
In the general case, is evaluated using a partition of unity.
5.2. Continuous variational stresses
Equation (5.4) shows that variational stresses may be as singular as measures. In this section, we restrict our attention to continuous variational stresses, that is, variational stresses for which the measures are absolutely continuous with respect to some smooth volume form on .
Definition 14**.**
The bundle of stress densities is
[TABLE]
It is a vector bundle over , with projection which we denote by . For ,
[TABLE]
is the -bundle of variational stress densities along ; it is a vector bundle over .
Definition 15**.**
A variational stress at is termed continuous if there exists a variational stress density field at ,
[TABLE]
such that for every velocity jet at , the virtual power that expends on is given by
[TABLE]
Note that on the left-hand side, is viewed as an element of , whereas on the right-hand side, is viewed as an element of . (See below the local expressions for continuous variational stress densities.)
Let be a force at and suppose that is represented by a continuous variational stress at , with variational stress density field . Then, the virtual power expended by is given by
[TABLE]
5.3. Traction stresses
In classical formulations of continuum mechanics in a Euclidean space, the stress object plays two important roles: it determines the traction fields on sub-bodies via the Cauchy formula, and it acts on velocity jets to produce power. For continuous stresses on manifolds, two distinct objects play these two roles.
The variational stress, as defined above and as its name suggests, produces power when it acts on velocity jets. The object that determines the traction fields on the boundaries of sub-bodies will be referred to as traction stress (see [Seg02], where it is referred to as the Cauchy stress, and [Seg13], for the case of a trivial bundle).
Definition 16**.**
The bundle of traction stress densities is
[TABLE]
It is a vector bundle over , with projection which we denote by . For ,
[TABLE]
is the bundle of traction stresses along ; it is a vector bundle over .
Definition 17**.**
A traction stress density field at is a continuous section of the bundle of traction stress densities along ,
[TABLE]
One would like to restrict traction stress density fields to co-dimension submanifolds of . In particular, to the boundary of . Consider therefore, an embedded -dimensional, oriented submanifold . Denote by the inclusion. We denote by the restriction of the fiber bundle to . Formally,
[TABLE]
Let be a vector bundle over (below will represent the vector bundles and ). One can restrict to by pulling back over using the map to obtain the bundle with the corresponding projection
[TABLE]
see the following diagram.
[TABLE]
Equipped with this notation scheme,
[TABLE]
The bundle is the bundle of traction stress densities restricted to , which nonetheless act on any -tuple of vectors in ; it is a vector bundle over .
The inclusion induces a restriction
[TABLE]
of -forms to vectors tangent to . It follows that
[TABLE]
Composition with the latter defines a vector bundle morphism over ,
[TABLE]
The mapping is a generalization of the traditional Cauchy formula for continuum mechanics in Euclidean space, , where is the unit normal to the oriented submanifold. We will therefore refer to it as the Cauchy mapping.
Let . Denote by
[TABLE]
the restriction of to , namely,
[TABLE]
Note that for every vector bundle over ,
[TABLE]
Let be a traction stress field at . Then, is a section of , where
[TABLE]
and we write , rather than , as no ambiguity should arise. Moreover, by (5.6),
[TABLE]
We may therefore apply the pullback of the Cauchy mapping on to obtain a section
[TABLE]
In particular, for the case , a traction stress density field at induces via the Cauchy mapping a surface force density field at , that is, a vector bundle morphism
[TABLE]
In order to simplify the notation, we define the morphism
[TABLE]
by
[TABLE]
so that
[TABLE]
Thus, is the Cauchy mapping along . These formal definitions simply imply that
[TABLE]
5.4. The traction stress induced by a variational stress density
The variational stress determines uniquely the traction stress, but the converse does not hold. This section introduces the construction of the traction stress from the variational stress for the fiber bundle setting.
The vector bundle is a sub-bundle of . Its elements are represented by paths in that are vertical over along the fibers of . The fiber bundle is an affine bundle modeled on the vector bundle [Sau89, Theorem 4.1.11]
[TABLE]
Consequently,
[TABLE]
The inclusion induces a restriction
[TABLE]
defined by
[TABLE]
In view of the isomorphism
[TABLE]
we define
[TABLE]
to be the contraction of the third and first factors in the product, namely,
[TABLE]
Note that is a vector bundle morphism over .
Next, define
[TABLE]
a vector bundle morphism over , by
[TABLE]
For ,
[TABLE]
maps variational stress densities at to traction stress densities at . It follows that composition with maps variational stress density fields along to traction stress fields along .
An element of at is of the form
[TABLE]
Its restriction to , it can be written as
[TABLE]
Then,
[TABLE]
Thus, for a variational stress density at given locally by
[TABLE]
we have
[TABLE]
5.5. The exterior jet of a differentiable traction stress density
Recall the definition of a linear differential operator (see [Pal68, Chapter 3]).
Definition 18**.**
Let and be vector bundles over the same base manifold . A linear map is called a first-order linear differential operator from to if there exists a vector bundle morphism , such that
[TABLE]
Note that is a vector bundle over only if is a vector bundle. We will refer to as the morphism associated with .
For convenience, we recall the definitions of the following vector bundles:
[TABLE]
Each of these bundles can be pulled back with either or ; sections of the pullback bundles are referred to as fields along .
Definition 19**.**
Let . The exterior jet differential operator along
[TABLE]
is defined as follows. Let be a traction stress density field along . Then, for all ,
[TABLE]
Proposition 20**.**
* is a well-defined first-order linear differential operator.*
Proof.
In local coordinates, a traction stress density field along takes the form
[TABLE]
where
[TABLE]
A velocity at is given locally by
[TABLE]
hence,
[TABLE]
Taking the exterior derivative
[TABLE]
By the local expression (4.4) for , it follows that
[TABLE]
satisfies the defining property of and depends linearly on and its derivatives. ∎
5.6. The divergence of differentiable variational stress densities and the equilibrium field equations
In this section we define the divergence differential operator for differentiable variational stress densities. The divergence operator enables one to tranform the weak form of the compatibility condition between continuous forces and stresses to a strong form of the equilibrium differential equation. For the rest of this section, we restrict ourselves to -configurations and -stress density fields.
Proposition 21**.**
Let be a -configuration. There exists a first-order linear differential operator mapping differentiable variational stress density fields along into continuous body force density fields along ,
[TABLE]
satisfying for every variational stress density field and virtual velocity ,
[TABLE]
Proof.
Using coordinates, a variational stress density field has a local representation in the form
[TABLE]
and a velocity has a local representation
[TABLE]
By (4.4),
[TABLE]
On the other hand,
[TABLE]
and
[TABLE]
Subtracting, we obtain that
[TABLE]
That is,
[TABLE]
∎
Consider now a continuous force , given by
[TABLE]
where and . Consider further a continuous stress represented by a variational stress density field . Then, (5.5) takes the form
[TABLE]
We conclude that is represented by a variational stress density field if for every
[TABLE]
It is observed that while the restriction of the various terms in the integrand to and to vectors tangent to is implied in integration theory, formally, in view of (5.7) we write the integrand as . Thus, since equality holds for every , we obtain
[TABLE]
In coordinates, equation (5.11) transforms to an underdetermined set of equations for the components of .
Note that the above proposition holds if the vector bundle is replaced by an arbitrary vector bundle , in which case , which is compatible with [Seg02].
6. The Continuum Mechanics Problem
It is well known that a given force distribution, does not determine a unique stress distribution. The source of this non-uniqueness may be traced back to Section 5.1. A unique stress field is determined when additional information in the form of a constitutive relation is provided. This couples the statics problem described above with the kinematics. The basic notions corresponding to the introduction of constitutive relations are discussed in this section.
Generally, the continuum mechanics problem takes the following form: the system under consideration is subject to external forces, usually dictated by a loading, which is an assignment of a force to every admissible configuration. A loading may consist of a body force component and a surface force component, and it may be singular or continuous. In analogy, a constitutive relation assigns stresses, regular or singular, to deformation jets, in particular, to jets of configurations. The continuum mechanics problem seeks a configuration such that the stress associated through the constitutive relation with represents the force assigned by the loading to .
6.1. Loadings
Definition 22**.**
A loading, , is a one-form on the configuration space assigning a force to every configuration .
Definition 6 of continuous forces extends to a definition of continuous loadings:
Definition 23**.**
A loading is termed continuous if there exists a body loading density
[TABLE]
and a surface loading density
[TABLE]
such that for every and ,
[TABLE]
That is, is continuous with body force density field and surface force density field .
Note that by our conventions, we write rather than , because has multiple bundle structures, and the domain of those sections is not the base manifold, .
A body loading density has local representation,
[TABLE]
where are real valued continuous functions defined locally on .
Assume that the chart is adapted to so that is a chart on and is transversal to . Then, one has a volume element on , and locally,
[TABLE]
where are continuous functions defined locally on . Let
[TABLE]
be a local representation of a velocity at . As
[TABLE]
we have the local expression,
[TABLE]
If the support of may be covered by a single chart, we may write explicitly,
[TABLE]
Definition 24**.**
A loading is termed conservative if
[TABLE]
for some loading potential,
[TABLE]
Definition 25**.**
A conservative loading is continuous if there exists a body loading potential density, which is a -section
[TABLE]
and a boundary loading potential density, which is a -section
[TABLE]
such that the loading potential is given by
[TABLE]
(see diagrams).
[TABLE]
Proposition 26**.**
Consider a continuous conservative loading , the potential function of which is given by a body loading potential density and boundary loading potential . Then, is a continuous loading with corresponding loading densities
[TABLE]
Proof.
First, we should verify that this relation is well-defined type-wise. By the types (6.1) and (6.2) of and , it follows that
[TABLE]
Restricting to the vertical bundle,
[TABLE]
For every vector bundle , section and ,
[TABLE]
In other words, , and so,
[TABLE]
and so, and are indeed loading densities.
It remains to show that and are the loading densities corresponding to . By definition, for ,
[TABLE]
where satisfies and . Substituting the representation of in terms of a density,
[TABLE]
where the derivatives and are taken pointwise in and , respectively.
It follows from the chain rule and the definition of that
[TABLE]
and
[TABLE]
Thus,
[TABLE]
which completes the proof. ∎
In a local coordinate frame, a loading potential density takes the form,
[TABLE]
where and are differentiable functions defined on the domains of the adapted charts on and , respectively. Since the exterior derivatives of the volume elements vanish identically, the loading densities are given locally by
[TABLE]
6.2. Constitutive relations
All the notions analyzed above—configurations, velocities, forces, deformation jets and stresses—pertain to a particular theory depending on the choice of configuration space. Within a particular theory, the properties of a system are prescribed using a constitutive relation, associating the state-of-stress with the kinematics.
It is noted that since our base space may be interpreted naturally as physical space-time, constitutive relations may involve time even in cases where it is not explicitly indicated.
Definition 27**.**
A constitutive relation is a one-form on the manifold of deformation jets, assigning a stress to every deformation jet .
Since is injective, a constitutive relation induces a loading
[TABLE]
By the definition of the pullback of forms, for ,
[TABLE]
where in the first identity we identified, as before, with .
We note that at this level of generality, and interpreting as space-time, this, seemingly elastic constitutive relation, is actually non-local, time dependent, and not necessarily causal.
The definition of continuous stresses extends readily to a definition of -differentiable constitutive relations:
Definition 28**.**
A constitutive relation is termed -differentiable, , if there exists a constitutive density, a differentiable section,
[TABLE]
such that for every deformation jet and for every velocity jet at ,
[TABLE]
In the case of a differentiable constitutive relation, the induced loading is given by
[TABLE]
We note that a differentiable constitutive relation is local and elastic in the sense that the stress at a point depends only on the deformation jet at that point. Again, we mention that for the case where is interpreted as space-time or body-time, contains components that may reflect velocities. However, history dependence is excluded.
In coordinates, a constitutive density is represented locally as
[TABLE]
where are over the domain of a chart in .
6.3. The continuum mechanics equations
Given a constitutive relation and a loading , the continuum mechanics problem seeks a configuration for which the stress determined by the constitutive relation represents the loading for that configuration. Thus, the condition is expressed by
[TABLE]
Explicitly, a configuration is a solution of (6.3) if for every virtual velocity at ,
[TABLE]
6.4. The differential form of the continuum mechanics equations
Consider the continuum mechanics problem in the case of a -constitutive density and a continuous loading with densities and . A configuration which solves the continuum mechanics problem satisfies
[TABLE]
for every velocity field .
In view of the definition of the divergence, restricting ourselves to -configurations and constitutive densities, we can rewrite these equations as follows:
[TABLE]
Since this hold for every virtual velocity , we obtain a boundary-value problem
[TABLE]
Let the loading densities and the constitutive density be given locally by
[TABLE]
and
[TABLE]
Then,
[TABLE]
and
[TABLE]
If follows from the local expressions derived in Sections 5.4 and 5.6 that
[TABLE]
and
[TABLE]
so that the field equation is
[TABLE]
Since
[TABLE]
the boundary conditions are
[TABLE]
6.5. Conservative constitutive relations
Definition 29**.**
A constitutive relation is referred to as conservative if there exists an energy function
[TABLE]
such that the constitutive relation is given by
[TABLE]
Consider a conservative system with energy function , subject to a conservative loading . Then, the equilibrium equations are
[TABLE]
where we used the commutativity of external derivatives and pullbacks. Thus, the solution is a critical point of the total energy,
[TABLE]
Definition 30**.**
A conservative constitutive relation is said to be differentiable if there exists a Lagrangian density form, a -section
[TABLE]
such that the energy function is of the form
[TABLE]
[TABLE]
Evidently, differentiable conservative constitutive relations generalize hyperelastic constitutive relations to the setting considered in this paper.
Proposition 31**.**
Consider a differentiable constitutive relation with a Lagrangian density . The resulting constitutive relation is with a constitutive density
[TABLE]
Equation (6.7) is a generalization of the classical relation between the stress and the derivative of the elastic energy density.
Proof.
By definition, for ,
[TABLE]
where satisfies and . Substituting the representation of in terms of a density,
[TABLE]
where the derivative is taken pointwise at every . It follows from the chain rule and the definitions of and that
[TABLE]
i.e.,
[TABLE]
which completes the proof. ∎
Using a coordinate frame, a Lagrangian density is of the form
[TABLE]
where . Then,
[TABLE]
It follows that
[TABLE]
7. Some Special Cases
We present here a number of examples where the general settings assume particularly useful forms.
7.1. Vector bundles
Consider the case where is a vector bundle. By the natural isomorphism for any vector space , it follows that
[TABLE]
It follows that for ,
[TABLE]
i.e.,
[TABLE]
independently of . As such, this theory may be referred to as linear.
Next, since is a vector bundle, so is . Thus, in analogy, for any section ,
[TABLE]
7.2. Affine bundles
Consider the case where is an affine bundle modeled on the vector bundle (see [Sau89, p. 48]). It is implied that for every ,
[TABLE]
Hence,
[TABLE]
independently of . Likewise, by Lemma 11 ,
[TABLE]
independently of .
7.3. The bundle of frames
As mentioned in the introduction, the bundle of frames plays an important role in the geometric theory of continuous distribution of dislocations. Consider the bundle of frames whose fiber at is ), the space of invertible mappings viewed as bases (frames) in . Since is an open subset of the vector space of linear mappings , is a sub-bundle of the vector bundle . We may conclude that for any ,
[TABLE]
and for any frame field ,
[TABLE]
Again, we may further conclude that
[TABLE]
7.4. Form-conjugate forces and stresses
Consider the case where , where . This is a special case of 7.1 above. It follows that for any , and . Differentiable variational stress densities fields along are, therefore, sections of and continuous traction stress density fields are sections of .
A particularly simple case follows when the traction stress density field is given in terms of a -differential form by
[TABLE]
for any -differential form on . It follows that
[TABLE]
Set,
[TABLE]
It follows that,
[TABLE]
The representation of the force
[TABLE]
may be written now as
[TABLE]
Assume that , and consider the special case where . If we interpret as the -form potential (vector potential) of electrodynamics, the expression we obtained for the power, together with equations (7.10, 7.11) are the governing equations of electrodynamics. Here, is interpreted as the -current density, is interpreted as the Faraday -form, and is interpreted as the Maxwell -form. As no metric structure is used, the equations are in the framework of pre-metric electrodynamics (see [HIO06]). In case the Lorentz metric is used, one can apply the Hodge star operator and write and obtain the usual Maxwell equations in vacuum, as for example in [MTW73, Chapter 3].
In the general case, one obtains a generalization of electrodynamics, referred to as -form electrodynamics, as in [HT86, HT88]. (For further details see [Seg16].) A different theory in which form-conjugate forces appear is the theory of dislocations. In the case of dislocations, however, the traction stress does not have a simple form as assumed above. In fact, implies that no dislocations are present (see [ES14, ES15]).
7.5. Trivial fiber bundles
Consider the case where the fiber bundle is trivial, that is
[TABLE]
for some -dimensional manifold . A section representing a configuration in this case is the graph of a mapping Thus, it is natural in the case of trivial bundles to identify the configuration with such a mapping
[TABLE]
It follows that the configuration space is an open subset of the manifold of mappings .
Since , may be identified naturally with . It follows that a generalized velocity at may be represented by a mapping
[TABLE]
or alternatively, with a section of the vector bundle
[TABLE]
The jet bundle can now be replaced by the jet space of mapping, (see [Mic80, Chapter 1]). An element of is determined by the tangent mapping for some mapping ; may be identified with the space of continuous vector bundle morphisms over -mappings .
For further details regarding the forms assumed by continuous forces and stresses, see [Seg13].
7.6. Continuum mechanics on manifolds
The previous example includes the case of continuum mechanics on manifolds. Here, the manifold is interpreted as the physical space . For continuum mechanics, it is customary to require that configurations satisfy the principle of material impenetrability which implies that be the space of all embeddings . Indeed, the subset of embeddings is open in the manifold of mappings (see [Hir76, Mic80]).
In the classical case, both and are 3-dimensional and is a Euclidean space.
7.7. Continua with microstructure
Continuum mechanics of materials with microstructure falls under the case where has the structure of a Cartesian product , however, the manifold has the additional structure of a fiber bundle
[TABLE]
The fiber over the point is interpreted as possible micro-states that a material point located at may assume. Terms such as “internal variables”, “internal degrees of freedom”, “order parameters”, etc. are also used for the micro-states.
A configuration of a body with microstructure is a mapping
[TABLE]
for which
[TABLE]
is an embedding.
For bodies with microstructre, forces and stresses include components that are conjugate to the micro-velocities and their jets (see [Seg94]).
A number of examples of continua with microstructure are discussed in [Mer79, Cap89]. These include mixtures, liquid crystals, Superfluid helium-3, Cosserat continua, etc.
7.8. Group action
We consider the case where for some Lie group there is a smooth left action
[TABLE]
such that for all ,
[TABLE]
is a fiber bundle morphism over the identity of . Thus, for , the image of is contained in .
The tangent mapping
[TABLE]
may be decomposed into partial tangents, and in particular
[TABLE]
may be restricted to the Lie algebra, , and we obtain
[TABLE]
It is observed that the image of is a subset of the vertical sub-bundle. It follows that for any , , there is a generalized velocity
[TABLE]
It would be natural, therefore, to define an equilibrated force as an element such that
[TABLE]
(see also [Seg94]). Requiring that all forces on all subbodies be equilibrated restricts the class of stresses. For example, in the classical formulation of continuum mechanics in a Euclidean space, invariance under the Euclidean group implies that the components of the variational stress vanish and the components satisfy the usual symmetry conditions for the first Piola-Kirchhoff stress.
Acknowledgement: RK was partially supported by the Israel Science Foundation (Grant No. 661/13), and by a grant from the Ministry of Science, Technology and Space, Israel and the Russian Foundation for Basic Research, the Russian Federation. RS was partially supported by the H. Greenhill Chair for Theoretical and Applied Mechanics and by the Pearlstone Center for Aeronautical Engineering Studies at Ben-Gurion University.
The reference list from the paper itself. Each links out to its DOI / PubMed record.
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