Vector and tensor calculus
In this chapter, attention is given to the definition and manipulation of vector and tensor fields. This mathematical description is used in many physical disciplines, and mechanics in particular. Vectors and tensors enable a compact notation and manipulation, without the necessity to resort to individual components with respect to a particular basis. The latter is needed only at the point that quantitative calculations need to be done, which is generally postponed to the last step. Special attention is given to Cartesian tensor calculus, which provides the basis for the elaboration of coordinate-free equations. Within this specific framework, no distinction is made between contravariant and covariant tensors while the metric tensor is not introduced neither. The quantification into components
measured with respect to a specific basis, and the related matrix calculus is also elaborated.
A.1 Scalars ¶ A scalar a a a is a quantity which has only a measure but no direction. It is the most
trivial tensor, the tensor of order zero. The value of a scalar does not depend on the
choice of a basis. Well-known examples are the temperature T T T or the density ρ \rho ρ in a
material point.
A.2 Vectors ¶ A.2.1 Definition ¶ A vector is a physical quantity possessing both a magnitude (or length)
and a direction.
Figure A.1: Magnitude and direction of a vector a ⃗ \V{a} a .
In case of a vector a ⃗ \V{a} a :
a ⃗ = ∥ a ⃗ ∥ e ⃗ \V{a} \;=\; \| \V{a} \| \V{e} a = ∥ a ∥ e the length is given by ∥ a ⃗ ∥ \|\V{a}\| ∥ a ∥ , and the direction is given by a unit
vector e ⃗ \V{e} e , having a unit length. A vector is a first-order tensor. The zero vector 0 ⃗ \V{0} 0 is a special vector having zero length. The
so-called index notation of a vector a ⃗ \V{a} a is given by
a ⃗ ⟹ a i \V{a} \;\Longrightarrow\; a_i a ⟹ a i A vector is thus indicated with a single index (i.c. i i i ), the value of which ranges
between 1 and the dimension of the Euclidian space it is used in (commonly this
dimension equals 3). The order of this tensor (i.e. 1) thus equals its number of
indices. The index notation obtains a specific meaning once a basis has been chosen, since
the components of a vector are trivially identified with this notation,
see Section A.2.3 .
A.2.2 Vector operations ¶ Multiplication of a vector a ⃗ = ∥ a ⃗ ∥ e ⃗ \V{a} = \|\V{a}\| \V{e} a = ∥ a ∥ e by a scalar
α \alpha α yields a vector b ⃗ \V{b} b with length α ∥ a ⃗ ∥ \alpha \|\V{a}\| α ∥ a ∥ in the direction e ⃗ \V{e} e :
b ⃗ = α a ⃗ \V{b} \;=\; \alpha \V{a} b = α a Figure A.2: Multiplication of a vector: b ⃗ = α a ⃗ \V{b} = \alpha\V{a} b = α a .
The sum of two vectors a ⃗ \V{a} a and b ⃗ \V{b} b is a new vector c ⃗ \V{c} c , equal to the diagonal
of the parallelogram spanned by a ⃗ \V{a} a and b ⃗ \V{b} b .
c ⃗ = a ⃗ + b ⃗ \V{c} \;=\; \V{a} + \V{b} c = a + b Figure A.3: The sum of two vectors: c ⃗ = a ⃗ + b ⃗ \V{c}=\V{a}+\V{b} c = a + b .
scalar product , inner product or dot product [1] of
two vectors is a scalar quantity, defined as:
a ⃗ ⋅ b ⃗ = ∥ a ⃗ ∥ ∥ b ⃗ ∥ cos ( ϕ ) \V{a} \inp \V{b} \;=\; \| \V{a} \|\; \| \V{b} \| \cos(\phi) a ⋅ b = ∥ a ∥ ∥ b ∥ cos ( ϕ ) where ϕ \phi ϕ is the smallest angle between a ⃗ \V{a} a and b ⃗ \V{b} b .
Note that the dot product of two nonzero mutually perpendicular vectors
equals zero.
Figure A.4: The inner product of two vectors: a ⃗ ⋅ b ⃗ \V{a}\inp\V{b} a ⋅ b .
The product is commutative, i.e.:
a ⃗ ⋅ b ⃗ = b ⃗ ⋅ a ⃗ \V{a} \inp \V{b} \;=\; \V{b} \inp \V{a} a ⋅ b = b ⋅ a and linear
a ⃗ ⋅ ( b ⃗ + c ⃗ ) = a ⃗ ⋅ b ⃗ + a ⃗ ⋅ c ⃗ \V{a} \inp (\V{b} + \V{c}) \;=\; \V{a}\inp\V{b} + \V{a}\inp\V{c} a ⋅ ( b + c ) = a ⋅ b + a ⋅ c Using index notations, Einstein’s summation convention has to be
introduced. This convention states, that a summation is made over
all repeated indices, where the range of the summation equals the
dimension n n n of the problem. For the inner product, this is written
as
a ⃗ ⋅ b ⃗ = a i b i = ∑ i = 1 3 a i b i \V{a}\cdot\V{b} \;=\; a_ib_i \;=\; \sum_{i=1}^3 a_i b_i a ⋅ b = a i b i = i = 1 ∑ 3 a i b i The summation symbol is generally not written, but here simply added to clarify the
convention.
The scalar product of a vector with itself yields the square of its length:
a ⃗ ⋅ a ⃗ = ∥ a ⃗ ∥ 2 ≥ 0 \V{a} \inp \V{a} \;=\; \| \V{a} \|^2 \geq 0 a ⋅ a = ∥ a ∥ 2 ≥ 0 The vector product or cross product of two vectors is a
vector quantity:
a ⃗ × b ⃗ = c ⃗ \V{a} \cross \V{b} \;=\; \V{c} a × b = c The length of the vector c ⃗ \V{c} c is given by:
∥ c ⃗ ∥ = ∥ a ⃗ ∥ ∥ b ⃗ ∥ sin ( ϕ ) \| \V{c} \| \;=\; \| \V{a} \|\; \| \V{b} \| \sin(\phi) ∥ c ∥ = ∥ a ∥ ∥ b ∥ sin ( ϕ ) where ϕ \phi ϕ is the smallest angle between a ⃗ \V{a} a and b ⃗ \V{b} b . Its value equals the area
of the parallelogram spanned by the vectors a ⃗ \V{a} a and b ⃗ \V{b} b . The direction of c ⃗ \V{c} c
is perpendicular to both a ⃗ \V{a} a and b ⃗ \V{b} b , such that the vectors a ⃗ \V{a} a , b ⃗ \V{b} b and
c ⃗ \V{c} c form a righthanded system.
Figure A.5: The cross product of two vectors: c ⃗ = a ⃗ × b ⃗ \V{c}=\V{a}\cross\V{b} c = a × b .
The linearity of the vector product is expressed through
a ⃗ × ( b ⃗ + c ⃗ ) = a ⃗ × b ⃗ + a ⃗ × c ⃗ \V{a} \cross (\V{b} + \V{c}) \;=\; \V{a} \cross \V{b} + \V{a} \cross \V{c} a × ( b + c ) = a × b + a × c The vector product is not commutative:
b ⃗ × a ⃗ = − a ⃗ × b ⃗ \V{b} \cross \V{a} \;=\; - \V{a} \cross \V{b} b × a = − a × b which can be concluded from the definition. It can be shown that:
a ⃗ × ( b ⃗ × c ⃗ ) = ( a ⃗ ⋅ c ⃗ ) b ⃗ − ( a ⃗ ⋅ b ⃗ ) c ⃗ \V{a} \cross (\V{b} \cross \V{c}) \;=\;
(\V{a} \inp \V{c}) \V{b} - (\V{a} \inp \V{b}) \V{c} a × ( b × c ) = ( a ⋅ c ) b − ( a ⋅ b ) c The triple product [2] of three vectors is a scalar quantity, defined as:
a ⃗ × b ⃗ ⋅ c ⃗ = ∥ a ⃗ ∥ ∥ b ⃗ ∥ sin ( ϕ ) ( n ⃗ ⋅ c ⃗ ) = ∥ a ⃗ ∥ ∥ b ⃗ ∥ sin ( ϕ ) ∥ c ⃗ ∥ cos ( ψ ) \begin{aligned}
\V{a} \cross \V{b} \inp \V{c} \;&\;=
\| \V{a} \|\; \| \V{b} \| \sin(\phi) (\V{n} \inp \V{c}) \\
\;&=\; \| \V{a} \|\; \| \V{b} \| \sin(\phi) \| \V{c} \| \cos(\psi)
\end{aligned} a × b ⋅ c = ∥ a ∥ ∥ b ∥ sin ( ϕ ) ( n ⋅ c ) = ∥ a ∥ ∥ b ∥ sin ( ϕ ) ∥ c ∥ cos ( ψ ) where n ⃗ \V{n} n is the unit vector in the direction a ⃗ × b ⃗ \V{a} \cross \V{b} a × b , ϕ \phi ϕ is the
smallest angle between a ⃗ \V{a} a and b ⃗ \V{b} b and ψ \psi ψ is the smallest angle between
c ⃗ \V{c} c and n ⃗ \V{n} n .
Figure A.6: The triple product of three vectors a ⃗ × b ⃗ ⋅ c ⃗ \V{a}\cross\V{b}\inp\V{c} a × b ⋅ c .
The absolute value of the triple product equals the volume of the parallelepiped spanned
by the three vectors. If a ⃗ × b ⃗ ⋅ c ⃗ ≠ 0 \V{a} \cross \V{b} \inp \V{c} \neq 0 a × b ⋅ c = 0 , the vectors are not lying
within one plane, and are called mutually independent .
The tensor product [3] or open
product of two vectors
a ⃗ b ⃗ \V{a}\V{b} a b is a linear vector transformation called a dyad .
Application of the dyad a ⃗ b ⃗ \V{a}\V{b} a b to a vector p ⃗ \V{p} p yields a
vector a ⃗ \V{a} a , multiplied by the scalar ( b ⃗ ⋅ p ⃗ ) (\V{b} \inp \V{p}) ( b ⋅ p ) :
a ⃗ b ⃗ ⋅ p ⃗ = a ⃗ ( b ⃗ ⋅ p ⃗ ) \V{a}\V{b} \inp \V{p} \;=\; \V{a} (\V{b} \inp \V{p}) a b ⋅ p = a ( b ⋅ p ) or in index notation
( a i b j ) p j = a i ( b j p j ) (a_ib_j) p_j \;=\; a_i (b_jp_j) ( a i b j ) p j = a i ( b j p j ) Figure A.7: The tensor product: a ⃗ b ⃗ ⋅ p ⃗ \V{a} \V{b} \inp \V{p} a b ⋅ p .
The linearity of the transformation is expressed by:
a ⃗ b ⃗ ⋅ ( α p ⃗ + β q ⃗ ) = α a ⃗ ( b ⃗ ⋅ p ⃗ ) + β a ⃗ ( b ⃗ ⋅ q ⃗ ) \V{a}\V{b} \inp ( \alpha \V{p} + \beta \V{q} ) \;=\;
\alpha \V{a} (\V{b} \inp \V{p}) + \beta \V{a} (\V{b} \inp \V{q}) a b ⋅ ( α p + β q ) = α a ( b ⋅ p ) + β a ( b ⋅ q ) The transpose of a dyad (also called conjugate dyad or adjoint
dyad )[4] is defined as:
( a ⃗ b ⃗ ) T = b ⃗ a ⃗ ≠ a ⃗ b ⃗ ( \V{a}\V{b} )^T \;=\; \V{b}\V{a} \neq \V{a}\V{b} ( a b ) T = b a = a b If ( a ⃗ b ⃗ ) T = a ⃗ b ⃗ ( \V{a}\V{b} )^T = \V{a}\V{b} ( a b ) T = a b , the dyad a ⃗ b ⃗ \V{a}\V{b} a b is called
symmetric.
A.2.3 Vector basis ¶ In three-dimensional space, a set of three vectors c ⃗ 1 \V{c}_1 c 1 , c ⃗ 2 \V{c}_2 c 2 and c ⃗ 3 \V{c}_3 c 3 is
called a basis , denoted by { c ⃗ 1 , c ⃗ 2 , c ⃗ 3 } \{ \V{c}_1, \V{c}_2, \V{c}_3 \} { c 1 , c 2 , c 3 } , if the
vectors are independent, i.e. if the triple product of the vectors is nonzero:
{ c ⃗ 1 , c ⃗ 2 , c ⃗ 3 } ⇒ c ⃗ 1 × c ⃗ 2 ⋅ c ⃗ 3 ≠ 0 \{ \V{c}_1, \V{c}_2, \V{c}_3 \} \quad \Rightarrow \quad
\V{c}_1 \cross \V{c}_2 \inp \V{c}_3 \neq 0 { c 1 , c 2 , c 3 } ⇒ c 1 × c 2 ⋅ c 3 = 0 The three vectors c ⃗ 1 \V{c}_1 c 1 , c ⃗ 2 \V{c}_2 c 2 and c ⃗ 3 \V{c}_3 c 3 are called base vectors .
If the basis consists of mutually perpendicular vectors, the basis is
called an orthogonal basis .
If the basis consists of mutually perpendicular unit vectors, the basis is called an
orthonormal basis . In the latter case the base vectors are
usually denoted by e ⃗ 1 \V{e}_1 e 1 , e ⃗ 2 \V{e}_2 e 2 and e ⃗ 3 \V{e}_3 e 3 . Thus it holds that:
{ e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } ⇒ e ⃗ i ⋅ e ⃗ j = δ i j = { 0 if i ≠ j 1 if i = j \basis \quad \Rightarrow \quad \V{e}_i \inp \V{e}_j \;=\; \delta_{ij}
\;=\; \left\{ \begin{array}{lcl}
0 & \mbox{if} & \mbox{$i \neq j$} \\
1 & \mbox{if} & \mbox{$i = j$}
\end{array}
\right. { e 1 , e 2 , e 3 } ⇒ e i ⋅ e j = δ ij = { 0 1 if if i = j i = j where δ i j \delta_{ij} δ ij is called the Kronecker delta . A basis { e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 } is called righthanded [5] if the order of
e ⃗ 1 \V{e}_1 e 1 , e ⃗ 2 \V{e}_2 e 2 and e ⃗ 3 \V{e}_3 e 3 is such that:
e ⃗ 1 × e ⃗ 2 = e ⃗ 3 e ⃗ 2 × e ⃗ 3 = e ⃗ 1 e ⃗ 3 × e ⃗ 1 = e ⃗ 2 \begin{aligned}
\V{e}_1 \cross \V{e}_2 \;&=\; \V{e}_3 \\
\V{e}_2 \cross \V{e}_3 \;&=\; \V{e}_1 \\
\V{e}_3 \cross \V{e}_1 \;&=\; \V{e}_2
\end{aligned} e 1 × e 2 e 2 × e 3 e 3 × e 1 = e 3 = e 1 = e 2 A Cartesian basis is an orthonormal basis in which the base vectors
are independent of the location in three-dimensional space. It is
usually denoted by { e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 } or { e ⃗ x , e ⃗ y , e ⃗ z } \xyzbasis { e x , e y , e z } .
Figure A.8: A Cartesian orthonormal basis { e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 } .
A cylindrical basis is an orthonormal basis as well. It is usually
denoted by { e ⃗ r , e ⃗ t , e ⃗ z } \cylbasis { e r , e t , e z } . The bases { e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 } and { e ⃗ r , e ⃗ t , e ⃗ z } \cylbasis { e r , e t , e z } are mutually related by:
e ⃗ r ( θ ) = cos ( θ ) e ⃗ 1 + sin ( θ ) e ⃗ 2 e ⃗ t ( θ ) = − sin ( θ ) e ⃗ 1 + c o s ( θ ) e ⃗ 2 e ⃗ z = e ⃗ 3 \begin{aligned}
\V{e}_r(\theta) \;&=\; \cos(\theta) \V{e}_1 + \sin(\theta) \V{e}_2 \\
\V{e}_t(\theta) \;&=\; - \sin(\theta) \V{e}_1 + cos(\theta) \V{e}_2 \\
\V{e}_z \;&=\; \V{e}_3
\end{aligned} e r ( θ ) e t ( θ ) e z = cos ( θ ) e 1 + sin ( θ ) e 2 = − sin ( θ ) e 1 + cos ( θ ) e 2 = e 3 Figure A.9: A cylindrical orthonormal basis { e ⃗ r , e ⃗ t , e ⃗ z } \cylbasis { e r , e t , e z } .
It is important to note that the base vectors
e ⃗ r \V{e}_r e r and e ⃗ t \V{e}_t e t depend on the circumferential coordinate
θ \theta θ . The derivatives of the vectors with respect to θ \theta θ are given by:
d e ⃗ r ( θ ) d θ = e ⃗ t ( θ ) d e ⃗ t ( θ ) d θ = − e ⃗ r ( θ ) \begin{aligned}
\frac{d\V{e}_r(\theta)}{d\theta} \;&=\; \V{e}_t(\theta)\\
\frac{d\V{e}_t(\theta)}{d\theta} \;&=\; - \V{e}_r(\theta)
\end{aligned} d θ d e r ( θ ) d θ d e t ( θ ) = e t ( θ ) = − e r ( θ ) A.2.4 Vector components; matrix notation of a vector ¶ Let { c ⃗ 1 , c ⃗ 2 , c ⃗ 3 } \{ \V{c}_1, \V{c}_2, \V{c}_3 \} { c 1 , c 2 , c 3 } be a basis in three-dimensional
space. Then any vector a ⃗ \V{a} a can be expressed as a unique linear
combination of the base vectors. In case of an orthonormal basis { e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 }
we may write:
a ⃗ = a 1 e ⃗ 1 + a 2 e ⃗ 2 + a 3 e ⃗ 3 = a i e ⃗ i , \V{a} \;=\; a_1 \V{e}_1 + a_2 \V{e}_2 + a_3 \V{e}_3 = a_i\V{e}_i, a = a 1 e 1 + a 2 e 2 + a 3 e 3 = a i e i , where we again used the Einstein summation convention , i.e. we sum over
the repeated index i i i .
Figure A.10: Components a i a_i a i of a vector a ⃗ \V{a} a with respect to a Cartesian
basis { e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 } .
The coefficients a i a_i a i are called the
components of the vector a ⃗ \V{a} a with respect to the basis.
Note that, since the basis is orthonormal, a component a i a_i a i of a vector
a ⃗ \V{a} a with respect to the base
vector e ⃗ i \V{e}_i e i can be found by:
a i = a ⃗ ⋅ e ⃗ i a_i \;=\; \V{a}\inp\V{e}_i a i = a ⋅ e i The component a i a_i a i represents the length of the projection of the
vector a ⃗ \V{a} a on the line with direction e ⃗ i \V{e}_i e i .
For convenience we can use a matrix notation in which we
store base vectors and components in a column :
a ∼ = [ a 1 a 2 a 3 ] e ⃗ ∼ = [ e ⃗ 1 e ⃗ 2 e ⃗ 3 ] \begin{aligned}
\C{a} \;&=\; \begin{bmatrix} a_1 \\ a_2 \\ a_3 \end{bmatrix} \\
\C{\V{e}} \;&=\; \begin{bmatrix} \V{e}_1 \\ \V{e}_2 \\ \V{e}_3 \end{bmatrix}
\end{aligned} ∼ a ∼ e = ⎣ ⎡ a 1 a 2 a 3 ⎦ ⎤ = ⎣ ⎡ e 1 e 2 e 3 ⎦ ⎤ Thus we may write:
a ⃗ = [ a 1 a 2 a 3 ] [ e ⃗ 1 e ⃗ 2 e ⃗ 3 ] = a ∼ T e ⃗ ∼ \V{a} \;=\; \begin{bmatrix} a_1 & a_2 & a_3 \end{bmatrix}
\begin{bmatrix} \V{e}_1 \\ \V{e}_2 \\ \V{e}_3 \end{bmatrix} \;=\;
\C{a}^T \C{\V{e}} a = [ a 1 a 2 a 3 ] ⎣ ⎡ e 1 e 2 e 3 ⎦ ⎤ = ∼ a T ∼ e or, equivalently:
a ⃗ = [ e ⃗ 1 e ⃗ 2 e ⃗ 3 ] [ a 1 a 2 a 3 ] = e ⃗ ∼ T a ∼ \V{a} \;=\; \begin{bmatrix} \V{e}_1 & \V{e}_2 & \V{e}_3 \end{bmatrix}
\begin{bmatrix} a_1 \\ a_2 \\ a_3 \end{bmatrix} =
\C{\V{e}}^T \C{a} a = [ e 1 e 2 e 3 ] ⎣ ⎡ a 1 a 2 a 3 ⎦ ⎤ = ∼ e T ∼ a The relations a i = a ⃗ ⋅ e ⃗ i a_i = \V{a}\inp\V{e}_i a i = a ⋅ e i can now be written as:
a ∼ = a ⃗ ⋅ e ⃗ ∼ \C{a} \;=\; \V{a}\inp\C{\V{e}} ∼ a = a ⋅ ∼ e A.3 Second order tensors ¶ A.3.1 Definition ¶ A second order tensor is a linear transformation of a vector
into another vector:
A ⋅ p ⃗ = q ⃗ \T{A} \inp \V{p} \;=\; \V{q} A ⋅ p = q or in index notation
A i j p j = q i A_{ij}p_j \;=\; q_i A ij p j = q i Note that we limit ourselves here to so-called Cartesian tensors, which allow orthogonal
linear coordinate transformations only. In a three-dimensional space, a second-order
tensor is fully defined by the image of three independent vectors, see
Figure A.11 .
Figure A.11: A second-order tensor A \T{A} A in a three-dimensional space.
Indeed, any set of three independent vectors constitutes a vector basis by means of which
any other vector can be expressed. The image of an arbitrary vector can be found
trivially through the images of three such vectors. This property is a direct consequence
of the linearity of the transformation, which is expressed by:
A ⋅ ( α m ⃗ + β n ⃗ ) = α A ⋅ m ⃗ + β A ⋅ n ⃗ \T{A} \inp ( \alpha \V{m} + \beta \V{n} ) \;=\;
\alpha \T{A} \inp \V{m} + \beta \T{A} \inp \V{n} A ⋅ ( α m + β n ) = α A ⋅ m + β A ⋅ n For an arbitrary vector a ⃗ = a 1 e ⃗ 1 + a 2 e ⃗ 2 + a 3 e ⃗ 3 \V{a}=a_1\V{e}_1 + a_2\V{e}_2 + a_3\V{e}_3 a = a 1 e 1 + a 2 e 2 + a 3 e 3 the image vector thus
equals
A ⋅ a ⃗ = a 1 ( A ⋅ e ⃗ 1 ) + a 2 ( A ⋅ e ⃗ 2 ) + a 3 ( A ⋅ e ⃗ 3 ) \T{A}\inp\V{a} \;=\; a_1(\T{A}\inp\V{e}_1) + a_2(\T{A}\inp\V{e}_2) + a_3(\T{A}\inp\V{e}_3) A ⋅ a = a 1 ( A ⋅ e 1 ) + a 2 ( A ⋅ e 2 ) + a 3 ( A ⋅ e 3 ) A.3.2 Some properties ¶ Any second order tensor may be represented by a finite, nonunique, sum of dyads:
A = α 1 a ⃗ 1 b ⃗ 1 + α 2 a ⃗ 2 b ⃗ 2 + α 3 a ⃗ 3 b ⃗ 3 + … \T{A} \;=\;
\alpha_1 \V{a}_1 \V{b}_1 + \alpha_2 \V{a}_2 \V{b}_2 +
\alpha_3 \V{a}_3 \V{b}_3 + \dots A = α 1 a 1 b 1 + α 2 a 2 b 2 + α 3 a 3 b 3 + … Two special tensors are the zero tensor O \T{O} O and the
unit tensor [6] I \T{I} I . If applied to vector
p ⃗ \V{p} p , these tensors yield the following:
O ⋅ p ⃗ = 0 ⃗ \T{O} \inp \V{p} \;=\; \V{0} O ⋅ p = 0 I ⋅ p ⃗ = p ⃗ \T{I} \inp \V{p} \;=\; \V{p} I ⋅ p = p The index notations for O \T{O} O and I \T{I} I are respectively
0 ⇔ 0 i j I ⇔ δ i j \begin{aligned}
\T{0} \;&\Leftrightarrow\; 0_{ij}\\
\T{I} \;&\Leftrightarrow\; \delta_{ij}
\end{aligned} 0 I ⇔ 0 ij ⇔ δ ij where the Kronecker delta δ i j \delta_{ij} δ ij is used for the unit tensor.
The transpose or conjugate A T \T{A}^T A T of a tensor A \T{A} A is defined by the
following relation:
A T ⋅ p ⃗ = p ⃗ ⋅ A \T{A}^T \inp \V{p} \;=\; \V{p} \inp \T{A} A T ⋅ p = p ⋅ A In index notation it holds that
A ⇔ A i j ⟹ A T ⇔ A j i \T{A}\;\Leftrightarrow\;A_{ij} \quad\Longrightarrow\quad \T{A}^T\;\Leftrightarrow\;A_{ji} A ⇔ A ij ⟹ A T ⇔ A ji For the special case A = a ⃗ b ⃗ \T{A} = \V{a}\V{b} A = a b , we find:
( a ⃗ b ⃗ ) T ⋅ p ⃗ = p ⃗ ⋅ ( a ⃗ b ⃗ ) = ( p ⃗ ⋅ a ⃗ ) b ⃗ = b ⃗ ( p ⃗ ⋅ a ⃗ ) = b ⃗ ( a ⃗ ⋅ p ⃗ ) = ( b ⃗ a ⃗ ) ⋅ p ⃗ \begin{aligned}
(\V{a}\V{b})^T \inp \V{p} \;&=\; \V{p} \inp (\V{a}\V{b}) \\
\;&=\; (\V{p} \inp \V{a}) \V{b} \\
\;&=\; \V{b} (\V{p} \inp \V{a}) \\
\;&=\; \V{b} (\V{a} \inp \V{p}) \\
\;&=\; (\V{b} \V{a}) \inp \V{p}
\end{aligned} ( a b ) T ⋅ p = p ⋅ ( a b ) = ( p ⋅ a ) b = b ( p ⋅ a ) = b ( a ⋅ p ) = ( b a ) ⋅ p showing that:
( a ⃗ b ⃗ ) T = b ⃗ a ⃗ (\V{a}\V{b})^T \;=\; \V{b} \V{a} ( a b ) T = b a If A \T{A} A is written as a sum of dyads, the conjugate A T \T{A}^T A T is
obtained by reversing the two vectors in each dyad.
Tensors can be multiplied by a scalar, summed with another tensor, or
multiplied by another tensor:
( α A ) ⋅ v ⃗ = A ⋅ ( α v ⃗ ) , ( A + B ) ⋅ v ⃗ = A ⋅ v ⃗ + B ⋅ v ⃗ , ( A ⋅ B ) ⋅ v ⃗ = A ⋅ ( B ⋅ v ⃗ ) \begin{aligned}
(\alpha \T{A}) \inp \V{v} \;&=\; \T{A} \inp (\alpha \V{v}) ,\\
(\T{A} + \T{B}) \inp \V{v} \;&=\; \T{A} \inp \V{v} + \T{B} \inp \V{v} ,\\
(\T{A}\inp\T{B})\inp\V{v} \;&=\; \T{A}\inp(\T{B}\inp\V{v})
\end{aligned} ( α A ) ⋅ v ( A + B ) ⋅ v ( A ⋅ B ) ⋅ v = A ⋅ ( α v ) , = A ⋅ v + B ⋅ v , = A ⋅ ( B ⋅ v ) Note that (in general):
A ⋅ B ≠ B ⋅ A \T{A}\inp\T{B} \;\neq\; \T{B}\inp\T{A} A ⋅ B = B ⋅ A The inner product of a tensor with itself is called the square of a tensor, i.e.
A 2 = A ⋅ A \T{A}^2 \;=\; \T{A}\inp\T{A} A 2 = A ⋅ A Likewise, higher-order exponents are defined through repeated inner products, e.g.,
A 3 = A ⋅ A ⋅ A \T{A}^3 \;=\; \T{A}\inp\T{A}\inp\T{A} A 3 = A ⋅ A ⋅ A A.3.3 Tensor components; matrix notation of a tensor ¶ Consider a three-dimensional space with a basis { e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 } . Then, according to
(A.25) , all vectors a ⃗ i \V{a}_i a i and b ⃗ i \V{b}_i b i in relation (A.35) can
be written with respect to this basis. Substitution of these expressions in
(A.35) results into:
A = A 11 e ⃗ 1 e ⃗ 1 + A 12 e ⃗ 1 e ⃗ 2 + A 13 e ⃗ 1 e ⃗ 3 + A 21 e ⃗ 2 e ⃗ 1 + A 22 e ⃗ 2 e ⃗ 2 + A 23 e ⃗ 2 e ⃗ 3 + A 31 e ⃗ 3 e ⃗ 1 + A 32 e ⃗ 3 e ⃗ 2 + A 33 e ⃗ 3 e ⃗ 3 \begin{aligned}
\T{A} \;=\; & A_{11}\V{e}_1\V{e}_1 + A_{12}\V{e}_1\V{e}_2 + A_{13}\V{e}_1\V{e}_3 + \\
& A_{21}\V{e}_2\V{e}_1 + A_{22}\V{e}_2\V{e}_2 + A_{23}\V{e}_2\V{e}_3 + \\
& A_{31}\V{e}_3\V{e}_1 + A_{32}\V{e}_3\V{e}_2 + A_{33}\V{e}_3\V{e}_3
\end{aligned} A = A 11 e 1 e 1 + A 12 e 1 e 2 + A 13 e 1 e 3 + A 21 e 2 e 1 + A 22 e 2 e 2 + A 23 e 2 e 3 + A 31 e 3 e 1 + A 32 e 3 e 2 + A 33 e 3 e 3 where the coefficients A i j A_{ij} A ij are functions of the coefficients
α i \alpha_i α i and the components of the vectors a ⃗ \V{a} a and b ⃗ \V{b} b . Note that the
coefficients now coincide with the index notation. Thus the tensor A \T{A} A can be
expressed as a finite sum of 9 dyads of the base vectors. The coefficients A i j A_{ij} A ij are
called the components of the tensor A \T{A} A with respect to the basis
{ e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 } . In general, a component A i j A_{ij} A ij of a tensor A \T{A} A can
be obtained by:
A i j = e ⃗ i ⋅ A ⋅ e ⃗ j A_{ij} \;=\; \V{e}_i \inp \T{A} \inp \V{e}_j A ij = e i ⋅ A ⋅ e j as can be verified from substitution of (A.47) in this equation. For
convenience, we can store the components
A i j A_{ij} A ij in a matrix A ‾ \M{A} A :
A ‾ = [ A 11 A 12 A 13 A 21 A 22 A 23 A 31 A 32 A 33 ] = [ ( e ⃗ 1 ⋅ A ⋅ e ⃗ 1 ) ( e ⃗ 1 ⋅ A ⋅ e ⃗ 2 ) ( e ⃗ 1 ⋅ A ⋅ e ⃗ 3 ) ( e ⃗ 2 ⋅ A ⋅ e ⃗ 1 ) ( e ⃗ 2 ⋅ A ⋅ e ⃗ 2 ) ( e ⃗ 2 ⋅ A ⋅ e ⃗ 3 ) ( e ⃗ 3 ⋅ A ⋅ e ⃗ 1 ) ( e ⃗ 3 ⋅ A ⋅ e ⃗ 2 ) ( e ⃗ 3 ⋅ A ⋅ e ⃗ 3 ) ] = [ e ⃗ 1 e ⃗ 2 e ⃗ 3 ] ⋅ A ⋅ [ e ⃗ 1 e ⃗ 2 e ⃗ 3 ] = e ⃗ ∼ ⋅ A ⋅ e ⃗ ∼ T \begin{aligned}
\M{A}
\;&=\;
\begin{bmatrix}
A_{11} & A_{12} & A_{13} \\
A_{21} & A_{22} & A_{23} \\
A_{31} & A_{32} & A_{33}
\end{bmatrix} \\
\;&=\; \begin{bmatrix}
(\V{e}_1 \inp \T{A} \inp \V{e}_1) & (\V{e}_1 \inp \T{A} \inp \V{e}_2) &
(\V{e}_1 \inp \T{A} \inp \V{e}_3) \\
(\V{e}_2 \inp \T{A} \inp \V{e}_1) & (\V{e}_2 \inp \T{A} \inp \V{e}_2) &
(\V{e}_2 \inp \T{A} \inp \V{e}_3) \\
(\V{e}_3 \inp \T{A} \inp \V{e}_1) & (\V{e}_3 \inp \T{A} \inp \V{e}_2) &
(\V{e}_3 \inp \T{A} \inp \V{e}_3)
\end{bmatrix} \\
\;&=\; \begin{bmatrix} \V{e}_1 \\ \V{e}_2 \\ \V{e}_3 \end{bmatrix} \inp
\T{A} \inp \begin{bmatrix} \V{e}_1 & \V{e}_2 & \V{e}_3 \end{bmatrix} \\
\;&=\; \C{\V{e}} \inp \T{A} \inp \C{\V{e}}^T
\end{aligned} A = ⎣ ⎡ A 11 A 21 A 31 A 12 A 22 A 32 A 13 A 23 A 33 ⎦ ⎤ = ⎣ ⎡ ( e 1 ⋅ A ⋅ e 1 ) ( e 2 ⋅ A ⋅ e 1 ) ( e 3 ⋅ A ⋅ e 1 ) ( e 1 ⋅ A ⋅ e 2 ) ( e 2 ⋅ A ⋅ e 2 ) ( e 3 ⋅ A ⋅ e 2 ) ( e 1 ⋅ A ⋅ e 3 ) ( e 2 ⋅ A ⋅ e 3 ) ( e 3 ⋅ A ⋅ e 3 ) ⎦ ⎤ = ⎣ ⎡ e 1 e 2 e 3 ⎦ ⎤ ⋅ A ⋅ [ e 1 e 2 e 3 ] = ∼ e ⋅ A ⋅ ∼ e T Using the matrix A ‾ \M{A} A , relation (A.47) can be rewritten as:
A = [ e ⃗ 1 e ⃗ 2 e ⃗ 3 ] [ A 11 A 12 A 13 A 21 A 22 A 23 A 31 A 32 A 33 ] [ e ⃗ 1 e ⃗ 2 e ⃗ 3 ] = e ⃗ ∼ T A ‾ e ⃗ ∼ \begin{aligned}
\T{A} \;&=\; \begin{bmatrix} \V{e}_1 & \V{e}_2 & \V{e}_3 \end{bmatrix}
\begin{bmatrix} A_{11} & A_{12} & A_{13} \\
A_{21} & A_{22} & A_{23} \\
A_{31} & A_{32} & A_{33} \end{bmatrix}
\begin{bmatrix} \V{e}_1 \\ \V{e}_2 \\ \V{e}_3 \end{bmatrix} \\
\;&=\; \C{\V{e}}^T \M{A} \; \C{\V{e}}
\end{aligned} A = [ e 1 e 2 e 3 ] ⎣ ⎡ A 11 A 21 A 31 A 12 A 22 A 32 A 13 A 23 A 33 ⎦ ⎤ ⎣ ⎡ e 1 e 2 e 3 ⎦ ⎤ = ∼ e T A ∼ e Together, equations (A.49) and (A.50) describe the transformation from
tensor to matrix and back.
In (A.37) , the unit tensor I \T{I} I was defined. After
writing I \T{I} I in the general form (A.47) and applying definition
(A.37) , it can be derived that the unit tensor can be written as:
I = e ⃗ 1 e ⃗ 1 + e ⃗ 2 e ⃗ 2 + e ⃗ 3 e ⃗ 3 \T{I} \;=\; \V{e}_1\V{e}_1 + \V{e}_2\V{e}_2 + \V{e}_3\V{e}_3 I = e 1 e 1 + e 2 e 2 + e 3 e 3 Thus, for the unit matrix I ‾ \M{I} I belonging to the unit tensor I \T{I} I it
holds:
I ‾ = e ⃗ ∼ ⋅ e ⃗ ∼ T = [ 1 0 0 0 1 0 0 0 1 ] \M{I} \;=\; \C{\V{e}}\inp\C{\V{e}}^T =
\begin{bmatrix} 1 & 0 & 0 \\ 0 & 1 & 0 \\ 0 & 0 & 1 \end{bmatrix} I = ∼ e ⋅ ∼ e T = ⎣ ⎡ 1 0 0 0 1 0 0 0 1 ⎦ ⎤ A.3.4 Scalar functions of a tensor ¶ A.3.4.1 Euclidean norm ¶ The Euclidean norm [7] m m m of a tensor, a measure of its
magnitude, is defined by:
m = ∥ A ∥ = max e ⃗ ∥ A ⋅ e ⃗ ∥ ∀ e ⃗ with ∥ e ⃗ ∥ = 1. m \;=\; \| \T{A} \| = \max_{\V{e}} \| \T{A} \inp \V{e} \| \quad \forall\;
\V{e} \text{ with } \| \V{e} \| = 1 . m = ∥ A ∥ = e max ∥ A ⋅ e ∥ ∀ e with ∥ e ∥ = 1. The norm is an invariant quantity [8] , i.e. it is independent of
the choice of the basis. With respect to the norm of a tensor, the following properties
hold:
∥ A ∥ ≥ 0 ∥ α A ∥ = ∣ α ∣ ∥ A ∥ ∥ A ⋅ B ∥ ≤ ∥ A ∥ ∥ B ∥ ∥ A + B ∥ ≤ ∥ A ∥ + ∥ B ∥ \begin{aligned}
\| \T{A} \| \;&\geq\; 0 \\
\| \alpha \T{A} \| \;&=\; |\alpha|\; \| \T{A} \| \\
\| \T{A} \inp \T{B} \| \;&\leq\; \| \T{A} \|\; \| \T{B} \| \\
\| \T{A} + \T{B} \| \;&\leq\; \| \T{A} \| + \| \T{B} \|
\end{aligned} ∥ A ∥ ∥ α A ∥ ∥ A ⋅ B ∥ ∥ A + B ∥ ≥ 0 = ∣ α ∣ ∥ A ∥ ≤ ∥ A ∥ ∥ B ∥ ≤ ∥ A ∥ + ∥ B ∥ A.3.4.2 The first invariant ¶ The first invariant of a tensor A \T{A} A , also called the trace [9]
of A \T{A} A , is defined as:
J 1 ( A ) = tr ( A ) = 1 c ⃗ 1 × c ⃗ 2 ⋅ c ⃗ 3 [ c ⃗ 1 ⋅ A ⋅ ( c ⃗ 2 × c ⃗ 3 ) + c ⃗ 2 ⋅ A ⋅ ( c ⃗ 3 × c ⃗ 1 ) + c ⃗ 3 ⋅ A ⋅ ( c ⃗ 1 × c ⃗ 2 ) ] \begin{alignedat}{2}
J_1(\T{A}) \;&=\; \tr(\T{A}) && \\
&\;=\; \tfrac{1}{\V{c}_1 \cross \V{c}_2 \inp \V{c}_3}
[&& \V{c}_1 \inp \T{A} \inp ( \V{c}_2 \cross \V{c}_3 ) + \\
& && \V{c}_2 \inp \T{A} \inp ( \V{c}_3 \cross \V{c}_1 ) +
\V{c}_3 \inp \T{A} \inp ( \V{c}_1 \cross \V{c}_2 ) ]
\end{alignedat} J 1 ( A ) = tr ( A ) = c 1 × c 2 ⋅ c 3 1 [ c 1 ⋅ A ⋅ ( c 2 × c 3 ) + c 2 ⋅ A ⋅ ( c 3 × c 1 ) + c 3 ⋅ A ⋅ ( c 1 × c 2 )] where { c ⃗ 1 , c ⃗ 2 , c ⃗ 3 } \{ \V{c}_1, \V{c}_2, \V{c}_3 \} { c 1 , c 2 , c 3 } represents a vector basis.
Since J 1 ( A ) J_1(\T{A}) J 1 ( A ) is an invariant quantity, it can also be calculated
using an orthonormal basis { e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 } :
J 1 ( A ) = e ⃗ 1 ⋅ A ⋅ e ⃗ 1 + e ⃗ 2 ⋅ A ⋅ e ⃗ 2 + e ⃗ 3 ⋅ A ⋅ e ⃗ 3 = A 11 + A 22 + A 33 = tr A ‾ \begin{aligned}
J_1(\T{A}) \;&=\;
\V{e}_1 \inp \T{A} \inp \V{e}_1 +
\V{e}_2 \inp \T{A} \inp \V{e}_2 +
\V{e}_3 \inp \T{A} \inp \V{e}_3 \\
\;&=\; A_{11} + A_{22} + A_{33}\\
\;&=\; \tr{\M{A}}
\end{aligned} J 1 ( A ) = e 1 ⋅ A ⋅ e 1 + e 2 ⋅ A ⋅ e 2 + e 3 ⋅ A ⋅ e 3 = A 11 + A 22 + A 33 = tr A The following properties hold for the first invariant:
J 1 ( A ) = J 1 ( A T ) J 1 ( I ) = 3 J 1 ( α A ) = α J 1 ( A ) J 1 ( A + B ) = J 1 ( A ) + J 1 ( B ) \begin{aligned}
J_1(\T{A}) \;&=\; J_1(\T{A}^T) \\
J_1(\T{I}) \;&=\; 3 \\
J_1(\alpha \T{A}) \;&=\; \alpha J_1(\T{A}) \\
J_1(\T{A} + \T{B}) \;&=\; J_1(\T{A}) + J_1(\T{B})
\end{aligned} J 1 ( A ) J 1 ( I ) J 1 ( α A ) J 1 ( A + B ) = J 1 ( A T ) = 3 = α J 1 ( A ) = J 1 ( A ) + J 1 ( B ) A.3.4.3 The second invariant ¶ The second invariant of a tensor A \T{A} A is defined as:
J 2 ( A ) = 1 2 { tr 2 ( A ) − tr ( A 2 ) } = 1 c ⃗ 1 × c ⃗ 2 ⋅ c ⃗ 3 [ c ⃗ 1 ⋅ ( A ⋅ c ⃗ 2 ) × ( A ⋅ c ⃗ 3 ) + c ⃗ 2 ⋅ ( A ⋅ c ⃗ 3 ) × ( A ⋅ c ⃗ 1 ) + c ⃗ 3 ⋅ ( A ⋅ c ⃗ 1 ) × ( A ⋅ c ⃗ 2 ) ] \begin{alignedat}{2}
J_2(\T{A}) \;&=\; \half \{ \tr^2(\T{A}) - &&\tr(\T{A}^2) \} \\
\;&=\; \tfrac{1}{\V{c}_1 \cross \V{c}_2 \inp \V{c}_3}
[&& \V{c}_1 \inp (\T{A} \inp \V{c}_2) \cross (\T{A} \inp \V{c}_3) + \\
&&& \V{c}_2 \inp (\T{A} \inp \V{c}_3) \cross (\T{A} \inp \V{c}_1) + \\
&&& \V{c}_3 \inp (\T{A} \inp \V{c}_1) \cross (\T{A} \inp \V{c}_2) ]
\end{alignedat} J 2 ( A ) = 2 1 { tr 2 ( A ) − = c 1 × c 2 ⋅ c 3 1 [ tr ( A 2 )} c 1 ⋅ ( A ⋅ c 2 ) × ( A ⋅ c 3 ) + c 2 ⋅ ( A ⋅ c 3 ) × ( A ⋅ c 1 ) + c 3 ⋅ ( A ⋅ c 1 ) × ( A ⋅ c 2 )] The following properties hold for the second invariant:
J 2 ( A ) = J 2 ( A T ) J 2 ( I ) = 3 J 2 ( α A ) = α 2 J 2 ( A ) \begin{aligned}
J_2(\T{A}) \;&=\; J_2(\T{A}^T) \\
J_2(\T{I}) \;&=\; 3 \\
J_2(\alpha \T{A}) \;&=\; \alpha^2 J_2(\T{A})
\end{aligned} J 2 ( A ) J 2 ( I ) J 2 ( α A ) = J 2 ( A T ) = 3 = α 2 J 2 ( A ) A.3.4.4 The third invariant ¶ The third invariant of a tensor A \T{A} A , also called the
determinant of A \T{A} A , is defined as:
J 3 ( A ) = det ( A ) = 1 c ⃗ 1 × c ⃗ 2 ⋅ c ⃗ 3 ( A ⋅ c ⃗ 1 ) ⋅ ( A ⋅ c ⃗ 2 ) × ( A ⋅ c ⃗ 3 ) J_3(\T{A}) \;=\; \det(\T{A}) \;=\;
\tfrac{1}{\V{c}_1 \cross \V{c}_2 \inp \V{c}_3}
(\T{A} \inp \V{c}_1) \inp (\T{A} \inp \V{c}_2) \cross (\T{A} \inp
\V{c}_3) J 3 ( A ) = det ( A ) = c 1 × c 2 ⋅ c 3 1 ( A ⋅ c 1 ) ⋅ ( A ⋅ c 2 ) × ( A ⋅ c 3 ) For the third invariant, the following properties hold:
J 3 ( A ) = J 3 ( A T ) J 3 ( I ) = 1 J 3 ( α A ) = α 3 J 3 ( A ) J 3 ( A ⋅ B ) = J 3 ( A ) J 3 ( B ) \begin{aligned}
J_3(\T{A}) \;&=\; J_3(\T{A}^T)\\
J_3(\T{I}) \;&=\; 1 \\
J_3(\alpha \T{A}) \;&=\; \alpha^3 J_3(\T{A}) \\
J_3(\T{A} \inp \T{B}) \;&=\; J_3(\T{A}) J_3(\T{B})
\end{aligned} J 3 ( A ) J 3 ( I ) J 3 ( α A ) J 3 ( A ⋅ B ) = J 3 ( A T ) = 1 = α 3 J 3 ( A ) = J 3 ( A ) J 3 ( B ) The determinant of a tensor equals the determinant of its matrix with respect to an
orthonormal basis.
det ( A ) = det ( A ‾ ) \det(\T{A}) \;=\; \det(\M{A}) det ( A ) = det ( A ) If det ( A ) \det(\T{A}) det ( A ) is nonzero, i.e. the triple product of the transformed base vectors is
nonzero, the tensor is called a regular tensor [10] . If det ( A ) \det(\T{A}) det ( A ) is zero, the tensor A \T{A} A is called a singular
tensor [11] . In the latter case all vectors in
three-dimensional space are transformed into vectors lying in a plane (or on a line).
Vectors perpendicular to that plane (or that line), are transformed into the zero vector.
A.3.4.5 Scalar product ¶ The scalar product , double dot product or double inner product or convolution [12] of two tensors A \T{A} A and B \T{B} B is the contraction of these two tensors, denoted by A : B \T{A}\dinp\T{B} A : B , is a scalar, defined
as:
A : B = tr ( A ⋅ B ) \T{A}\dinp\T{B} \;=\; \tr (\T{A}\inp\T{B} ) A : B = tr ( A ⋅ B ) In index notation, this product is the full contraction of indices
A : B = A i j B j i \T{A}\dinp\T{B} \;=\; A_{ij} B_{ji} A : B = A ij B ji Some properties are:
A : I = tr ( A ) A : B = B : A = A T : B T = B T : A T \begin{aligned}
\T{A}\dinp\T{I} \;&=\; \tr(\T{A})\\
\T{A}\dinp\T{B} \;&=\; \T{B}\dinp\T{A} \\
\;&=\; \T{A}^T\dinp\T{B}^T\\
\;&=\; \T{B}^T\dinp\T{A}^T
\end{aligned} A : I A : B = tr ( A ) = B : A = A T : B T = B T : A T A.3.4.6 Some properties of the invariants of a tensor ¶ The three principal invariants of a tensor are related through the Caley-Hamilton
theorem :
A 3 − J 1 ( A ) A 2 + J 2 ( A ) A − J 3 ( A ) I = 0 \T{A}^3 - J_1(\T{A})\T{A}^2 + J_2(\T{A})\T{A} - J_3(\T{A})\T{I} \;=\; \T{0} A 3 − J 1 ( A ) A 2 + J 2 ( A ) A − J 3 ( A ) I = 0 The conjugated tensor A T \T{A}^T A T satisfies the same equation.
For any non-singular tensor it holds that:
J 1 ( A − 1 ) = J 2 ( A ) J 3 ( A ) J 2 ( A − 1 ) = J 1 ( A ) J 3 ( A ) J 3 ( A − 1 ) = 1 J 3 ( A ) \begin{aligned}
J_1(\T{A}^{-1}) \;&=\; \frac{J_2(\T{A})}{J_3(\T{A})}\\
J_2(\T{A}^{-1}) \;&=\; \frac{J_1(\T{A})}{J_3(\T{A})}\\
J_3(\T{A}^{-1}) \;&=\; \frac{1}{J_3(\T{A})}
\end{aligned} J 1 ( A − 1 ) J 2 ( A − 1 ) J 3 ( A − 1 ) = J 3 ( A ) J 2 ( A ) = J 3 ( A ) J 1 ( A ) = J 3 ( A ) 1 Any function of the principal invariants of a tensor A \T{A} A is an invariant as well.
A.3.5 Eigenvalues and eigenvectors of a tensor ¶ The eigenvalues [13] λ \lambda λ and the
eigenvectors [14] n ⃗ \V{n} n of a tensor A \T{A} A are defined as those
scalars and vectors that satisfy the following equation:
A ⋅ n ⃗ = λ n ⃗ with n ⃗ ≠ 0 ⃗ \T{A} \inp \V{n} \;=\; \lambda \V{n} \quad \text{ with } \quad \V{n} \neq
\V{0} A ⋅ n = λ n with n = 0 To compute the eigenvalues and eigenvectors of a tensor, we proceed as
follows. First equation (A.68) is rewritten as:
A ⋅ n ⃗ = λ n ⃗ ⇒ A ⋅ n ⃗ − λ n ⃗ = 0 ⃗ ⇒ A ⋅ n ⃗ − λ I ⋅ n ⃗ = 0 ⃗ ⇒ ( A − λ I ) ⋅ n ⃗ = 0 ⃗ \begin{aligned}
\T{A} \inp \V{n} \;&=\; \lambda \V{n} \quad \Rightarrow \\
\T{A} \inp \V{n} - \lambda \V{n} \;&=\; \V{0} \quad \Rightarrow \\
\T{A} \inp \V{n} - \lambda \T{I} \inp \V{n} \;&=\; \V{0} \quad \Rightarrow \\
(\T{A} - \lambda \T{I}) \inp \V{n} \;&=\; \V{0}
\end{aligned} A ⋅ n A ⋅ n − λ n A ⋅ n − λ I ⋅ n ( A − λ I ) ⋅ n = λ n ⇒ = 0 ⇒ = 0 ⇒ = 0 Since n ⃗ ≠ 0 ⃗ \V{n} \neq \V{0} n = 0 , the tensor A − λ I \T{A} - \lambda \T{I} A − λ I must be
singular, meaning that:
det ( A − λ I ) = 0 ⇒ det ( A ‾ − λ I ‾ ) = 0 \det(\T{A} - \lambda \T{I}) \;=\; 0 \quad \Rightarrow \quad
\det(\M{A} - \lambda \M{I}) \;=\; 0 det ( A − λ I ) = 0 ⇒ det ( A − λ I ) = 0 Elaboration of the latter equation leads to the characteristic equation :
λ 3 − J 1 ( A ) λ 2 + J 2 ( A ) λ − J 3 ( A ) = 0 \lambda^3 - J_1(\T{A}) \lambda^2 + J_2(\T{A}) \lambda - J_3(\T{A}) \;=\;
0 λ 3 − J 1 ( A ) λ 2 + J 2 ( A ) λ − J 3 ( A ) = 0 This equation has three roots λ 1 \lambda_1 λ 1 , λ 2 \lambda_2 λ 2 and λ 3 \lambda_3 λ 3 .
The eigenvector n ⃗ i \V{n}_i n i corresponding with the eigenvalue λ i \lambda_i λ i
is found from the following set of linear equations:
( A − λ i I ) ⋅ n ⃗ i = 0 ⃗ ⇒ ( A ‾ − λ i I ‾ ) n ∼ i = 0 ∼ (\T{A} - \lambda_i \T{I}) \inp \V{n}_i \;=\; \V{0} \quad \Rightarrow \quad
(\M{A} - \lambda_i \M{I}) \C{n}_i \;=\; \C{0} ( A − λ i I ) ⋅ n i = 0 ⇒ ( A − λ i I ) ∼ n i = ∼ 0 Since this is not an independent set of equations, it yields only the
ratio n i 1 : n i 2 : n i 3 n_{i1} \dinp n_{i2} \dinp n_{i3} n i 1 : n i 2 : n i 3 of the components
of the eigenvector. A unique solution is obtained by the additional
requirement that the eigenvector has unit length:
∥ n ⃗ i ∥ = 1 ⇒ n i 1 2 + n i 2 2 + n i 3 2 = 1 \| \V{n}_i \| \;=\; 1 \quad \Rightarrow \quad n_{i1}^2 + n_{i2}^2 + n_{i3}^2 = 1 ∥ n i ∥ = 1 ⇒ n i 1 2 + n i 2 2 + n i 3 2 = 1 The principal invariants of a tensor are then equal to:
J 1 ( A ) = λ 1 + λ 2 + λ 3 J 2 ( A ) = λ 1 λ 2 + λ 1 λ 3 + λ 2 λ 3 J 3 ( A ) = λ 1 λ 2 λ 3 \begin{aligned}
J_1(\T{A}) \;&=\; \lambda_1 + \lambda_2 + \lambda_3 \\
J_2(\T{A}) \;&=\; \lambda_1\lambda_2 + \lambda_1\lambda_3 + \lambda_2\lambda_3\\
J_3(\T{A}) \;&=\; \lambda_1 \lambda_2 \lambda_3
\end{aligned} J 1 ( A ) J 2 ( A ) J 3 ( A ) = λ 1 + λ 2 + λ 3 = λ 1 λ 2 + λ 1 λ 3 + λ 2 λ 3 = λ 1 λ 2 λ 3 A.3.6 Some special tensors ¶ A.3.6.1 Inverse tensor ¶ The inverse tensor A − 1 \T{A}^{-1} A − 1 of a tensor A \T{A} A is defined as the tensor that satisfies the following
equation:
A − 1 ⋅ A = I \T{A}^{-1} \inp \T{A} \;=\; \T{I} A − 1 ⋅ A = I A − 1 \T{A}^{-1} A − 1 only exists if A \T{A} A is regular.
The components of the inverse tensor are given by the inverse matrix A ‾ − 1 \M{A}^{-1} A − 1
[ A − 1 ] i j = 1 det ( A ‾ ) [ ( − 1 ) i + j M i j ] T [A^{-1}]_{ij} \;=\; \frac{1}{\det(\M{A})}\left[ (-1)^{i+j} M_{ij}\right]^T [ A − 1 ] ij = det ( A ) 1 [ ( − 1 ) i + j M ij ] T where M i j M_{ij} M ij is the minor of the component A i j A_{ij} A ij , i.e. the determinant of the matrix
that is obtained by deleting row i i i and column j j j .
The inverse of the product of two tensors is given by:
( A ⋅ B ) − 1 = B − 1 ⋅ A − 1 (\T{A} \inp \T{B} )^{-1} \;=\; \T{B}^{-1} \inp \T{A}^{-1} ( A ⋅ B ) − 1 = B − 1 ⋅ A − 1 The proof is obtained by comparing the following expressions for a ⃗ \V{a} a :
( A ⋅ B ) ⋅ a ⃗ = b ⃗ ⇒ a ⃗ = ( A ⋅ B ) − 1 ⋅ b ⃗ \begin{aligned}
(\T{A} \inp \T{B}) \inp \V{a} \;&=\; \V{b} \quad \Rightarrow \\
\V{a} \;&=\; (\T{A} \inp \T{B})^{-1} \inp \V{b}
\end{aligned} ( A ⋅ B ) ⋅ a a = b ⇒ = ( A ⋅ B ) − 1 ⋅ b and
( A ⋅ B ) ⋅ a ⃗ = A ⋅ ( B ⋅ a ⃗ ) = b ⃗ ⇒ B ⋅ a ⃗ = A − 1 ⋅ b ⃗ ⇒ a ⃗ = B − 1 ⋅ A − 1 ⋅ b ⃗ \begin{aligned}
(\T{A} \inp \T{B}) \inp \V{a} \;&=\; \T{A} \inp (\T{B} \inp \V{a}) = \V{b} \quad \Rightarrow \\
\T{B} \inp \V{a} \;&=\; \T{A}^{-1} \inp \V{b} \qquad \Rightarrow \\
\V{a} \;&=\; \T{B}^{-1} \inp \T{A}^{-1} \inp \V{b}
\end{aligned} ( A ⋅ B ) ⋅ a B ⋅ a a = A ⋅ ( B ⋅ a ) = b ⇒ = A − 1 ⋅ b ⇒ = B − 1 ⋅ A − 1 ⋅ b A.3.6.2 Deviatoric part of a tensor ¶ The deviatoric part [15] A d \T{A}^d A d of a tensor A \T{A} A is
defined as:
A d = A − 1 3 tr ( A ) I \T{A}^d \;=\; \T{A} - \tfrac{1}{3} \tr(\T{A}) \T{I} A d = A − 3 1 tr ( A ) I where 1 3 tr ( A ) I \tfrac{1}{3} \tr(\T{A}) \T{I} 3 1 tr ( A ) I is called the hydrostatic or
spherical[16] part of
A \T{A} A . For the deviatoric part, the
following properties hold:
( A + B ) d = A d + B d tr ( A d ) = 0 \begin{aligned}
(\T{A} + \T{B})^d \;&=\; \T{A}^d + \T{B}^d \\
\tr(\T{A}^d) \;&=\; 0
\end{aligned} ( A + B ) d tr ( A d ) = A d + B d = 0 A.3.6.3 Symmetric tensor ¶ A tensor A \T{A} A is called symmetric if:
A T = A \T{A}^T \;=\; \T{A} A T = A For the components A i j A_{ij} A ij of a symmetric tensor A \T{A} A with respect to
an orthonormal basis it holds that:
A i j = A j i A_{ij} \;=\; A_{ji} A ij = A ji i.e. the matrix A ‾ \M{A} A corresponding to A \T{A} A is symmetric too.
The eigenvalues λ i \lambda_i λ i and eigenvectors n ⃗ i \V{n}_i n i of a symmetric
tensor have the following important properties:
the eigenvalues and eigenvectors are real
if two eigenvalues are different, the corresponding eigenvectors are mutually perpendicular
if two eigenvalues are equal, the corresponding eigenvectors can be chosen mutually perpendicular
Thus, the set of eigenvectors can be used as an orthonormal basis.
Figure A.12: The orthonormal basis of eigenvectors { n ⃗ 1 , n ⃗ 2 , n ⃗ 3 } \{ \V{n}_1, \V{n}_2, \V{n}_3 \} { n 1 , n 2 , n 3 }
of a symmetric tensor.
If a tensor A \T{A} A is considered with respect to the basis of its eigenvectors, we find
the spectral form [17] of the tensor:
A = A ⋅ I = A ⋅ ( n ⃗ 1 n ⃗ 1 + n ⃗ 2 n ⃗ 2 + n ⃗ 3 n ⃗ 3 ) = λ 1 n ⃗ 1 n ⃗ 1 + λ 2 n ⃗ 2 n ⃗ 2 + λ 3 n ⃗ 3 n ⃗ 3 \begin{aligned}
\T{A} \;&=\; \T{A} \inp \T{I} \\
\;&=\; \T{A} \inp ( \V{n}_1\V{n}_1 + \V{n}_2\V{n}_2 + \V{n}_3\V{n}_3 ) \\
\;&=\; \lambda_1 \V{n}_1\V{n}_1 + \lambda_2 \V{n}_2\V{n}_2 + \lambda_3 \V{n}_3\V{n}_3
\end{aligned} A = A ⋅ I = A ⋅ ( n 1 n 1 + n 2 n 2 + n 3 n 3 ) = λ 1 n 1 n 1 + λ 2 n 2 n 2 + λ 3 n 3 n 3 The matrix A ‾ \M{A} A of A \T{A} A with respect to this basis is a diagonal
matrix:
A ‾ = [ λ 1 0 0 0 λ 2 0 0 0 λ 3 ] \M{A} \;=\; \begin{bmatrix}
\lambda_1 & 0 & 0 \\
0 & \lambda_2 & 0 \\
0 & 0 & \lambda_3
\end{bmatrix} A = ⎣ ⎡ λ 1 0 0 0 λ 2 0 0 0 λ 3 ⎦ ⎤ Using the spectral form, some functions of a tensor can easily be calculated. E.g. for
the inverse , the square root , and the natural logarithm of a tensor
A \T{A} A it holds that:
A − 1 = λ 1 − 1 n ⃗ 1 n ⃗ 1 + λ 2 − 1 n ⃗ 2 n ⃗ 2 + λ 3 − 1 n ⃗ 3 n ⃗ 3 A 1 / 2 = λ 1 1 / 2 n ⃗ 1 n ⃗ 1 + λ 2 1 / 2 n ⃗ 2 n ⃗ 2 + λ 3 1 / 2 n ⃗ 3 n ⃗ 3 ln A = ln ( λ 1 ) n ⃗ 1 n ⃗ 1 + ln ( λ 2 ) n ⃗ 2 n ⃗ 2 + ln ( λ 3 ) n ⃗ 3 n ⃗ 3 \begin{aligned}
\T{A}^{-1} \;&=\; \lambda_1^{-1} \V{n}_1\V{n}_1 + \lambda_2^{-1} \V{n}_2\V{n}_2 + \lambda_3^{-1} \V{n}_3\V{n}_3 \\
\T{A}^{1/2} \;&=\; \lambda_1^{1/2} \V{n}_1\V{n}_1 + \lambda_2^{1/2} \V{n}_2\V{n}_2 + \lambda_3^{1/2} \V{n}_3\V{n}_3 \\
\ln \T{A} \;&=\; \ln(\lambda_1) \V{n}_1\V{n}_1 + \ln(\lambda_2)
\V{n}_2\V{n}_2 + \ln(\lambda_3) \V{n}_3\V{n}_3
\end{aligned} A − 1 A 1/2 ln A = λ 1 − 1 n 1 n 1 + λ 2 − 1 n 2 n 2 + λ 3 − 1 n 3 n 3 = λ 1 1/2 n 1 n 1 + λ 2 1/2 n 2 n 2 + λ 3 1/2 n 3 n 3 = ln ( λ 1 ) n 1 n 1 + ln ( λ 2 ) n 2 n 2 + ln ( λ 3 ) n 3 n 3 A.3.6.4 Skewsymmetric tensor ¶ A tensor A \T{A} A is called skewsymmetric [18] or
antisymmetric if:
A T = − A \T{A}^T \;=\; - \T{A} A T = − A For the components A i j A_{ij} A ij of a skewsymmetric tensor A \T{A} A with respect to
an orthonormal basis it holds that:
A i j = − A j i ⇒ A i i = 0 A_{ij} \;=\; - A_{ji} \quad \Rightarrow \quad A_{ii} \;=\; 0 A ij = − A ji ⇒ A ii = 0 If A \T{A} A is skewsymmetric and B \T{B} B is symmetric, then:
A : B = 0 e s p e c i a l l y A : I = tr A = 0 \T{A}:\T{B}=0 \quad {\rm especially} \quad \T{A}:\T{I} = \tr\T{A} = 0 A : B = 0 especially A : I = tr A = 0 The proof follows from:
A : B = A T : B T = − A : B \T{A} \dinp \T{B} \;=\; \T{A}^T \dinp \T{B}^T \;=\; - \T{A} \dinp \T{B} A : B = A T : B T = − A : B If A \T{A} A is skewsymmetric, then a unique axial vector [19]
ω ⃗ \V{\omega} ω exists, such that:
A ⋅ q ⃗ = ω ⃗ × q ⃗ \T{A} \inp \V{q} \;=\; \V{\omega} \cross \V{q} A ⋅ q = ω × q The proof of the existence of ω ⃗ \V{\omega} ω is as follows:
A ⋅ q ⃗ = p ⃗ ⇒ q ⃗ ⋅ A ⋅ q ⃗ = q ⃗ ⋅ A T ⋅ q ⃗ = − q ⃗ ⋅ A ⋅ q ⃗ ⇒ q ⃗ ⋅ A ⋅ q ⃗ = 0 ⇒ q ⃗ ⋅ p ⃗ = 0 ⇒ q ⃗ ⊥ p ⃗ ⇒ ∃ ω ⃗ such that p ⃗ = ω ⃗ × q ⃗ \begin{aligned}
\T{A} \inp \V{q} \;&=\; \V{p} \quad \Rightarrow \\
\V{q} \inp \T{A} \inp \V{q} \;&=\; \V{q} \inp \T{A}^T \inp \V{q} \\
\;&=\; - \; \V{q} \inp \T{A} \inp \V{q} \quad \Rightarrow \\
\V{q} \inp \T{A} \inp \V{q} \;&=\; 0 \quad \Rightarrow \\
\V{q} \inp \V{p} \;&=\; 0 \quad \Rightarrow \\
\V{q} \;&\perp\; \V{p} \quad \Rightarrow \quad
\exists\;\V{\omega} \; \text{ such that } \V{p} \;=\; \V{\omega} \cross \V{q}
\end{aligned} A ⋅ q q ⋅ A ⋅ q q ⋅ A ⋅ q q ⋅ p q = p ⇒ = q ⋅ A T ⋅ q = − q ⋅ A ⋅ q ⇒ = 0 ⇒ = 0 ⇒ ⊥ p ⇒ ∃ ω such that p = ω × q On the other hand, if:
A ⋅ q ⃗ = ω ⃗ × q ⃗ ∀ q ⃗ \T{A} \inp \V{q} \;=\; \V{\omega} \cross \V{q} \quad \forall\ \V{q} A ⋅ q = ω × q ∀ q comparison of the following expressions:
A ⋅ q ⃗ = [ e ⃗ 1 e ⃗ 2 e ⃗ 3 ] [ A 11 A 12 A 13 A 21 A 22 A 23 A 31 A 32 A 33 ] [ q 1 q 2 q 3 ] = [ e ⃗ 1 e ⃗ 2 e ⃗ 3 ] [ A 11 q 1 + A 12 q 2 + A 13 q 3 A 21 q 1 + A 22 q 2 + A 23 q 3 A 31 q 1 + A 32 q 2 + A 33 q 3 ] \begin{aligned}
\T{A} \inp \V{q}
\;&=\;
\begin{bmatrix} \V{e}_1 & \V{e}_2 & \V{e}_3 \end{bmatrix}
\begin{bmatrix}
A_{11} & A_{12} & A_{13} \\
A_{21} & A_{22} & A_{23} \\
A_{31} & A_{32} & A_{33}
\end{bmatrix}
\begin{bmatrix} q_1 \\ q_2 \\ q_3 \end{bmatrix} \\
\;&=\;
\begin{bmatrix} \V{e}_1 & \V{e}_2 & \V{e}_3 \end{bmatrix}
\begin{bmatrix}
A_{11}q_1 + A_{12}q_2 + A_{13}q_3 \\
A_{21}q_1 + A_{22}q_2 + A_{23}q_3 \\
A_{31}q_1 + A_{32}q_2 + A_{33}q_3
\end{bmatrix}
\end{aligned} A ⋅ q = [ e 1 e 2 e 3 ] ⎣ ⎡ A 11 A 21 A 31 A 12 A 22 A 32 A 13 A 23 A 33 ⎦ ⎤ ⎣ ⎡ q 1 q 2 q 3 ⎦ ⎤ = [ e 1 e 2 e 3 ] ⎣ ⎡ A 11 q 1 + A 12 q 2 + A 13 q 3 A 21 q 1 + A 22 q 2 + A 23 q 3 A 31 q 1 + A 32 q 2 + A 33 q 3 ⎦ ⎤ and
ω ⃗ × q ⃗ = ( ω 1 e ⃗ 1 + ω 2 e ⃗ 2 + ω 3 e ⃗ 3 ) × ( q 1 e ⃗ 1 + q 2 e ⃗ 2 + q 3 e ⃗ 3 ) = ω 1 q 2 ( e ⃗ 3 ) + ω 1 q 3 ( − e ⃗ 2 ) + ω 2 q 1 ( − e ⃗ 3 ) + ω 2 q 3 ( e ⃗ 1 ) + ω 3 q 1 ( e ⃗ 2 ) + ω 3 q 2 ( − e ⃗ 1 ) = [ e ⃗ 1 e ⃗ 2 e ⃗ 3 ] [ ω 2 q 3 − ω 3 q 2 ω 3 q 1 − ω 1 q 3 ω 1 q 2 − ω 2 q 1 ] \begin{alignedat}{2}
\V{\omega} \cross \V{q}
\;&=\;
&&( \omega_1 \V{e}_1 + \omega_2 \V{e}_2 + \omega_3 \V{e}_3 ) \cross
( q_1 \V{e}_1 + q_2 \V{e}_2 + q_3 \V{e}_3 ) \\
\;&=\;
&&\omega_1 q_2 ( \V{e}_3) + \omega_1 q_3 (-\,\V{e}_2) +
\omega_2 q_1 (-\,\V{e}_3) + \omega_2 q_3 ( \V{e}_1) + \\
&&& \omega_3 q_1 ( \V{e}_2) + \omega_3 q_2 (-\,\V{e}_1) \\
\;&=\; && \begin{bmatrix} \V{e}_1 & \V{e}_2 & \V{e}_3 \end{bmatrix}
\begin{bmatrix}
\omega_2 q_3 - \omega_3 q_2 \\
\omega_3 q_1 - \omega_1 q_3 \\
\omega_1 q_2 - \omega_2 q_1
\end{bmatrix}
\end{alignedat} ω × q = = = ( ω 1 e 1 + ω 2 e 2 + ω 3 e 3 ) × ( q 1 e 1 + q 2 e 2 + q 3 e 3 ) ω 1 q 2 ( e 3 ) + ω 1 q 3 ( − e 2 ) + ω 2 q 1 ( − e 3 ) + ω 2 q 3 ( e 1 ) + ω 3 q 1 ( e 2 ) + ω 3 q 2 ( − e 1 ) [ e 1 e 2 e 3 ] ⎣ ⎡ ω 2 q 3 − ω 3 q 2 ω 3 q 1 − ω 1 q 3 ω 1 q 2 − ω 2 q 1 ⎦ ⎤ shows that:
A ‾ = [ 0 − ω 3 ω 2 ω 3 0 − ω 1 − ω 2 ω 1 0 ] \M{A} \;=\;
\begin{bmatrix}
0 & -\,\omega_3 & \omega_2 \\
\omega_3 & 0 & -\,\omega_1 \\
-\,\omega_2 & \omega_1 & 0
\end{bmatrix} A = ⎣ ⎡ 0 ω 3 − ω 2 − ω 3 0 ω 1 ω 2 − ω 1 0 ⎦ ⎤ and thus that the tensor A \T{A} A is skewsymmetric.
A.3.6.5 Positive-definite tensor ¶ A tensor A \T{A} A is called positive-definite [20]
if:
a ⃗ ⋅ A ⋅ a ⃗ > 0 ∀ a ⃗ ≠ 0 ⃗ \V{a} \inp \T{A} \inp \V{a} \;>\; 0 \quad \forall\;\V{a} \neq \V{0} a ⋅ A ⋅ a > 0 ∀ a = 0 A positive-definite tensor A \T{A} A cannot be skewsymmetric.
This follows from:
a ⃗ ⋅ A ⋅ a ⃗ = a ⃗ ⋅ A T ⋅ a ⃗ > 0 ∀ a ⃗ ≠ 0 ⃗ ⇒ a ⃗ ⋅ ( A − A T ) ⋅ a ⃗ = 0 ∧ a ⃗ ≠ 0 ⃗ \begin{aligned}
\V{a} \inp \T{A} \inp \V{a}
\;&=\; \V{a} \inp \T{A}^T \inp \V{a} \\
\;&>\; 0 \quad \forall\; \V{a} \neq \V{0} \quad \Rightarrow \\
\V{a} \inp (\T{A} - \T{A}^T) \inp \V{a} \;&=\; 0 \quad \wedge \quad \V{a} \neq \V{0}
\end{aligned} a ⋅ A ⋅ a a ⋅ ( A − A T ) ⋅ a = a ⋅ A T ⋅ a > 0 ∀ a = 0 ⇒ = 0 ∧ a = 0 If A \T{A} A would be skewsymmetric, the latter equation would yield zero, since then A T = − A \T{A}^T = -\T{A} A T = − A .
A.3.6.6 Orthogonal tensor ¶ A tensor A \T{A} A is called orthogonal [21] if:
( A ⋅ a ⃗ ) ⋅ ( A ⋅ b ⃗ ) = a ⃗ ⋅ b ⃗ ∀ a ⃗ , b ⃗ (\T{A} \inp \V{a}) \inp (\T{A} \inp \V{b}) \;=\; \V{a} \inp \V{b}
\quad \forall\ \V{a},\V{b} ( A ⋅ a ) ⋅ ( A ⋅ b ) = a ⋅ b ∀ a , b For the special case b ⃗ = a ⃗ \V{b} = \V{a} b = a we get:
( A ⋅ a ⃗ ) ⋅ ( A ⋅ a ⃗ ) = a ⃗ ⋅ a ⃗ ⇒ ∥ A ⋅ a ⃗ ∥ = ∥ a ⃗ ∥ (\T{A} \inp \V{a}) \inp (\T{A} \inp \V{a}) \;=\; \V{a} \inp \V{a}
\quad \Rightarrow \quad \| \T{A} \inp \V{a} \| \;=\; \| \V{a} \| ( A ⋅ a ) ⋅ ( A ⋅ a ) = a ⋅ a ⇒ ∥ A ⋅ a ∥ = ∥ a ∥ Thus, an orthogonal transformation preserves lengths of vectors and
angles between vectors.
The inverse of an orthogonal tensor is identical to its conjugate:
A T = A − 1 \T{A}^T \;=\; \T{A}^{-1} A T = A − 1 as follows from:
( A ⋅ a ⃗ ) ⋅ ( A ⋅ b ⃗ ) = a ⃗ ⋅ A T ⋅ A ⋅ b ⃗ = a ⃗ ⋅ b ⃗ ⇒ A ⋅ A T = I ⇒ A T = A − 1 \begin{aligned}
(\T{A} \inp \V{a}) \inp (\T{A} \inp \V{b})
\;&=\; \V{a} \inp \T{A}^T \inp \T{A} \inp \V{b} \\
\;&=\; \V{a} \inp \V{b} \quad \Rightarrow \\
\T{A} \inp \T{A}^T \;&=\; \T{I} \quad \Rightarrow \\
\T{A}^T \;&=\; \T{A}^{-1}
\end{aligned} ( A ⋅ a ) ⋅ ( A ⋅ b ) A ⋅ A T A T = a ⋅ A T ⋅ A ⋅ b = a ⋅ b ⇒ = I ⇒ = A − 1 Moreover, this equation shows that:
det ( A ⋅ A T ) = [ det ( A ) ] 2 = det ( I ) = 1 ⇒ det ( A ) = ± 1 \begin{aligned}
\det(\T{A} \inp \T{A}^T) \;&=\; [\det(\T{A})]^2 = \det(\T{I}) = 1 \quad \Rightarrow \\
\det(\T{A}) \;&=\; \pm 1
\end{aligned} det ( A ⋅ A T ) det ( A ) = [ det ( A ) ] 2 = det ( I ) = 1 ⇒ = ± 1 Thus, an orthogonal tensor is a regular tensor. If det ( A ) = 1 \det(\T{A}) = 1 det ( A ) = 1 , A \T{A} A can be
shown to describe a rotation . If det ( A ) = − 1 \det(\T{A}) = -1 det ( A ) = − 1 , A \T{A} A
can be shown to describe a reflection .
A.4 Spatial derivatives of scalar and vector fields ¶ A.4.1 Derivatives of functions of one or more variables ¶ Figure A.13: A function f f f of one variable x x x and its derivative.
Consider a scalar function f ( x ) f(x) f ( x ) of one variable x x x . Using a Taylor series, the change
d f df df of the value of f f f due to a change d x dx d x in the parameter x x x can be expressed as:
d f = f ( x + d x ) − f ( x ) = f ( x ) + d f d x ∣ x d x + 1 2 d 2 f d x 2 ∣ x d x 2 + ⋯ − f ( x ) ≈ d f d x ∣ x d x \begin{aligned}
df \;&=\; f(x+dx) - f(x) \\
\;&=\; f(x) + \left.\tfrac{df}{dx}\right|_x dx +
\half \left.\tfrac{d^2f}{dx^2}\right|_x dx^2 + \dots - f(x) \\
\;&\approx\; \left.\tfrac{df}{dx}\right|_x dx
\end{aligned} df = f ( x + d x ) − f ( x ) = f ( x ) + d x df ∣ ∣ x d x + 2 1 d x 2 d 2 f ∣ ∣ x d x 2 + ⋯ − f ( x ) ≈ d x df ∣ ∣ x d x Extension to a function of two variables f ( x , y ) f(x,y) f ( x , y ) yields:
d f = f ( x + d x , y + d y ) − f ( x , y ) = f ( x , y ) + ∂ f ∂ x ∣ x , y d x + ∂ f ∂ y ∣ x , y d y + ⋯ − f ( x , y ) ≈ ∂ f ∂ x ∣ x , y d x + ∂ f ∂ y ∣ x , y d y \begin{aligned}
df \;&=\; f(x+dx,y+dy) - f(x,y) \\
\;&=\; f(x,y) + \left.\parder{f}{x}\right|_{x,y} dx +
\left.\parder{f}{y}\right|_{x,y} dy + \dots - f(x,y) \\
\;&\approx\; \left.\parder{f}{x}\right|_{x,y} dx +
\left.\parder{f}{y}\right|_{x,y} dy
\end{aligned} df = f ( x + d x , y + d y ) − f ( x , y ) = f ( x , y ) + ∂ x ∂ f ∣ ∣ x , y d x + ∂ y ∂ f ∣ ∣ x , y d y + ⋯ − f ( x , y ) ≈ ∂ x ∂ f ∣ ∣ x , y d x + ∂ y ∂ f ∣ ∣ x , y d y And for a function a ( x 1 , x 2 , x 3 ) a(x_1, x_2, x_3) a ( x 1 , x 2 , x 3 ) of three variables, the variation d a da d a of a a a , due
to (infinitesimal) variations d x 1 dx_1 d x 1 , d x 2 dx_2 d x 2 and d x 3 dx_3 d x 3 can be written as:
d a = d x 1 ∂ a ∂ x 1 + d x 2 ∂ a ∂ x 2 + d x 3 ∂ a ∂ x 3 da \;=\; dx_1 \parder{a}{x_1} + dx_2 \parder{a}{x_2} + dx_3 \parder{a}{x_3} d a = d x 1 ∂ x 1 ∂ a + d x 2 ∂ x 2 ∂ a + d x 3 ∂ x 3 ∂ a The index notation for differentiation with respect to one of the
variables (i.c. x i x_i x i ) is commonly denoted with a comma between or in
front of the indices. The equation (A.106) for d a da d a with this
convention reads
d a = d x i a , i da \;=\; dx_i a_{,i} d a = d x i a , i A.4.2 Components of the position vector ¶ In three-dimensional space, we may interpret the variables x 1 x_1 x 1 , x 2 x_2 x 2 and x 3 x_3 x 3 in the
function a ( x 1 , x 2 , x 3 ) a(x_1, x_2, x_3) a ( x 1 , x 2 , x 3 ) as the components of the position
vector [22] x ⃗ \V{x} x with respect to a Cartesian basis { e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 } . The
position vector x ⃗ \V{x} x of a point with respect to a fixed point in space, the origin O O O , can be expressed as:
x ⃗ = x 1 e ⃗ 1 + x 2 e ⃗ 2 + x 3 e ⃗ 3 \V{x} \;=\; x_1 \V{e}_1 + x_2 \V{e}_2 + x_3 \V{e}_3 x = x 1 e 1 + x 2 e 2 + x 3 e 3 Figure A.14: Components x i x_i x i of the position vector x ⃗ \V{x} x with respect to a Cartesian
basis { e ⃗ 1 , e ⃗ 2 , e ⃗ 3 } \basis { e 1 , e 2 , e 3 } .
For the position vector x ⃗ + d x ⃗ \V{x} + d\V{x} x + d x
of a neighbouring point we can write:
x ⃗ + d x ⃗ = ( x 1 + d x 1 ) e ⃗ 1 + ( x 2 + d x 2 ) e ⃗ 2 + ( x 3 + d x 3 ) e ⃗ 3 \V{x} + d\V{x} \;=\;
(x_1 + dx_1) \V{e}_1 + (x_2 + dx_2) \V{e}_2 + (x_3 + dx_3) \V{e}_3 x + d x = ( x 1 + d x 1 ) e 1 + ( x 2 + d x 2 ) e 2 + ( x 3 + d x 3 ) e 3 and thus the vector d x ⃗ d\V{x} d x can be expressed as:
d x ⃗ = d x 1 e ⃗ 1 + d x 2 e ⃗ 2 + d x 3 e ⃗ 3 d\V{x} \;=\; dx_1 \V{e}_1 + dx_2 \V{e}_2 + dx_3 \V{e}_3 d x = d x 1 e 1 + d x 2 e 2 + d x 3 e 3 From the latter relation it is obvious that the changes d x 1 dx_1 d x 1 , d x 2 dx_2 d x 2
and d x 3 dx_3 d x 3 can be related to the vector d x ⃗ d\V{x} d x according to:
d x 1 = d x ⃗ ⋅ e ⃗ 1 d x 2 = d x ⃗ ⋅ e ⃗ 2 d x 3 = d x ⃗ ⋅ e ⃗ 3 \begin{aligned}
dx_1 \;&=\; d\V{x} \inp \V{e}_1 \\
dx_2 \;&=\; d\V{x} \inp \V{e}_2 \\
dx_3 \;&=\; d\V{x} \inp \V{e}_3
\end{aligned} d x 1 d x 2 d x 3 = d x ⋅ e 1 = d x ⋅ e 2 = d x ⋅ e 3 We could also express the function a ( x ⃗ ) a(\V{x}) a ( x ) in terms of the components r r r , θ \theta θ , z z z of the position vector x ⃗ \V{x} x with
respect to a cylindrical basis { e ⃗ r , e ⃗ t , e ⃗ z } \cylbasis { e r , e t , e z } . Then the position vector equals:
x ⃗ = r e ⃗ r ( θ ) + z e ⃗ z \V{x} \;=\; r \V{e}_r(\theta) + z \V{e}_z x = r e r ( θ ) + z e z Figure A.15: Components r r r , θ \theta θ , z z z of the position vector x ⃗ \V{x} x with respect to a
cylindrical basis { e ⃗ r , e ⃗ t , e ⃗ z } \cylbasis { e r , e t , e z } .
Within the cylindrical basis, the position x ⃗ + d x ⃗ \V{x} + d\V{x} x + d x of a
neighbouring point equals:
x ⃗ + d x ⃗ = ( r + d r ) e ⃗ r ( θ + d θ ) + ( z + d z ) e ⃗ z = ( r + d r ) { e ⃗ r ( θ ) + d e ⃗ r d θ d θ } + ( z + d z ) e ⃗ z = r e ⃗ r ( θ ) + z e ⃗ z + r e ⃗ t ( θ ) d θ + d r e ⃗ r ( θ ) + e ⃗ t ( θ ) d r d θ + d z e ⃗ z \begin{alignedat}{2}
\V{x} + d\V{x}
\;&=\; &&(r + dr) \V{e}_r(\theta + d\theta) + (z + dz) \V{e}_z \\
\;&=\; &&(r + dr) \{ \V{e}_r(\theta) + \tfrac{d\V{e}_r}{d\theta} d\theta \} +
(z + dz) \V{e}_z \\
\;&=\; &&r \V{e}_r(\theta) + z \V{e}_z + \\
& &&r \V{e}_t(\theta) d\theta +
dr \V{e}_r(\theta) + \V{e}_t(\theta) dr d\theta + dz \V{e}_z
\end{alignedat} x + d x = = = ( r + d r ) e r ( θ + d θ ) + ( z + d z ) e z ( r + d r ) { e r ( θ ) + d θ d e r d θ } + ( z + d z ) e z r e r ( θ ) + z e z + r e t ( θ ) d θ + d r e r ( θ ) + e t ( θ ) d r d θ + d z e z from which it can be concluded that, in a linear approximation, the
vector d x ⃗ d\V{x} d x equals:
d x ⃗ ≈ d r e ⃗ r ( θ ) + r d θ e ⃗ t ( θ ) + d z e ⃗ z d\V{x} \;\approx\; dr \V{e}_r(\theta) + r d\theta \V{e}_t(\theta) + dz
\V{e}_z d x ≈ d r e r ( θ ) + r d θ e t ( θ ) + d z e z The changes d r dr d r , d θ d\theta d θ and d z dz d z are related to the vector d x ⃗ d\V{x} d x
according to:
d r = d x ⃗ ⋅ e ⃗ r d θ = 1 r d x ⃗ ⋅ e ⃗ t d z = d x ⃗ ⋅ e ⃗ z \begin{aligned}
dr \;&=\; d\V{x} \inp \V{e}_r \\
d\theta \;&=\; \tfrac{1}{r} d\V{x} \inp \V{e}_t\\
dz \;&=\; d\V{x} \inp \V{e}_z
\end{aligned} d r d θ d z = d x ⋅ e r = r 1 d x ⋅ e t = d x ⋅ e z A.4.3 The gradient operator ¶ Considering a a a as a function of the position vector x ⃗ \V{x} x , we can investigate the
variation d a da d a due to a variation d x ⃗ d\V{x} d x :
d a = d x 1 ∂ a ∂ x 1 + d x 2 ∂ a ∂ x 2 + d x 3 ∂ a ∂ x 3 = ( d x ⃗ ⋅ e ⃗ 1 ) ∂ a ∂ x 1 + ( d x ⃗ ⋅ e ⃗ 2 ) ∂ a ∂ x 2 + ( d x ⃗ ⋅ e ⃗ 3 ) ∂ a ∂ x 3 = d x ⃗ ⋅ [ e ⃗ 1 ∂ a ∂ x 1 + e ⃗ 2 ∂ a ∂ x 2 + e ⃗ 3 ∂ a ∂ x 3 ] = d x ⃗ ⋅ ( ∇ ⃗ a ) \begin{aligned}
da \;&=\; dx_1 \parder{a}{x_1} + dx_2 \parder{a}{x_2} + dx_3 \parder{a}{x_3} \\
\;&=\; (d\V{x} \inp \V{e}_1) \parder{a}{x_1} + (d\V{x} \inp \V{e}_2) \parder{a}{x_2} +
(d\V{x} \inp \V{e}_3) \parder{a}{x_3} \\
\;&=\; d\V{x} \inp \left[ \V{e}_1 \parder{a}{x_1} + \V{e}_2 \parder{a}{x_2} +
\V{e}_3 \parder{a}{x_3} \right] \\
\;&=\; d\V{x} \inp (\grad a)
\end{aligned} d a = d x 1 ∂ x 1 ∂ a + d x 2 ∂ x 2 ∂ a + d x 3 ∂ x 3 ∂ a = ( d x ⋅ e 1 ) ∂ x 1 ∂ a + ( d x ⋅ e 2 ) ∂ x 2 ∂ a + ( d x ⋅ e 3 ) ∂ x 3 ∂ a = d x ⋅ [ e 1 ∂ x 1 ∂ a + e 2 ∂ x 2 ∂ a + e 3 ∂ x 3 ∂ a ] = d x ⋅ ( ∇ a ) The symbol ∇ ⃗ \grad ∇ is called the gradient operator [23] :
∇ ⃗ = [ e ⃗ 1 ∂ ∂ x 1 + e ⃗ 2 ∂ ∂ x 2 + e ⃗ 3 ∂ ∂ x 3 ] = e ⃗ ∼ T ∇ ∼ \begin{aligned}
\grad \;&=\; \left[ \V{e}_1 \parder{}{x_1} + \V{e}_2 \parder{}{x_2} +
\V{e}_3 \parder{}{x_3} \right] \\
\;&=\; \C{\V{e}}^T \C{\nabla}
\end{aligned} ∇ = [ e 1 ∂ x 1 ∂ + e 2 ∂ x 2 ∂ + e 3 ∂ x 3 ∂ ] = ∼ e T ∼ ∇ and
the expression ∇ ⃗ a \grad a ∇ a is called the gradient of a a a .
The gradient of a vector function a ⃗ \V{a} a is obtained similarly:
d a ⃗ = d x 1 ∂ a ⃗ ∂ x 1 + d x 2 ∂ a ⃗ ∂ x 2 + d x 3 ∂ a ⃗ ∂ x 3 = ( d x ⃗ ⋅ e ⃗ 1 ) ∂ a ⃗ ∂ x 1 + ( d x ⃗ ⋅ e ⃗ 2 ) ∂ a ⃗ ∂ x 2 + ( d x ⃗ ⋅ e ⃗ 3 ) ∂ a ⃗ ∂ x 3 = d x ⃗ ⋅ [ e ⃗ 1 ∂ a ⃗ ∂ x 1 + e ⃗ 2 ∂ a ⃗ ∂ x 2 + e ⃗ 3 ∂ a ⃗ ∂ x 3 ] = d x ⃗ ⋅ ( ∇ ⃗ a ⃗ ) \begin{aligned}
d\V{a} \;&=\; dx_1 \parder{\V{a}}{x_1} + dx_2 \parder{\V{a}}{x_2} + dx_3 \parder{\V{a}}{x_3} \\
\;&=\; (d\V{x} \inp \V{e}_1) \parder{\V{a}}{x_1} +
(d\V{x} \inp \V{e}_2) \parder{\V{a}}{x_2} +
(d\V{x} \inp \V{e}_3) \parder{\V{a}}{x_3} \\
\;&=\; d\V{x} \inp \left[ \V{e}_1 \parder{\V{a}}{x_1} + \V{e}_2 \parder{\V{a}}{x_2} +
\V{e}_3 \parder{\V{a}}{x_3} \right] \\
\;&=\; d\V{x} \inp (\grad \V{a})
\end{aligned} d a = d x 1 ∂ x 1 ∂ a + d x 2 ∂ x 2 ∂ a + d x 3 ∂ x 3 ∂ a = ( d x ⋅ e 1 ) ∂ x 1 ∂ a + ( d x ⋅ e 2 ) ∂ x 2 ∂ a + ( d x ⋅ e 3 ) ∂ x 3 ∂ a = d x ⋅ [ e 1 ∂ x 1 ∂ a + e 2 ∂ x 2 ∂ a + e 3 ∂ x 3 ∂ a ] = d x ⋅ ( ∇ a ) or in index notation
d a j = d x i a j , i da_j \;=\; dx_i a_{j,i} d a j = d x i a j , i For the special case a ⃗ = x ⃗ \V{a} = \V{x} a = x we find:
∇ ⃗ x ⃗ = I \grad \V{x} \;=\; \T{I} ∇ x = I The gradient operator ∇ ⃗ \grad ∇ can be applied to a vector a ⃗ \V{a} a in several manners, the
result of which is called the gradient of a ⃗ \V{a} a (grad a ⃗ \V{a} a ),
the divergence [24] of a ⃗ \V{a} a (div a ⃗ \V{a} a ), or the
rotation [25] or curl of a ⃗ \V{a} a (rot a ⃗ \V{a} a ):
g r a d a ⃗ = ∇ ⃗ a ⃗ = e ⃗ 1 ∂ a ⃗ ∂ x 1 + e ⃗ 2 ∂ a ⃗ ∂ x 2 + e ⃗ 3 ∂ a ⃗ ∂ x 3 , d i v a ⃗ = ∇ ⃗ ⋅ a ⃗ = e ⃗ 1 ⋅ ∂ a ⃗ ∂ x 1 + e ⃗ 2 ⋅ ∂ a ⃗ ∂ x 2 + e ⃗ 3 ⋅ ∂ a ⃗ ∂ x 3 , r o t a ⃗ = ∇ ⃗ × a ⃗ = e ⃗ 1 × ∂ a ⃗ ∂ x 1 + e ⃗ 2 × ∂ a ⃗ ∂ x 2 + e ⃗ 3 × ∂ a ⃗ ∂ x 3 \begin{aligned}
{\rm grad\ }\V{a} \;&=\; \grad \V{a}
= \V{e}_1 \parder{\V{a}}{x_1} + \V{e}_2 \parder{\V{a}}{x_2} +
\V{e}_3 \parder{\V{a}}{x_3} ,\\
{\rm div\ }\V{a} \;&=\; \grad \inp \V{a}
= \V{e}_1 \inp \parder{\V{a}}{x_1} + \V{e}_2 \inp \parder{\V{a}}{x_2} +
\V{e}_3 \inp \parder{\V{a}}{x_3} ,\\
{\rm rot\ }\V{a} \;&=\; \grad \cross \V{a}
= \V{e}_1 \cross \parder{\V{a}}{x_1} + \V{e}_2 \cross \parder{\V{a}}{x_2} +
\V{e}_3 \cross \parder{\V{a}}{x_3}
\end{aligned} grad a div a rot a = ∇ a = e 1 ∂ x 1 ∂ a + e 2 ∂ x 2 ∂ a + e 3 ∂ x 3 ∂ a , = ∇ ⋅ a = e 1 ⋅ ∂ x 1 ∂ a + e 2 ⋅ ∂ x 2 ∂ a + e 3 ⋅ ∂ x 3 ∂ a , = ∇ × a = e 1 × ∂ x 1 ∂ a + e 2 × ∂ x 2 ∂ a + e 3 × ∂ x 3 ∂ a Note that div a ⃗ \V{a} a yields a scalar, rot a ⃗ \V{a} a yields a vector, and
grad a ⃗ \V{a} a yields a second order tensor. Applied to tensors in general, the gradient
increases the order by 1, the divergence diminishes the order by 1, while the order
remains unaffected by the curl.
The expression for the gradient operator in cylindrical coordinates can be found
following a similar derivation as in the case of a Cartesian coordinate
system:
d a = d r ∂ a ∂ r + d θ ∂ a ∂ θ + d z ∂ a ∂ z = ( d x ⃗ ⋅ e ⃗ r ) ∂ a ∂ r + ( 1 r d x ⃗ ⋅ e ⃗ t ) ∂ a ∂ θ + ( d x ⃗ ⋅ e ⃗ z ) ∂ a ∂ z = d x ⃗ ⋅ [ e ⃗ r ∂ a ∂ r + 1 r e ⃗ t ∂ a ∂ θ + e ⃗ z ∂ a ∂ z ] = d x ⃗ ⋅ ( ∇ ⃗ a ) \begin{aligned}
da \;&=\; dr \parder{a}{r} + d\theta \parder{a}{\theta} + dz \parder{a}{z} \\
\;&=\; (d\V{x} \inp \V{e}_r) \parder{a}{r} +
(\tfrac{1}{r} d\V{x} \inp \V{e}_t) \parder{a}{\theta} +
(d\V{x} \inp \V{e}_z) \parder{a}{z} \\
\;&=\; d\V{x} \inp \left[ \V{e}_r \parder{a}{r} +
\tfrac{1}{r} \V{e}_t \parder{a}{\theta} + \V{e}_z \parder{a}{z} \right] \\
\;&=\; d\V{x} \inp (\grad a)
\end{aligned} d a = d r ∂ r ∂ a + d θ ∂ θ ∂ a + d z ∂ z ∂ a = ( d x ⋅ e r ) ∂ r ∂ a + ( r 1 d x ⋅ e t ) ∂ θ ∂ a + ( d x ⋅ e z ) ∂ z ∂ a = d x ⋅ [ e r ∂ r ∂ a + r 1 e t ∂ θ ∂ a + e z ∂ z ∂ a ] = d x ⋅ ( ∇ a ) Thus the expression for the gradient operator
in a cylindrical coordinate system equals:
∇ ⃗ = e ⃗ r ∂ ∂ r + e ⃗ t 1 r ∂ ∂ θ + e ⃗ z ∂ ∂ z \grad \;=\;
\V{e}_r \parder{}{r} + \V{e}_t \frac{1}{r} \parder{}{\theta} + \V{e}_z \parder{}{z} ∇ = e r ∂ r ∂ + e t r 1 ∂ θ ∂ + e z ∂ z ∂ The following relations on differentiable scalar functions ϕ \phi ϕ , vectors a ⃗ , b ⃗ \V{a},\V{b} a , b , tensors A , B , C \T{A},\T{B},\T{C} A , B , C , inner/outer products and their derivatives can be proven:
A : ( B ⋅ C ) = ( A ⋅ B ) : C ∇ ⃗ ( ϕ a ⃗ ) = ( ∇ ⃗ ϕ ) a ⃗ + ϕ ∇ ⃗ a ⃗ ∇ ⃗ ⋅ ( ϕ a ⃗ ) = ( ∇ ⃗ ϕ ) ⋅ a ⃗ + ϕ ∇ ⃗ ⋅ a ⃗ ∇ ⃗ ( a ⃗ ⋅ b ⃗ ) = ( ∇ ⃗ a ⃗ ) ⋅ b ⃗ + ( ∇ ⃗ b ⃗ ) ⋅ a ⃗ ∇ ⃗ ⋅ ( a ⃗ b ⃗ ) = ( ∇ ⃗ ⋅ a ⃗ ) b ⃗ + a ⃗ ⋅ ∇ ⃗ b ⃗ ∇ ⃗ ⋅ ( ϕ A ) = ( ∇ ⃗ ϕ ) ⋅ A + ϕ ∇ ⃗ ⋅ A ∇ ⃗ ⋅ ( A ⋅ a ⃗ ) = ( ∇ ⃗ ⋅ A ) ⋅ a ⃗ + A : ( ∇ ⃗ a ⃗ ) T ∇ ⃗ ⋅ a ⃗ = ( ∇ ⃗ a ⃗ ) : I = tr ( ∇ ⃗ a ⃗ ) \begin{aligned}
\T{A} \dinp (\T{B}\inp\T{C}) \;&=\; (\T{A}\inp\T{B}) \dinp \T{C}\\
\grad(\phi\V{a}) \;&=\; (\grad\phi)\V{a} + \phi\grad\V{a}\\
\grad \inp (\phi \V{a}) \;&=\; (\grad\phi) \inp \V{a} + \phi \grad \inp \V{a}\\
\grad(\V{a}\inp\V{b}) \;&=\; (\grad\V{a})\inp\V{b} + (\grad\V{b})\inp\V{a}\\
\grad \inp (\V{a}\V{b}) \;&=\; (\grad \inp \V{a}) \V{b} + \V{a} \inp \grad\V{b}\\
\grad \inp (\phi \T{A}) \;&=\; (\grad\phi) \inp \T{A} + \phi \grad \inp \T{A}\\
\grad \inp (\T{A} \inp \V{a}) \;&=\; (\grad \inp \T{A}) \inp \V{a} + \T{A} :(\grad\V{a})^T\\
\grad \inp \V{a} \;&=\; (\grad\V{a}) \dinp \T{I} = \tr(\grad\V{a})
\end{aligned} A : ( B ⋅ C ) ∇ ( ϕ a ) ∇ ⋅ ( ϕ a ) ∇ ( a ⋅ b ) ∇ ⋅ ( a b ) ∇ ⋅ ( ϕ A ) ∇ ⋅ ( A ⋅ a ) ∇ ⋅ a = ( A ⋅ B ) : C = ( ∇ ϕ ) a + ϕ ∇ a = ( ∇ ϕ ) ⋅ a + ϕ ∇ ⋅ a = ( ∇ a ) ⋅ b + ( ∇ b ) ⋅ a = ( ∇ ⋅ a ) b + a ⋅ ∇ b = ( ∇ ϕ ) ⋅ A + ϕ ∇ ⋅ A = ( ∇ ⋅ A ) ⋅ a + A : ( ∇ a ) T = ( ∇ a ) : I = tr ( ∇ a ) A.6 Gauss’ divergence theorem ¶ Gauss’ divergence theorem relates volume integrals and surface integrals.
Let’s consider a closed volume V V V with and external closed surface A A A , which has an outward normal n ⃗ \vec{n} n in each point on that surface.
Let a ⃗ \vec{a} a be a continuous vector field that is defined in the entire volume V V V . The divergence theorem then states that the volume integral over V V V of the divergence of this vector field p ⃗ \vec{p} p equals the surface integral on A A A of the normal projection of this vector field p ⃗ \vec{p} p on the external surface.
∫ ∫ ∫ V ∇ ⃗ ⋅ p ⃗ d V = ∫ ∫ A n ⃗ ⋅ p ⃗ d A = ∫ ∫ A p ⃗ ⋅ n ⃗ d A \int\int\int_V \: \grad \inp \vec{p} \: dV \;=\; \int\int_A \: \vec{n} \inp \vec{p} \: dA \;=\; \int\int_A \: \vec{p}\inp\vec{n} \: dA ∫∫ ∫ V ∇ ⋅ p d V = ∫ ∫ A n ⋅ p d A = ∫ ∫ A p ⋅ n d A The divergence theorem is often used in deriving balance equations in continua.
Using the divergence theorem, it is often possible to convert volume integrals into surface integrals, if a vector field can be found of which the divergence equals the integrand in the volume integral.
The generalised form of Gauss’ divergence theorem applies to a tensor field P \T{P} P , for which an equal results hold (even though the integrand in the surface integral is not longer a scalar):
∫ ∫ ∫ V ∇ ⃗ ⋅ P d V = ∫ ∫ A n ⃗ ⋅ P d A \int\int\int_V \: \grad \inp \T{P} \: dV \;=\; \int\int_A \: \vec{n} \inp \T{P} \: dA ∫∫ ∫ V ∇ ⋅ P d V = ∫ ∫ A n ⋅ P d A A.7 Higher-order and fourth-order tensors ¶ A.7.1 Definition ¶ Some problems invoke the transformation of tensors. Such transformations are carried out
by means of higher-order tensors. A general definition of a tensor could be: an
invariant object with an arbitrary number of indices . The number of indices is the
order (or rank) of the tensor. The transformation which is most relevant in the
mechanics of materials is the transformation of a second-order tensor into another
second-order tensor by means of a fourth-order tensor.
Figure A.16: A fourth-order tensor 4 C \TQ{C} 4 C that maps a (linear) second-order tensor A \T{A} A
onto a second-order tensor B \T{B} B .
An arbitrary tensor A \T{A} A (which is a linear transformation of vectors) is mapped onto a
different tensor B \T{B} B (which is another linear transformation of vectors) by means of the
double inner product with a fourth-order tensor 4 C \TQ{C} 4 C , see Figure A.16 .
B = 4 C : A \T{B} \;=\; \TQ{C} \dinp \T{A} B = 4 C : A Using index tensor notations, the tensor A l k A_{lk} A l k transforms to B i j B_{ij} B ij according to
B i j = C i j k l A l k B_{ij} \;=\; C_{ijkl}\,A_{lk} B ij = C ijk l A l k The tensor C i j k l C_{ijkl} C ijk l which was used to perform this transformation has 4 indices.
A.7.2 Properties ¶ Since a fourth-order tensor is built on quadrades rather than dyades, some new calculus
rules apply. Each fourth-order tensor can be written as a finite sum of quadrades. With
respect to a two-dimensional Cartesian basis, a tensor 4 C \TQ{C} 4 C would be given by s i x t e e n sixteen s i x t ee n
terms, i.e.
4 C = C 1111 e ⃗ 1 e ⃗ 1 e ⃗ 1 e ⃗ 1 + C 1112 e ⃗ 1 e ⃗ 1 e ⃗ 1 e ⃗ 2 + C 1121 e ⃗ 1 e ⃗ 1 e ⃗ 2 e ⃗ 1 + C 1122 e ⃗ 1 e ⃗ 1 e ⃗ 2 e ⃗ 2 C 1211 e ⃗ 1 e ⃗ 2 e ⃗ 1 e ⃗ 1 + C 1212 e ⃗ 1 e ⃗ 2 e ⃗ 1 e ⃗ 2 + C 1221 e ⃗ 1 e ⃗ 2 e ⃗ 2 e ⃗ 1 + C 1222 e ⃗ 1 e ⃗ 2 e ⃗ 2 e ⃗ 2 C 2111 e ⃗ 2 e ⃗ 1 e ⃗ 1 e ⃗ 1 + C 2112 e ⃗ 2 e ⃗ 1 e ⃗ 1 e ⃗ 2 + C 2121 e ⃗ 2 e ⃗ 1 e ⃗ 2 e ⃗ 1 + C 2122 e ⃗ 2 e ⃗ 1 e ⃗ 2 e ⃗ 2 C 2211 e ⃗ 2 e ⃗ 2 e ⃗ 1 e ⃗ 1 + C 2212 e ⃗ 2 e ⃗ 2 e ⃗ 1 e ⃗ 2 + C 2221 e ⃗ 2 e ⃗ 2 e ⃗ 2 e ⃗ 1 + C 2222 e ⃗ 2 e ⃗ 2 e ⃗ 2 e ⃗ 2 \begin{split}
\TQ{C} \;=\; & C_{1111}\V{e}_1\V{e}_1\V{e}_1\V{e}_1 +
C_{1112}\V{e}_1\V{e}_1\V{e}_1\V{e}_2 + C_{1121}\V{e}_1\V{e}_1\V{e}_2\V{e}_1 + C_{1122}\V{e}_1\V{e}_1\V{e}_2\V{e}_2\\
& C_{1211}\V{e}_1\V{e}_2\V{e}_1\V{e}_1 +
C_{1212}\V{e}_1\V{e}_2\V{e}_1\V{e}_2 + C_{1221}\V{e}_1\V{e}_2\V{e}_2\V{e}_1 +
C_{1222}\V{e}_1\V{e}_2\V{e}_2\V{e}_2\\
& C_{2111}\V{e}_2\V{e}_1\V{e}_1\V{e}_1 +
C_{2112}\V{e}_2\V{e}_1\V{e}_1\V{e}_2 + C_{2121}\V{e}_2\V{e}_1\V{e}_2\V{e}_1 +
C_{2122}\V{e}_2\V{e}_1\V{e}_2\V{e}_2\\
& C_{2211}\V{e}_2\V{e}_2\V{e}_1\V{e}_1 +
C_{2212}\V{e}_2\V{e}_2\V{e}_1\V{e}_2 + C_{2221}\V{e}_2\V{e}_2\V{e}_2\V{e}_1 + C_{2222}\V{e}_2\V{e}_2\V{e}_2\V{e}_2
\end{split} 4 C = C 1111 e 1 e 1 e 1 e 1 + C 1112 e 1 e 1 e 1 e 2 + C 1121 e 1 e 1 e 2 e 1 + C 1122 e 1 e 1 e 2 e 2 C 1211 e 1 e 2 e 1 e 1 + C 1212 e 1 e 2 e 1 e 2 + C 1221 e 1 e 2 e 2 e 1 + C 1222 e 1 e 2 e 2 e 2 C 2111 e 2 e 1 e 1 e 1 + C 2112 e 2 e 1 e 1 e 2 + C 2121 e 2 e 1 e 2 e 1 + C 2122 e 2 e 1 e 2 e 2 C 2211 e 2 e 2 e 1 e 1 + C 2212 e 2 e 2 e 1 e 2 + C 2221 e 2 e 2 e 2 e 1 + C 2222 e 2 e 2 e 2 e 2 In a three-dimensional space a tensor 4 C \TQ{C} 4 C has 3 × 3 × 3 × 3 = 81 3 \times\ 3 \times 3 \times 3 = 81 3 × 3 × 3 × 3 = 81
components. The correct full matrix representation of a higher-order tensor can only be
achieved with multi-dimensional matrices (which exist in modern computing
languages). A fourth-order 3D tensor is then represented by a
[ 3 × 3 × 3 × 3 ] [3 \times 3 \times 3 \times 3] [ 3 × 3 × 3 × 3 ] matrix.
Different types of transposed tensors are defined: the total transpose 4 C T \TQ{C}^{T} 4 C T , the
left transpose 4 C L T \TQ{C}^{LT} 4 C L T or the right transpose 4 C R T \TQ{C}^{RT} 4 C RT . If the tensor 4 C \TQ{C} 4 C
is denoted C i j k l C_{ijkl} C ijk l in index notation, each of these transposes is given by
4 C T ⇔ C l k j i 4 C L T ⇔ C j i k l 4 C R T ⇔ C i j l k \begin{aligned}
\TQ{C}^{T} \;&\Leftrightarrow\; C_{lkji} \\
\TQ{C}^{LT} \;&\Leftrightarrow\; C_{jikl} \\
\TQ{C}^{RT} \;&\Leftrightarrow\; C_{ijlk}
\end{aligned} 4 C T 4 C L T 4 C RT ⇔ C l kji ⇔ C jik l ⇔ C ij l k Different types of minor symmetries can be defined for a fourth-order tensor.
A left symmetric fourth-order tensor, is a tensor for which
4 C = 4 C L T ⟹ C i j k l = C j i k l \TQ{C} \;=\;\TQ{C}^{LT} \quad\Longrightarrow\quad C_{ijkl}\;=\;C_{jikl} 4 C = 4 C L T ⟹ C ijk l = C jik l In a 3D space, it has 81 − 1 × 3 × 3 × 3 = 54 81 - 1 \times 3 \times 3 \times 3 = 54 81 − 1 × 3 × 3 × 3 = 54 distinct components.
A right symmetric fourth-order tensor is given by
4 C = 4 C R T ⟹ C i j k l = C i j l k \TQ{C} \;=\;\TQ{C}^{RT} \quad\Longrightarrow\quad C_{ijkl}\;=\;C_{ijlk} 4 C = 4 C RT ⟹ C ijk l = C ij l k In a 3D space, it has 81 − 3 × 3 × 3 × 1 = 54 81 - 3 \times 3 \times 3 \times 1 = 54 81 − 3 × 3 × 3 × 1 = 54 distinct components. A tensor
which is left and right symmetric, has only 54 − 1 × 3 × 3 × 2 = 36 54 - 1 \times 3 \times 3 \times 2 = 36 54 − 1 × 3 × 3 × 2 = 36 distinct
components. A middle symmetric fourth-order tensor complies with
4 C = 4 C T ⟹ C i j k l = C l k j i \TQ{C} \;=\;\TQ{C}^{T} \quad\Longrightarrow\quad C_{ijkl}\;=\;C_{lkji} 4 C = 4 C T ⟹ C ijk l = C l kji In a 3D space, it has 81 − 2 × 3 × 3 × 2 = 45 81 - 2 \times 3 \times 3 \times 2 = 45 81 − 2 × 3 × 3 × 2 = 45
distinct components.
A total symmetric fourth-order tensor equals is left, right and
central symmetric, i.e.
4 C = 4 C L T = 4 C R T = 4 C T \TQ{C} \;=\; \TQ{C}^{LT} \;=\; \TQ{C}^{RT} \;=\; \TQ{C}^{T} 4 C = 4 C L T = 4 C RT = 4 C T In a 3D space, it has 36 − 1 2 6 × 5 = 21 36 - \half 6 \times 5 = 21 36 − 2 1 6 × 5 = 21
distinct components.
The fourth-order null tensor 4 0 \TQ{0} 4 0 is defined by
4 0 : A = 0 \TQ{0}\dinp\T{A} \;=\; \T{0} 4 0 : A = 0 The fourth-order unit tensor 4 I \TQ{I} 4 I maps a second-order tensor A \T{A} A on itself
4 I : A = A \TQ{I}\dinp\T{A} \;=\; \T{A} 4 I : A = A This tensor is given in index notation by
4 I ⟹ I i j k l = δ i l δ j k \TQ{I} \;\Longrightarrow\; I_{ijkl} \;=\; \delta_{il}\delta_{jk} 4 I ⟹ I ijk l = δ i l δ jk or with respect to a 3D Cartesian basis
4 I = e ⃗ 1 e ⃗ 1 e ⃗ 1 e ⃗ 1 + e ⃗ 1 e ⃗ 2 e ⃗ 2 e ⃗ 1 + e ⃗ 1 e ⃗ 3 e ⃗ 3 e ⃗ 1 e ⃗ 2 e ⃗ 1 e ⃗ 1 e ⃗ 2 + e ⃗ 2 e ⃗ 2 e ⃗ 2 e ⃗ 2 + e ⃗ 2 e ⃗ 3 e ⃗ 3 e ⃗ 2 e ⃗ 3 e ⃗ 1 e ⃗ 1 e ⃗ 3 + e ⃗ 3 e ⃗ 2 e ⃗ 2 e ⃗ 3 + e ⃗ 3 e ⃗ 3 e ⃗ 3 e ⃗ 3 \begin{split}
\TQ{I} \;=\; &\V{e}_1\V{e}_1\V{e}_1\V{e}_1 + \V{e}_1\V{e}_2\V{e}_2\V{e}_1 +
\V{e}_1\V{e}_3\V{e}_3\V{e}_1 \\
&\V{e}_2\V{e}_1\V{e}_1\V{e}_2 + \V{e}_2\V{e}_2\V{e}_2\V{e}_2 +
\V{e}_2\V{e}_3\V{e}_3\V{e}_2 \\
&\V{e}_3\V{e}_1\V{e}_1\V{e}_3 + \V{e}_3\V{e}_2\V{e}_2\V{e}_3 +
\V{e}_3\V{e}_3\V{e}_3\V{e}_3
\end{split} 4 I = e 1 e 1 e 1 e 1 + e 1 e 2 e 2 e 1 + e 1 e 3 e 3 e 1 e 2 e 1 e 1 e 2 + e 2 e 2 e 2 e 2 + e 2 e 3 e 3 e 2 e 3 e 1 e 1 e 3 + e 3 e 2 e 2 e 3 + e 3 e 3 e 3 e 3 The symmetric fourth-order unit tensor 4 I s \TQ{I}^s 4 I s maps a second-order tensor A \T{A} A on the
symmetric part of A \T{A} A , denoted A s \T{A}^s A s :
4 I s : A = A s = 1 2 ( A + A T ) \TQ{I}^s\dinp\T{A} \;=\; \T{A}^s \;=\; \tfrac{1}{2}(\T{A} + \T{A}^T) 4 I s : A = A s = 2 1 ( A + A T ) This tensor is given in index notation by
4 I s ⇔ I i j k l s = 1 2 ( δ i l δ j k + δ i k δ j l ) \TQ{I}^s \;\Leftrightarrow\; I_{ijkl}^s \;=\; \tfrac{1}{2}\left(\delta_{il}\delta_{jk} + \delta_{ik}\delta_{jl}\right) 4 I s ⇔ I ijk l s = 2 1 ( δ i l δ jk + δ ik δ j l ) This tensor is a total symmetric tensor, i.e. left symmetric, right symmetric and central symmetric.
Note that this tensor is also given by
4 I s = 1 2 ( 4 I + 4 I R T ) \TQ{I}^s \;=\; \tfrac{1}{2}(\TQ{I}+\TQ{I}^{RT}) 4 I s = 2 1 ( 4 I + 4 I RT ) or with respect to a Cartesian basis by
4 I s = e ⃗ 1 e ⃗ 1 e ⃗ 1 e ⃗ 1 + 1 2 e ⃗ 1 e ⃗ 2 e ⃗ 2 e ⃗ 1 + 1 2 e ⃗ 1 e ⃗ 2 e ⃗ 1 e ⃗ 2 + 1 2 e ⃗ 1 e ⃗ 3 e ⃗ 3 e ⃗ 1 + 1 2 e ⃗ 1 e ⃗ 3 e ⃗ 1 e ⃗ 3 1 2 e ⃗ 2 e ⃗ 1 e ⃗ 1 e ⃗ 2 + 1 2 e ⃗ 2 e ⃗ 1 e ⃗ 2 e ⃗ 1 + e ⃗ 2 e ⃗ 2 e ⃗ 2 e ⃗ 2 + 1 2 e ⃗ 2 e ⃗ 3 e ⃗ 3 e ⃗ 2 + 1 2 e ⃗ 2 e ⃗ 3 e ⃗ 2 e ⃗ 3 1 2 e ⃗ 3 e ⃗ 1 e ⃗ 1 e ⃗ 3 + 1 2 e ⃗ 3 e ⃗ 1 e ⃗ 3 e ⃗ 1 + 1 2 e ⃗ 3 e ⃗ 2 e ⃗ 2 e ⃗ 3 + 1 2 e ⃗ 3 e ⃗ 2 e ⃗ 3 e ⃗ 2 + e ⃗ 3 e ⃗ 3 e ⃗ 3 e ⃗ 3 \begin{split}
\TQ{I}^s \;=\; &\V{e}_1\V{e}_1\V{e}_1\V{e}_1 + \tfrac{1}{2}\V{e}_1\V{e}_2\V{e}_2\V{e}_1 +
\tfrac{1}{2}\V{e}_1\V{e}_2\V{e}_1\V{e}_2 + \tfrac{1}{2}\V{e}_1\V{e}_3\V{e}_3\V{e}_1
+ \tfrac{1}{2}\V{e}_1\V{e}_3\V{e}_1\V{e}_3 \\
& \tfrac{1}{2}\V{e}_2\V{e}_1\V{e}_1\V{e}_2 + \tfrac{1}{2}\V{e}_2\V{e}_1\V{e}_2\V{e}_1 +
\V{e}_2\V{e}_2\V{e}_2\V{e}_2 + \tfrac{1}{2}\V{e}_2\V{e}_3\V{e}_3\V{e}_2 +
\tfrac{1}{2}\V{e}_2\V{e}_3\V{e}_2\V{e}_3 \\
& \tfrac{1}{2}\V{e}_3\V{e}_1\V{e}_1\V{e}_3 + \tfrac{1}{2}\V{e}_3\V{e}_1\V{e}_3\V{e}_1 +
\tfrac{1}{2}\V{e}_3\V{e}_2\V{e}_2\V{e}_3 + \tfrac{1}{2}\V{e}_3\V{e}_2\V{e}_3\V{e}_2 +
\V{e}_3\V{e}_3\V{e}_3\V{e}_3
\end{split} 4 I s = e 1 e 1 e 1 e 1 + 2 1 e 1 e 2 e 2 e 1 + 2 1 e 1 e 2 e 1 e 2 + 2 1 e 1 e 3 e 3 e 1 + 2 1 e 1 e 3 e 1 e 3 2 1 e 2 e 1 e 1 e 2 + 2 1 e 2 e 1 e 2 e 1 + e 2 e 2 e 2 e 2 + 2 1 e 2 e 3 e 3 e 2 + 2 1 e 2 e 3 e 2 e 3 2 1 e 3 e 1 e 1 e 3 + 2 1 e 3 e 1 e 3 e 1 + 2 1 e 3 e 2 e 2 e 3 + 2 1 e 3 e 2 e 3 e 2 + e 3 e 3 e 3 e 3 Fourth-order tensors can be partially modified through inner products with second-order
tensors or double inner products with other fourth-order tensors. The inner product
between a fourth-order tensor 4 A \TQ{A} 4 A and a second-order tensor B \T{B} B yields a
fourth-order tensor given by
4 C = 4 A ⋅ B C i j k l = A i j k m B m l \begin{aligned}
\TQ{C} \;&=\; \TQ{A} \inp \T{B} \\
C_{ijkl} \;&=\; A_{ijkm}B_{ml}
\end{aligned} 4 C C ijk l = 4 A ⋅ B = A ijkm B m l The double inner product between a fourth-order tensor 4 A \TQ{A} 4 A and another fourth-order
tensor 4 B \TQ{B} 4 B again leads to a fourth-order tensor 4 C \TQ{C} 4 C according to
4 C = 4 A : 4 B C i j k l = A i j m n B n m k l \begin{aligned}
\TQ{C} \;&=\; \TQ{A}\dinp\TQ{B} \\
C_{ijkl} \;&=\; A_{ijmn}B_{nmkl}
\end{aligned} 4 C C ijk l = 4 A : 4 B = A ijmn B nmk l Note that, in general, the double inner product used in combination with fourth-order tensors is no
longer commutative
4 A : B ≠ B : 4 A 4 A : 4 B ≠ 4 B : 4 A \begin{aligned}
\TQ{A}\dinp\T{B} \;&\neq\; \T{B}\dinp\TQ{A}\\
\TQ{A}\dinp\TQ{B} \;&\neq\; \TQ{B}\dinp\TQ{A}
\end{aligned} 4 A : B 4 A : 4 B = B : 4 A = 4 B : 4 A A.7.3 Tensor rules ¶ 4 A : ( B ⋅ C ) = ( 4 A ⋅ B ) : C A ⋅ B + B T ⋅ A T = 4 I s : ( A ⋅ B ) = ( 4 I s ⋅ A ) : B \begin{aligned}
\TQ{A}\dinp(\T{B}\inp\T{C}) \;&=\; (\TQ{A}\inp\T{B})\dinp\T{C} \\
\T{A}\inp\T{B} + \T{B}^T\inp\T{A}^T \;&=\; \TQ{I}^s \dinp (\T{A}\inp\T{B}) \\
\;&=\; (\TQ{I}^s \inp \T{A})\dinp\T{B}
\end{aligned} 4 A : ( B ⋅ C ) A ⋅ B + B T ⋅ A T = ( 4 A ⋅ B ) : C = 4 I s : ( A ⋅ B ) = ( 4 I s ⋅ A ) : B A.7.4 Matrix condensation of the double inner product with a second-order tensor ¶ In many numerical implementations, tensor products are condensed in a two-dimensional
matrix format once a Cartesian basis has been chosen. Making use of special properties of
the tensors involved then permits to omit a considerable amount of computations for a
double inner product. Components of a second-order tensor B \T{B} B are normally represented
as a matrix
B ‾ = [ B 11 B 12 B 13 B 21 B 22 B 32 B 31 B 32 B 33 ] \M{B} \;=\; \begin{bmatrix} B_{11} & B_{12} & B_{13} \\
B_{21} & B_{22} & B_{32} \\
B_{31} & B_{32} & B_{33}
\end{bmatrix} B = ⎣ ⎡ B 11 B 21 B 31 B 12 B 22 B 32 B 13 B 32 B 33 ⎦ ⎤ For the computation of a double inner product with a fourth-order tensor, it is often more
convenient to store the 9 components in a column B ∼ \C{B} ∼ B Taking into account the
symmetry of a second-order tensor B \T{B} B permits to store the 6 distinct components in
a column rather than in a matrix, e.g.,
B ∼ = [ B 11 B 12 B 13 B 21 B 22 B 23 B 31 B 32 B 33 ] \C{B} \;=\; \begin{bmatrix}
B_{11} \\ B_{12} \\ B_{13} \\ B_{21} \\ B_{22} \\ B_{23} \\ B_{31} \\ B_{32} \\ B_{33}
\end{bmatrix} ∼ B = ⎣ ⎡ B 11 B 12 B 13 B 21 B 22 B 23 B 31 B 32 B 33 ⎦ ⎤ On the basis of this notation, it is possible to obtain the components of second-order
tensor C \T{C} C as a similarly structured column, which is the double inner product between
a fourth-order tensor 4 A \TQ{A} 4 A and a second-order tensor B \T{B} B , as a
matrix-column product, i.e. the components of
C = 4 A : B \T{C} \;=\; \TQ{A} \dinp \T{B} C = 4 A : B are obtained through
C ∼ = A ‾ ‾ B ∼ [ C 11 C 12 C 13 C 21 C 22 C 23 C 31 C 32 C 33 ] = [ A 1111 A 1121 A 1131 A 1112 A 1122 A 1132 A 1113 A 1123 A 1133 A 1211 A 1221 A 1231 A 1212 A 1222 A 1232 A 1213 A 1223 A 1233 A 1311 A 1321 A 1331 A 1312 A 1322 A 1332 A 1313 A 1323 A 1333 A 2111 A 2121 A 2131 A 2112 A 2122 A 2132 A 2113 A 2123 A 2133 A 2211 A 2221 A 2231 A 2212 A 2222 A 2232 A 2213 A 2223 A 2233 A 2311 A 2321 A 2331 A 2312 A 2322 A 2332 A 2313 A 2323 A 2333 A 3111 A 3121 A 3131 A 3112 A 3122 A 3132 A 3113 A 3123 A 3133 A 3211 A 3221 A 3231 A 3212 A 3222 A 3232 A 3213 A 3223 A 3233 A 3311 A 3321 A 3331 A 3312 A 3322 A 3332 A 3313 A 3323 A 3333 ] [ B 11 B 12 B 13 B 21 B 22 B 23 B 31 B 32 B 33 ] \begin{aligned}
\C{C} \;&=\; \MQ{A}\, \C{B} \\
\left[\begin{smallmatrix}
C_{11} \\ C_{12} \\ C_{13} \\ C_{21} \\ C_{22} \\ C_{23} \\ C_{31} \\ C_{32} \\ C_{33}
\end{smallmatrix} \right]
\;&=\; \left[\begin{smallmatrix}
A_{1111} & A_{1121} & A_{1131} & A_{1112} & A_{1122} & A_{1132} & A_{1113} &
A_{1123} & A_{1133} \\
A_{1211} & A_{1221} & A_{1231} & A_{1212} & A_{1222} & A_{1232} & A_{1213} &
A_{1223} & A_{1233} \\
A_{1311} & A_{1321} & A_{1331} & A_{1312} & A_{1322} & A_{1332} & A_{1313} &
A_{1323} & A_{1333} \\
A_{2111} & A_{2121} & A_{2131} & A_{2112} & A_{2122} & A_{2132} & A_{2113} &
A_{2123} & A_{2133} \\
A_{2211} & A_{2221} & A_{2231} & A_{2212} & A_{2222} & A_{2232} & A_{2213} &
A_{2223} & A_{2233} \\
A_{2311} & A_{2321} & A_{2331} & A_{2312} & A_{2322} & A_{2332} & A_{2313} &
A_{2323} & A_{2333} \\
A_{3111} & A_{3121} & A_{3131} & A_{3112} & A_{3122} & A_{3132} & A_{3113} &
A_{3123} & A_{3133} \\
A_{3211} & A_{3221} & A_{3231} & A_{3212} & A_{3222} & A_{3232} & A_{3213} &
A_{3223} & A_{3233} \\
A_{3311} & A_{3321} & A_{3331} & A_{3312} & A_{3322} & A_{3332} & A_{3313} &
A_{3323} & A_{3333} \\
\end{smallmatrix} \right]
\left[\begin{smallmatrix}
B_{11} \\ B_{12} \\ B_{13} \\ B_{21} \\ B_{22} \\ B_{23} \\ B_{31} \\ B_{32} \\ B_{33}
\end{smallmatrix}\right]
\end{aligned} ∼ C ⎣ ⎡ C 11 C 12 C 13 C 21 C 22 C 23 C 31 C 32 C 33 ⎦ ⎤ = A ∼ B = ⎣ ⎡ A 1111 A 1211 A 1311 A 2111 A 2211 A 2311 A 3111 A 3211 A 3311 A 1121 A 1221 A 1321 A 2121 A 2221 A 2321 A 3121 A 3221 A 3321 A 1131 A 1231 A 1331 A 2131 A 2231 A 2331 A 3131 A 3231 A 3331 A 1112 A 1212 A 1312 A 2112 A 2212 A 2312 A 3112 A 3212 A 3312 A 1122 A 1222 A 1322 A 2122 A 2222 A 2322 A 3122 A 3222 A 3322 A 1132 A 1232 A 1332 A 2132 A 2232 A 2332 A 3132 A 3232 A 3332 A 1113 A 1213 A 1313 A 2113 A 2213 A 2313 A 3113 A 3213 A 3313 A 1123 A 1223 A 1323 A 2123 A 2223 A 2323 A 3123 A 3223 A 3323 A 1133 A 1233 A 1333 A 2133 A 2233 A 2333 A 3133 A 3233 A 3333 ⎦ ⎤ ⎣ ⎡ B 11 B 12 B 13 B 21 B 22 B 23 B 31 B 32 B 33 ⎦ ⎤ Note that the matrix A ‾ ‾ \MQ{A} A has indeed 81 components (all the components of
4 A \TQ{A} 4 A ), although this matrix is only valid in conjunction with a double inner product
with a second-order tensor.
In the particular case of mechanics, symmetric second-order tensors play an important
role. Taking into account the symmetry of a second-order tensor B \T{B} B permits to store
the 6 distinct components in a smaller column with a somewhat different structure
B ∼ = [ B 11 B 22 B 33 B 12 B 13 B 23 ] \C{B} \;=\; \begin{bmatrix}
B_{11} \\ B_{22} \\ B_{33} \\ B_{12} \\ B_{13} \\ B_{23}
\end{bmatrix} ∼ B = ⎣ ⎡ B 11 B 22 B 33 B 12 B 13 B 23 ⎦ ⎤ If the resulting tensor C \T{C} C is not symmetric, it is represented
by a column with 9 components. The matrix A ‾ ‾ \MQ{A} A is
restructured and condensed to a [ 9 × 6 ] [9\times 6] [ 9 × 6 ] matrix by adding up
the appropriate columns in equation (A.150) , i.e. if
B ∼ \C{B} ∼ B has the format (A.151) and C ∼ \C{C} ∼ C
maintains the format (A.148) then C = 4 A : B \T{C}=\TQ{A} \dinp
\T{B} C = 4 A : B is represented in component form by
C ∼ = A ‾ ‾ B ∼ [ C 11 C 12 C 13 C 21 C 22 C 23 C 31 C 32 C 33 ] = [ A 1111 A 1122 A 1133 ( A 1112 + A 1121 ) ( A 1113 + A 1131 ) ( A 1123 + A 1132 ) A 1211 A 1222 A 1233 ( A 1212 + A 1221 ) ( A 1213 + A 1231 ) ( A 1223 + A 1232 ) A 1311 A 1322 A 1333 ( A 1312 + A 1321 ) ( A 1313 + A 1331 ) ( A 1323 + A 1332 ) A 2111 A 2122 A 2133 ( A 2112 + A 2121 ) ( A 2113 + A 2131 ) ( A 2123 + A 2132 ) A 2211 A 2222 A 2233 ( A 2212 + A 2221 ) ( A 2213 + A 2231 ) ( A 2223 + A 2232 ) A 2311 A 2322 A 2333 ( A 2312 + A 2321 ) ( A 2313 + A 2331 ) ( A 2323 + A 2332 ) A 3111 A 3122 A 3133 ( A 3112 + A 3121 ) ( A 3113 + A 3131 ) ( A 3123 + A 3132 ) A 3211 A 3222 A 3233 ( A 3212 + A 3221 ) ( A 3213 + A 3231 ) ( A 3223 + A 3232 ) A 3311 A 3322 A 3333 ( A 3312 + A 3321 ) ( A 3313 + A 3331 ) ( A 3323 + A 3332 ) ] [ B 11 B 22 B 33 B 12 B 13 B 23 ] \begin{aligned}
\C{C} \;&=\; \MQ{A}\, \C{B} \\
\left[\begin{smallmatrix}
C_{11} \\ C_{12} \\ C_{13} \\ C_{21} \\ C_{22} \\ C_{23} \\ C_{31} \\ C_{32} \\ C_{33}
\end{smallmatrix}\right]
&= \left[\begin{smallmatrix}
A_{1111} & A_{1122} & A_{1133} & (A_{1112}+A_{1121}) & (A_{1113}+A_{1131}) &
(A_{1123}+A_{1132}) \\
A_{1211} & A_{1222} & A_{1233} & (A_{1212}+A_{1221}) & (A_{1213}+A_{1231}) &
(A_{1223}+A_{1232}) \\
A_{1311} & A_{1322} & A_{1333} & (A_{1312}+A_{1321}) & (A_{1313}+A_{1331}) &
(A_{1323}+A_{1332}) \\
A_{2111} & A_{2122} & A_{2133} & (A_{2112}+A_{2121}) & (A_{2113}+A_{2131}) &
(A_{2123}+A_{2132}) \\
A_{2211} & A_{2222} & A_{2233} & (A_{2212}+A_{2221}) & (A_{2213}+A_{2231}) &
(A_{2223}+A_{2232}) \\
A_{2311} & A_{2322} & A_{2333} & (A_{2312}+A_{2321}) & (A_{2313}+A_{2331}) &
(A_{2323}+A_{2332}) \\
A_{3111} & A_{3122} & A_{3133} & (A_{3112}+A_{3121}) & (A_{3113}+A_{3131}) &
(A_{3123}+A_{3132}) \\
A_{3211} & A_{3222} & A_{3233} & (A_{3212}+A_{3221}) & (A_{3213}+A_{3231}) &
(A_{3223}+A_{3232}) \\
A_{3311} & A_{3322} & A_{3333} & (A_{3312}+A_{3321}) & (A_{3313}+A_{3331}) &
(A_{3323}+A_{3332})
\end{smallmatrix}\right]
\left[\begin{smallmatrix}
B_{11} \\ B_{22} \\ B_{33} \\ B_{12} \\ B_{13} \\ B_{23}
\end{smallmatrix}\right]
\end{aligned} ∼ C ⎣ ⎡ C 11 C 12 C 13 C 21 C 22 C 23 C 31 C 32 C 33 ⎦ ⎤ = A ∼ B = ⎣ ⎡ A 1111 A 1211 A 1311 A 2111 A 2211 A 2311 A 3111 A 3211 A 3311 A 1122 A 1222 A 1322 A 2122 A 2222 A 2322 A 3122 A 3222 A 3322 A 1133 A 1233 A 1333 A 2133 A 2233 A 2333 A 3133 A 3233 A 3333 ( A 1112 + A 1121 ) ( A 1212 + A 1221 ) ( A 1312 + A 1321 ) ( A 2112 + A 2121 ) ( A 2212 + A 2221 ) ( A 2312 + A 2321 ) ( A 3112 + A 3121 ) ( A 3212 + A 3221 ) ( A 3312 + A 3321 ) ( A 1113 + A 1131 ) ( A 1213 + A 1231 ) ( A 1313 + A 1331 ) ( A 2113 + A 2131 ) ( A 2213 + A 2231 ) ( A 2313 + A 2331 ) ( A 3113 + A 3131 ) ( A 3213 + A 3231 ) ( A 3313 + A 3331 ) ( A 1123 + A 1132 ) ( A 1223 + A 1232 ) ( A 1323 + A 1332 ) ( A 2123 + A 2132 ) ( A 2223 + A 2232 ) ( A 2323 + A 2332 ) ( A 3123 + A 3132 ) ( A 3223 + A 3232 ) ( A 3323 + A 3332 ) ⎦ ⎤ ⎣ ⎡ B 11 B 22 B 33 B 12 B 13 B 23 ⎦ ⎤ If the fourth-order tensor presents a symmetry, the equations can be simplified
considerably. A right symmetric tensor has only 54 distinct components (3 columns
equal 3 other columns in the matrix A ‾ ‾ \MQ{A} A ). A left symmetric tensor has also
only 54 distinct components (3 lines equal 3 other lines in the matrix
A ‾ ‾ \MQ{A} A ). A tensor which is left and right symmetric has only 36 independent
components (only 6 lines and columns remain in the matrix A ‾ ‾ \MQ{A} A ). The case
where the tensor 4 A \TQ{A} 4 A is left symmetric results in a tensor C \T{C} C which is
symmetric. Applying C = 4 A : B \T{C}=\TQ{A} \dinp \T{B} C = 4 A : B again to a symmetric B \T{B} B can then be
done with columns B ∼ \C{B} ∼ B and C ∼ \C{C} ∼ C of the form (A.151) . The result in
this particular case is then condensed as
C ∼ = A ‾ ‾ B ∼ [ C 11 C 22 C 33 C 12 C 13 C 23 ] = [ A 1111 A 1122 A 1133 A 1112 + A 1121 A 1113 + A 1131 A 1123 + A 1132 A 2211 A 2222 A 2233 A 2212 + A 2221 A 2213 + A 2231 A 2223 + A 2232 A 3311 A 3322 A 3333 A 3312 + A 3321 A 3313 + A 3331 A 3323 + A 3332 A 1211 A 1222 A 1233 A 1212 + A 1221 A 1213 + A 1231 A 1223 + A 1232 A 1311 A 1322 A 1333 A 1312 + A 1321 A 1313 + A 1331 A 1323 + A 1332 A 2311 A 2322 A 2333 A 2312 + A 2321 A 2313 + A 2331 A 2323 + A 2332 ] [ B 11 B 22 B 33 B 12 B 13 B 23 ] \begin{aligned}
\C{C} \;&=\; \MQ{A}\, \C{B} \\
\left[\begin{smallmatrix}
C_{11} \\ C_{22} \\ C_{33} \\ C_{12} \\ C_{13} \\ C_{23}
\end{smallmatrix} \right]
\;&=\; \left[\begin{smallmatrix}
A_{1111} & A_{1122} & A_{1133} & A_{1112}+A_{1121} & A_{1113}+A_{1131} &
A_{1123}+A_{1132} \\
A_{2211} & A_{2222} & A_{2233} & A_{2212}+A_{2221} & A_{2213}+A_{2231} &
A_{2223}+A_{2232} \\
A_{3311} & A_{3322} & A_{3333} & A_{3312}+A_{3321} & A_{3313}+A_{3331} &
A_{3323}+A_{3332} \\
A_{1211} & A_{1222} & A_{1233} & A_{1212}+A_{1221} & A_{1213}+A_{1231} &
A_{1223}+A_{1232} \\
A_{1311} & A_{1322} & A_{1333} & A_{1312}+A_{1321} & A_{1313}+A_{1331} &
A_{1323}+A_{1332} \\
A_{2311} & A_{2322} & A_{2333} & A_{2312}+A_{2321} & A_{2313}+A_{2331} &
A_{2323}+A_{2332}
\end{smallmatrix} \right]
\left[\begin{smallmatrix}
B_{11} \\ B_{22} \\ B_{33} \\ B_{12} \\ B_{13} \\ B_{23}
\end{smallmatrix}\right]
\end{aligned} ∼ C ⎣ ⎡ C 11 C 22 C 33 C 12 C 13 C 23 ⎦ ⎤ = A ∼ B = ⎣ ⎡ A 1111 A 2211 A 3311 A 1211 A 1311 A 2311 A 1122 A 2222 A 3322 A 1222 A 1322 A 2322 A 1133 A 2233 A 3333 A 1233 A 1333 A 2333 A 1112 + A 1121 A 2212 + A 2221 A 3312 + A 3321 A 1212 + A 1221 A 1312 + A 1321 A 2312 + A 2321 A 1113 + A 1131 A 2213 + A 2231 A 3313 + A 3331 A 1213 + A 1231 A 1313 + A 1331 A 2313 + A 2331 A 1123 + A 1132 A 2223 + A 2232 A 3323 + A 3332 A 1223 + A 1232 A 1323 + A 1332 A 2323 + A 2332 ⎦ ⎤ ⎣ ⎡ B 11 B 22 B 33 B 12 B 13 B 23 ⎦ ⎤ Other simplifications are easy to make and left to the reader.
A.8 Summary ¶ Vector operations
Multiplication b ⃗ = α a ⃗ \V{b} = \alpha \V{a} b = α a Sum c ⃗ = a ⃗ + b ⃗ \V{c} = \V{a} + \V{b} c = a + b Inner product a ⃗ ⋅ b ⃗ = ∥ a ⃗ ∥ ∥ b ⃗ ∥ cos ( ϕ ) \V{a} \inp \V{b} = \lVert \V{a} \rVert\; \lVert \V{b} \rVert\cos(\phi) a ⋅ b = ∥ a ∥ ∥ b ∥ cos ( ϕ ) a ⃗ ⋅ b ⃗ = b ⃗ ⋅ a ⃗ \V{a} \inp \V{b} = \V{b} \inp \V{a} a ⋅ b = b ⋅ a Cross product a ⃗ × b ⃗ = c ⃗ = ∥ a ⃗ ∥ ∥ b ⃗ ∥ sin ( ϕ ) \V{a} \cross \V{b} = \V{c} = \lVert \V{a} \rVert \; \lVert \V{b} \rVert \sin(\phi) a × b = c = ∥ a ∥ ∥ b ∥ sin ( ϕ ) b ⃗ × a ⃗ = − a ⃗ × b ⃗ \V{b} \cross \V{a} = - \V{a} \cross \V{b} b × a = − a × b Triple product a ⃗ × b ⃗ ⋅ c ⃗ = ∥ a ⃗ ∥ ∥ b ⃗ ∥ sin ( ϕ ) ∥ c ⃗ ∥ cos ( ψ ) \V{a} \cross \V{b} \inp \V{c} = \lVert \V{a} \rVert \; \lVert \V{b} \rVert \sin(\phi) \lVert \V{c} \rVert \cos(\psi) a × b ⋅ c = ∥ a ∥ ∥ b ∥ sin ( ϕ ) ∥ c ∥ cos ( ψ ) Tensor product (dyad) a ⃗ b ⃗ \V{a} \V{b} a b a ⃗ b ⃗ ⋅ p ⃗ = a ⃗ ( b ⃗ ⋅ p ⃗ ) \V{a} \V{b} \inp \V{p} = \V{a} (\V{b} \inp \V{p}) a b ⋅ p = a ( b ⋅ p ) ( a ⃗ b ⃗ ) T = b ⃗ a ⃗ (\V{a} \V{b})^T = \V{b} \V{a} ( a b ) T = b a
Gradient operators
Cartesian ∇ ⃗ = e ⃗ 1 ∂ ∂ x 1 + e ⃗ 2 ∂ ∂ x 2 + e ⃗ 3 ∂ ∂ x 3 \grad = \V{e}_1 \parder{}{x_1} + \V{e}_2 \parder{}{x_2} + \V{e}_3 \parder{}{x_3} ∇ = e 1 ∂ x 1 ∂ + e 2 ∂ x 2 ∂ + e 3 ∂ x 3 ∂ grad a ⃗ \text{grad\ }\V{a} grad a grad a ⃗ = ∇ ⃗ a ⃗ = e ⃗ 1 ∂ a ⃗ ∂ x 1 + e ⃗ 2 ∂ a ⃗ ∂ x 2 + e ⃗ 3 ∂ a ⃗ ∂ x 3 \text{grad\ }\V{a} = \grad \V{a} = \V{e}_1 \parder{\V{a}}{x_1} + \V{e}_2 \parder{\V{a}}{x_2} + \V{e}_3 \parder{\V{a}}{x_3} grad a = ∇ a = e 1 ∂ x 1 ∂ a + e 2 ∂ x 2 ∂ a + e 3 ∂ x 3 ∂ a ∇ ⃗ a ⃗ = a j , i e ⃗ i e ⃗ j \grad \V{a} = a_{j,i} \V{e}_i\V{e}_j ∇ a = a j , i e i e j div a ⃗ \text{div\ }\V{a} div a div a ⃗ = ∇ ⃗ ⋅ a ⃗ = e ⃗ 1 ⋅ ∂ a ⃗ ∂ x 1 + e ⃗ 2 ⋅ ∂ a ⃗ ∂ x 2 + e ⃗ 3 ⋅ ∂ a ⃗ ∂ x 3 \text{div\ }\V{a} = \grad \inp \V{a} = \V{e}_1 \inp \parder{\V{a}}{x_1} + \V{e}_2 \inp \parder{\V{a}}{x_2} + \V{e}_3 \inp\parder{\V{a}}{x_3} div a = ∇ ⋅ a = e 1 ⋅ ∂ x 1 ∂ a + e 2 ⋅ ∂ x 2 ∂ a + e 3 ⋅ ∂ x 3 ∂ a rot a ⃗ \text{rot\ }\V{a} rot a rot a ⃗ = ∇ ⃗ × a ⃗ = e ⃗ 1 × ∂ a ⃗ ∂ x 1 + e ⃗ 2 × ∂ a ⃗ ∂ x 2 + e ⃗ 3 × ∂ a ⃗ ∂ x 3 \text{rot\ }\V{a} = \grad \cross \V{a} = \V{e}_1 \cross \parder{\V{a}}{x_1} + \V{e}_2 \cross \parder{\V{a}}{x_2} + \V{e}_3 \cross \parder{\V{a}}{x_3} rot a = ∇ × a = e 1 × ∂ x 1 ∂ a + e 2 × ∂ x 2 ∂ a + e 3 × ∂ x 3 ∂ a Cylindrical ∇ ⃗ = e ⃗ r ∂ ∂ r + e ⃗ t 1 r ∂ ∂ θ + e ⃗ z ∂ ∂ z \grad = \V{e}_r \parder{}{r} + \V{e}_t \frac{1}{r} \parder{}{\theta} + \V{e}_z \parder{}{z} ∇ = e r ∂ r ∂ + e t r 1 ∂ θ ∂ + e z ∂ z ∂
Second-order Tensors
Second order tensor A ⋅ p ⃗ = q ⃗ \T{A} \inp \V{p} = \V{q} A ⋅ p = q A ⋅ ( α m ⃗ + β n ⃗ ) = α A ⋅ m ⃗ + β A ⋅ n ⃗ \T{A} \inp (\alpha \V{m} + \beta \V{n}) = \alpha \T{A} \inp \V{m} + \beta \T{A} \inp \V{n} A ⋅ ( α m + β n ) = α A ⋅ m + β A ⋅ n ( α A ) ⋅ v ⃗ = A ⋅ ( α v ⃗ ) (\alpha \T{A}) \inp \V{v} = \T{A} \inp (\alpha \V{v}) ( α A ) ⋅ v = A ⋅ ( α v ) ( A + B ) ⋅ v ⃗ = A ⋅ v ⃗ + B ⋅ v ⃗ (\T{A} + \T{B}) \inp \V{v} = \T{A} \inp \V{v} + \T{B} \inp \V{v} ( A + B ) ⋅ v = A ⋅ v + B ⋅ v ( A ⋅ B ) ⋅ v ⃗ = A ⋅ ( B ⋅ v ⃗ ) (\T{A}\inp\T{B})\inp\V{v} = \T{A}\inp(\T{B}\inp\V{v}) ( A ⋅ B ) ⋅ v = A ⋅ ( B ⋅ v ) Conjugate of tensor A T ⋅ p ⃗ = p ⃗ ⋅ A \T{A}^T \inp \V{p} = \V{p} \inp \T{A} A T ⋅ p = p ⋅ A Unit tensor I = e ⃗ 1 e ⃗ 1 + e ⃗ 2 e ⃗ 2 + e ⃗ 3 e ⃗ 3 \T{I} = \V{e}_1\V{e}_1 + \V{e}_2\V{e}_2 + \V{e}_3\V{e}_3 I = e 1 e 1 + e 2 e 2 + e 3 e 3 First invariant J 1 ( A ) = tr ( A ) J_1(\T{A}) = \tr(\T{A}) J 1 ( A ) = tr ( A ) Second invariant J 2 ( A ) = 1 2 { tr 2 ( A ) − tr ( A 2 ) } J_2(\T{A}) = \half \{ \tr^2(\T{A}) - \tr(\T{A}^2) \} J 2 ( A ) = 2 1 { tr 2 ( A ) − tr ( A 2 )} Third invariant J 3 ( A ) = det ( A ) J_3(\T{A}) = \det(\T{A}) J 3 ( A ) = det ( A ) Double dot product A : B = tr ( A ⋅ B ) \T{A}\dinp\T{B} = \tr (\T{A}\inp\T{B} ) A : B = tr ( A ⋅ B ) A : I = tr ( A ) \T{A} \dinp \T{I} = \tr(\T{A}) A : I = tr ( A ) A : B = A T : B T \T{A} \dinp \T{B} = \T{A}^T \dinp \T{B}^T A : B = A T : B T Inverse tensor A − 1 ⋅ A = I \T{A}^{-1} \inp \T{A} = \T{I} A − 1 ⋅ A = I ( A ⋅ B ) − 1 = B − 1 ⋅ A − 1 (\T{A} \inp \T{B} )^{-1} = \T{B}^{-1} \inp \T{A}^{-1} ( A ⋅ B ) − 1 = B − 1 ⋅ A − 1 Deviatoric part A d = A − 1 3 tr ( A ) I \T{A}^d = \T{A} - \tfrac{1}{3} \tr(\T{A}) \T{I} A d = A − 3 1 tr ( A ) I Symmetric tensor A T = A \T{A}^T = \T{A} A T = A Skew-symmetric tensor A T = − A \T{A}^T = -\T{A} A T = − A Positive definite tensor a ⃗ ⋅ A ⋅ a ⃗ > 0 ∀ a ⃗ ≠ 0 ⃗ \V{a} \inp \T{A} \inp \V{a} > 0 \quad \forall\;\V{a} \neq \V{0} a ⋅ A ⋅ a > 0 ∀ a = 0 Orthogonal tensor ( A ⋅ a ⃗ ) ⋅ ( A ⋅ b ⃗ ) = a ⃗ ⋅ b ⃗ ∀ a ⃗ , b ⃗ (\T{A} \inp \V{a}) \inp (\T{A} \inp \V{b}) = \V{a} \inp \V{b} \quad \forall\ \V{a},\V{b} ( A ⋅ a ) ⋅ ( A ⋅ b ) = a ⋅ b ∀ a , b
Fourth-order Tensors
Transformation B = 4 C : A \T{B} = \TQ{C} \dinp \T{A} B = 4 C : A Components [ 3 × 3 × 3 × 3 ] [3 \times 3 \times 3 \times 3] [ 3 × 3 × 3 × 3 ] matrixTotal transpose 4 C T = [ C i j k l ] T = C l k j i \TQ{C}^{T} = [C_{ijkl}]^{T} = C_{lkji} 4 C T = [ C ijk l ] T = C l kji Left transpose 4 C L T = [ C i j k l ] L T = C j i k l \TQ{C}^{LT} = [C_{ijkl}]^{LT} = C_{jikl} 4 C L T = [ C ijk l ] L T = C jik l Right transpose 4 C R T = [ C i j k l ] R T = C i j l k \TQ{C}^{RT} = [C_{ijkl}]^{RT} = C_{ijlk} 4 C RT = [ C ijk l ] RT = C ij l k Left symmetric 4 C = 4 C L T \TQ{C} = \TQ{C}^{LT} 4 C = 4 C L T Right symmetric 4 C = 4 C R T \TQ{C} = \TQ{C}^{RT} 4 C = 4 C RT Middle symmetric 4 C = 4 C T \TQ{C} = \TQ{C}^{T} 4 C = 4 C T Total symmetric 4 C = 4 C L T = 4 C R T = 4 C T \TQ{C} = \TQ{C}^{LT} = \TQ{C}^{RT} = \TQ{C}^{T} 4 C = 4 C L T = 4 C RT = 4 C T Fourth-order unit tensor 4 I : A = A \TQ{I}\dinp\T{A} = \T{A} 4 I : A = A Symmetric fourth-order unit 4 I s : A = A s = 1 2 ( A + A T ) \TQ{I}^s\dinp\T{A} = \T{A}^s = \tfrac{1}{2}(\T{A} + \T{A}^T) 4 I s : A = A s = 2 1 ( A + A T ) Products 4 C = 4 A ⋅ B \TQ{C} = \TQ{A} \inp \T{B} 4 C = 4 A ⋅ B 4 C = 4 A : 4 B \TQ{C} = \TQ{A}\dinp\TQ{B} 4 C = 4 A : 4 B Matrix condensation B = 4 C : A ⟹ B ∼ = C ‾ ‾ A ∼ \T{B} = \TQ{C} \dinp \T{A} \Longrightarrow \C{B} = \MQ{C}\, \C{A} B = 4 C : A ⟹ ∼ B = C ∼ A