Differential and Vector Calculus in the Context of Solid Mechanics, Exams of Dynamics

An introduction to the concepts of vector calculus, including the gradient, divergence, and curl of a vector field, as well as their applications in solid mechanics. the basics of vector differentiation, the relationship between Cartesian and cylindrical or spherical coordinates, and the physical interpretation of these operators. The document also includes several equations and problems for further study.

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Section 1.6
Solid Mechanics Part III Kelly
30
1.6 Vector Calculus 1 - Differentiation
Calculus involving vectors is discussed in this section, rather intuitively at first and more
formally toward the end of this section.
1.6.1 The Ordinary Calculus
Consider a scalar-valued function of a scalar, for example the time-dependent density
of a material )(t
. The calculus of scalar valued functions of scalars is just the
ordinary calculus. Some of the important concepts of the ordinary calculus are reviewed
in Appendix B to this Chapter, §1.B.2.
1.6.2 Vector-valued Functions of a scalar
Consider a vector-valued function of a scalar, for example the time-dependent
displacement of a particle )(tuu . In this case, the derivative is defined in the usual
way,
t
ttt
dt
d
t
)()(
lim 0
uuu ,
which turns out to be simply the derivative of the coefficients1,
i
i
d
t
du
d
t
du
d
t
du
d
t
du
d
t
deeee
u 3
3
2
2
1
1
Partial derivatives can also be defined in the usual way. For example, if u is a function of
the coordinates, ),,( 321 xxxu, then
1
3213211
0
1
),,(),,(
lim 1x
xxxxxxx
xx
uu
u
Differentials of vectors are also defined in the usual way, so that when 321 ,, uuu undergo
increments 332211 ,, uduuduudu
, the differential of u is
332211 eeeu dududud
and the differential and actual increment u
approach one another as
0,, 321 uuu .
1 assuming that the base vectors do not depend on t
pf3
pf4
pf5
pf8
pf9
pfa
pfd
pfe
pff
pf12
pf13
pf14

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1.6 Vector Calculus 1 - Differentiation

Calculus involving vectors is discussed in this section, rather intuitively at first and more

formally toward the end of this section.

1.6.1 The Ordinary Calculus

Consider a scalar-valued function of a scalar , for example the time-dependent density

of a material   ( t ). The calculus of scalar valued functions of scalars is just the

ordinary calculus. Some of the important concepts of the ordinary calculus are reviewed

in Appendix B to this Chapter, §1.B.2.

1.6.2 Vector-valued Functions of a scalar

Consider a vector-valued function of a scalar , for example the time-dependent

displacement of a particle uu ( t ). In this case, the derivative is defined in the usual

way,

t

t t t

dt

d t

lim (^0)

u u u ,

which turns out to be simply the derivative of the coefficients

1 ,

i

i

dt

du

dt

du

dt

du

dt

du

dt

d e e e e

u    3 

3 2

2 1

1

Partial derivatives can also be defined in the usual way. For example, if u is a function of

the coordinates, u ( x 1 , x 2 , x 3 ), then

1

1 1 2 3 1 2 3 0 1

lim 1 x

x x x x x x x

x

x

 

u u u

Differentials of vectors are also defined in the usual way, so that when u 1 (^) , u 2 , u 3 undergo

increments du 1 (^)   u 1 , du 2  u 2 , du 3  u 3 , the differential of u is

d udu 1 e 1  du 2 e 2  du 3 e 3

and the differential and actual increment  u approach one another as

u 1 ,  u 2 , u 3  0.

(^1) assuming that the base vectors do not depend on t

Space Curves

The derivative of a vector can be interpreted geometrically as shown in Fig. 1.6.1:  u is

the increment in u consequent upon an increment  t in t. As t changes, the end-point of

the vector u ( t )traces out the dotted curve  shown – it is clear that as  t  0 ,  u

approaches the tangent to  , so that d u / dt is tangential to . The unit vector tangent to

the curve is denoted by τ :

d dt

d dt

u

u τ  (1.6.1)

Figure 1.6.1: a space curve; (a) the tangent vector, (b) increment in arc length

Let s be a measure of the length of the curve  , measured from some fixed point on .

Let  s be the increment in arc-length corresponding to increments in the coordinates,

T  u   u 1 (^) ,  u 2 , u 3 , Fig. 1.6.1b. Then, from the ordinary calculus (see Appendix

1.B),

2 3

2 2

2 1

2 dsdududu

so that

2 3

2 2

2 1  

dt

du

dt

du

dt

du

dt

ds

But

3

3 2

2 1

1 e e e

u

dt

du

dt

du

dt

du

dt

d   

so that

dt

ds

dt

d

u (1.6.2)

u ( t ) u ( t  t )

u

τ

s

x 1

x 2

du 1

ds du 2

s

(a) (b)

ds

d τ ν

Figure 1.6.2: the curvature

This can be seen geometrically in Fig. 1.6.2: from Eqn. 1.6.5,  τ is a vector of

magnitude  s in the direction of the vector normal to τ. The radius of curvature R is

defined as the reciprocal of the curvature; it is the radius of the circle which just touches

the curve at s , Fig. 1.6.2.

Finally, the unit vector perpendicular to both the tangent vector and the principal normal

vector is called the unit binormal vector :

bτν (1.6.6)

The planes defined by these vectors are shown in Fig. 1.6.3; they are called the rectifying

plane , the normal plane and the osculating plane.

Figure 1.6.3: the unit tangent, principal normal and binormal vectors and associated

planes

τ ( s )

s

R

τ ( sds )

τ

ν ( s )

ν ( sds )

 s

 s

τ

ν

b

Normal plane

Osculating

plane

Rectifying

plane

Rules of Differentiation

The derivative of a vector is also a vector and the usual rules of differentiation apply,

dt

d

dt

d t dt

d

dt

d

dt

d

dt

d

  v

v v

u v u v

Also, it is straight forward to show that {▲Problem 2}

    a

a v a v a v

a v vav         dt

d

dt

d

dt

d

dt

d

dt

d

dt

d (1.6.8)

(The order of the terms in the cross-product expression is important here.)

1.6.3 Fields

In many applications of vector calculus, a scalar or vector can be associated with each

point in space x. In this case they are called scalar or vector fields. For example

 ( x ) temperature^ a scalar field (a scalar-valued function of position)

v ( x ) velocity a vector field (a vector valued function of position)

These quantities will in general depend also on time, so that one writes  ( x , t )or v ( x , t ).

Partial differentiation of scalar and vector fields with respect to the variable t is

symbolised by  /  t. On the other hand, partial differentiation with respect to the

coordinates is symbolised by  /  xi. The notation can be made more compact by

introducing the subscript comma to denote partial differentiation with respect to the

coordinate variables, in which case  (^) , i   / xi , ui (^) jk   ui / xjxk

2 , , and so on.

1.6.4 The Gradient of a Scalar Field

Let  ( x )be a scalar field. The gradient of  is a vector field defined by (see Fig. 1.6.4)

x

e

e e e

i xi

x x x

3 3

2 2

1 1

Gradient of a Scalar Field (1.6.9)

The gradient  is of considerable importance because if one takes the dot product of

  with d x^ , it gives the increment in  :

(iii) the direction of zero d  is in the direction perpendicular to 

Figure 1.6.5: gradient of a temperature field

The curves   x 1 , x 2  const.are called isotherms (curves of constant temperature). In

general, they are called iso-curves (or iso-surfaces in three dimensions).

Many physical laws are given in terms of the gradient of a scalar field. For example,

Fourier’s law of heat conduction relates the heat flux q (the rate at which heat flows

through a surface of unit area

3 ) to the temperature gradient through

q   k   (1.6.13)

where k is the thermal conductivity of the material, so that heat flows along the direction

normal to the isotherms.

The Normal to a Surface

In the above example, it was seen that  points in the direction normal to the curve

 const. Here it will be seen generally how and why the gradient can be used to obtain

a normal vector to a surface.

Consider a surface represented by the scalar function f^ (^ x 1 , x 2 , x 3 ) c ,^ c^ a constant^

(^4) , and

also a space curve C lying on the surface, defined by the position vector

rx 1 (^) ( t ) e 1  x 2 ( t ) e 2  x 3 ( t ) e 3. The components of r must satisfy the equation of the

surface, so f ( x 1 ( t ), x 2 ( t ), x 3 ( t )) c. Differentiation gives

3

3

2

2

1

1

dt

dx

x

f

dt

dx

x

f

dt

dx

x

f

dt

df

(^3) the flux is the rate of flow of fluid, particles or energy through a given surface; the flux density is the flux

per unit area but, as here, this is more commonly referred to simply as the flux

(^4) a surface can be represented by the equation f ( x , x , x ) c 1 2 3 ; for example, the expression

4

2 3

2 2

2 x 1 (^)  xx  is the equation for a sphere of radius 2 (with centre at the origin). Alternatively, the

surface can be written in the form x (^) 3  g ( x 1 , x 2 ), for example

2 2

2 x 3 (^)  4  x 1  x

which is equivalent to the equation grad f   d r / dt   0 and, as seen in §1.6.2, d r / dt is a

vector tangential to the surface. Thus grad f is normal to the tangent vector; grad f must

be normal to all the tangents to all the curves through p , so it must be normal to the plane

tangent to the surface.

Taylor’s Series

Writing  as a function of three variables (omitting time t ), so that   ( x 1 , x 2 , x 3 ), then

 can be expanded in a three-dimensional Taylor’s series:

2 2 1 1

2

3 3

2 2

1 1

1 1 2 2 3 3 1 2 3

dx x

dx x

dx x

dx x

x dx x dx x dx x x x

    

Neglecting the higher order terms, this can be written as

x x

x d x xd

which is equivalent to 1.6.9, 1.6.10.

1.6.5 The Nabla Operator

The symbolic vector operator  is called the Nabla operator

5

. One can write this in

component form as

i

i x x xx

  e e e e

3

3 2

2 1

One can generalise the idea of the gradient of a scalar field by defining the dot product

and the cross product of the vector operator  with a vector field   , according to the

rules

i

i i

i x x

e , e (1.6.15)

The following terminology is used:

u u

u u

curl

div

grad  

(^5) or del or the Gradient operator

with the partial derivatives evaluated at ( x 1 , x 2 , x 3 ), so the volume flux out is

3

1 2 3

1

2

1 2 2

1

1

1 2 3 1 (^1 , 2 , 3 ) 1 x

v x x

v x x

v x x v x x x x

Figure 1.6.6: a differential element; (a) flow through a face, (b) volume of material

flowing through the face

The net volume flux out (rate of volume flow out through the right-hand face minus the

rate of volume flow in through the left-hand face) is then  x 1  x 2  x 3   v 1 /  x 1 and the net

volume flux per unit volume is  v 1 (^) /  x 1. Carrying out a similar calculation for the other

two coordinate directions leads to

net unit volume flux out of an elemental volume : div v

3

3

2

2

1

1  

x

v

x

v

x

v (1.6.18)

which is the physical meaning of the divergence of the velocity field.

If div v  0 , there is a net flow out and the density of material is decreasing. On the other

hand, if div v  0 , the inflow equals the outflow and the density remains constant – such a

material is called incompressible

9

. A flow which is divergence free is said to be

isochoric. A vector v for which div v  0 is said to be solenoidal.

Notes:

 The above result holds only in the limit when the element shrinks to zero size – so that

the extra terms in the Taylor series tend to zero and the velocity field varies in a linear

fashion over a face

 consider the velocity at a fixed point in space, v x ( , ) t. The velocity at a later time,

v x ( , t   t ), actually gives the velocity of a different material particle. This is shown in

Fig. 1.6.7 below: the material particles 1 , 2 , 3 are moving through space and whereas

v ( x , t )represents the velocity of particle 2, v x ( , t   t )now represents the velocity of

particle 1, which has moved into position x. This point is important in the consideration

of the kinematics of materials, to be discussed in Chapter 2

(^9) a liquid , such as water, is a material which is incompressible

( x 1 , x 2 , x 3 ) v 1 (^) ( x 1  x 1 , x 2 , x 3 )  x 1

x 2

v 1 (^) ( x 1  x 1 , x 2 , x 3  x 3 )

v 1 (^) ( x 1  x 1 , x 2  x 2 , x 3  x 3 )

v 1 (^) ( x 1  x 1 , x 2  x 2 , x 3 )

x 3

v ave

(a) (b)

Figure 1.6.7: moving material particles

Another example would be the divergence of the heat flux vector q. This time suppose

also that there is some generator of heat inside the element (a source ), generating at a rate

of r per unit volume, r being a scalar field. Again, assuming the element to be small, one

takes r to be acting at the mid-point of the element, and one considers ( 2 1 , )

1 r x 1   x .

Assume a steady-state heat flow, so that the (heat) energy within the elemental volume

remains constant with time – the law of balance of (heat) energy then requires that the net

flow of heat out must equal the heat generated within, so

3

2 3

1

2

2 2

1

1

2 1

1 1 2 3 1 2 3

3

3 1 2 3 2

2 1 2 3 1

1 1 2 3

x

r x x

r x x

r x x x rx x x x

x

q x x x x

q x x x x

q x x x

Dividing through by  x 1 (^)  x 2  x 3 and taking the limit as  x 1 (^) ,  x 2 , x 3  0 , one obtains

div qr (1.6.19)

Here, the divergence of the heat flux vector field can be interpreted as the heat generated

(or absorbed) per unit volume per unit time in a temperature field. If the divergence is

zero, there is no heat being generated (or absorbed) and the heat leaving the element is

equal to the heat entering it.

1.6.7 The Laplacian

Combining Fourier’s law of heat conduction (1.6.13), q   k  , with the energy

balance equation (1.6.19), div qr , and assuming the conductivity is constant, leads to

k   r. Now

2 3

2

2 2

2

2 1

2

2

2

x x x

x x x x xi

ij i j

j i j

i

 e e

1 2 3

x   x x^ x  x

time t

time t  t

v ( x , t )

v ( x , t  t )

field. The paddle wheel would remain stationary in regions where curl v  0 , in which

case the velocity field v is called irrotational.

1.6.9 Identities

Here are some important identities of vector calculus {▲Problem 8}:

 u v  u v

u v u v

curl curl curl

div div div

grad grad grad

div grad grad grad

divcurl 0

curlgrad

div curl curl

curl curl grad

div div grad

grad( ) grad grad

2    

u

o

u v v u u v

u u u

u u u

1.6.10 Cylindrical and Spherical Coordinates

Cartesian coordinates have been used exclusively up to this point. In many practical

problems, it is easier to carry out an analysis in terms of cylindrical or spherical

coordinates. Differentiation in these coordinate systems is discussed in what follows

10 .

Cylindrical Coordinates

Cartesian and cylindrical coordinates are related through (see Fig. 1.6.8)

z z

y r

x r

sin

cos

z z

y x

r x y

 tan /

1

2 2

Then the Cartesian partial derivatives become

y r y r r

r

y

x r x r r

r

x

cos sin

sin cos

(^10) this section also serves as an introduction to the more general topic of Curvilinear Coordinates covered

in §1.16-§1.

Figure 1.6.8: cylindrical coordinates

The base vectors are related through

z z

y r

x r

e e

e e e

e e e

sin cos

cos sin

z z

x y

r x y

e e

e e e

e e e

 sin cos

cos sin

so that from Eqn. 1.6.14, after some algebra, the Nabla operator in cylindrical coordinates

reads as {▲Problem 9}

r r z

r z

  e e e

which allows one to take the gradient of a scalar field in cylindrical coordinates:

r z r r z

e e e

Cartesian base vectors are independent of position. However, the cylindrical base

vectors, although they are always of unit magnitude, change direction with position. In

particular, the directions of the base vectors e r , e  depend on  , and so these base

vectors have derivatives with respect to  : from Eqn. 1.6.29,

r

r

e e

e e

with all other derivatives of the base vectors with respect to r ,  , z equal to zero.

The divergence can now be evaluated:

x (^) 1  x

x (^) 2  y

x (^) 3  z

 x , y , z   r , , z 

 r^

e x

e z

e y

e z

e r

e

r

r

e e

e e

 ,

 

 

  

 

 

e e e

e e

e e

sin cos

cos

sin

r

r

and it can then be shown that {▲Problem 11}

   

2

2

2 2 2 2

2

2 2

2 2

2 2

sin

2 1 cot 1

sin

sin sin

sin

 

 

r r r r r r

v

r

v r

r v r r

r r r

r

r

v

e e e

1.6.11 The Directional Derivative

Consider a function    x. The directional derivative of  in the direction of some vector

w is the change in  in that direction. Now the difference between its values at position

x and xw is, Fig. 1.6.10,

d  ^ ^ x  w ^    x (1.6.39)

Figure 1.6.10: the directional derivative

x

w

( x )

( x  w )

D w ( x )

An approximation to d  can be obtained by introducing a parameter  and by

considering the function   x   w ; one has   x   w    0    x and

  x   w   1  x  w .

If one treats  as a function of  , a Taylor’s series about   0 gives

 (^)  0

2

2 2

 

d

d

d

d

or, writing it as a function of x   w ,

x w x  x  w

 0

d

d

By setting   1 , the derivative here can be seen to be a linear approximation to the

increment d  , Eqn. 1.6.39. This is defined as the directional derivative of the function

 ( x )at the point x in the direction of w , and is denoted by

x w ^  x^  w 

 0

[ ]

d

d The Directional Derivative (1.6.40)

The directional derivative is also written as D w  x .

The power of the directional derivative as defined by Eqn. 1.6.40 is its generality, as seen

in the following example.

Example (the Directional Derivative of the Determinant)

Consider the directional derivative of the determinant of the 2  2 matrix A , in the

direction of a second matrix T (the word “direction” is obviously used loosely in this

context). One has

11 22 2211 12 21 2112

11 11 22 22 12 12 21 21 0

0

det [ ] det

A T A T AT A T
A T A T A T A T

d

d

d

d

    

 

A A T A^ T

The Directional Derivative and The Gradient

Consider a scalar-valued function  of a vector z. Let z be a function of a parameter  ,

   z 1  , z 2  , z 3   . Then

A field is a function which is defined in a Euclidean (point) space

3 E. A scalar field is

then a function f ER

3 :. A scalar field is differentiable at a point

3 xE if there

exists a vector Df   x  E such that

fxh   f   xDf   xhoh  for all hE (1.6.46)

In that case, the vector Df   x is called the derivative (or gradient ) of f at x (and is given

the symbol  f   x ).

Now setting h   w in 1.6.46, where wE is a unit vector, dividing through by  and

taking the limit as   0 , one has the equivalent statement

  x w  x  w 

 (^) 

f d

d f

0

for all wE (1.6.47)

which is 1.6.41. In other words, for the derivative to exist, the scalar field must have a

directional derivative in all directions at x.

Using the chain rule as in §1.6.11, Eqn. 1.6.47 can be expressed in terms of the Cartesian

basis  e i ,

  i j j

i

i i

w x

f w x

f f x w ee

This must be true for all w and so, in a Cartesian basis,

  i

xi

f f x e

which is Eqn. 1.6.9.

1.6.13 Problems

  1. A particle moves along a curve in space defined by

      (^3)

2 3 2

2 1

3 rt  4 t et  4 t e  8 t  3 t e

Here, t is time. Find

(i) a unit tangent vector at t  2

(ii) the magnitudes of the tangential and normal components of acceleration at t  2

2. Use the index notation (1.3.12) to show that   a

a v vav    dt

d

dt

d

dt

d

. Verify this

result for (^12)

2 3

2 v  3 t e (^) 1  t e , at et e. [Note: the permutation symbol and the unit

vectors are independent of t ; the components of the vectors are scalar functions of t

which can be differentiated in the usual way, for example by using the product rule of

differentiation.]

3. The density distribution throughout a material is given by   1  x  x.

(i) what sort of function is this?

(ii) the density is given in symbolic notation - write it in index notation

(iii) evaluate the gradient of 

(iv) give a unit vector in the direction in which the density is increasing the most

(v) give a unit vector in any direction in which the density is not increasing

(vi) take any unit vector other than the base vectors and the other vectors you used

above and calculate d  / dx in the direction of this unit vector

(vii) evaluate and sketch all these quantities for the point (2,1).

In parts (iii-iv), give your answer in (a) symbolic, (b) index, and (c) full notation.

  1. Consider the scalar field defined by x 3 yx 2 z

2

(i) find the unit normal to the surface of constant  at the origin (0,0,0)

(ii) what is the maximum value of the directional derivative of  at the origin?

(iii) evaluate d  / dx at the origin if d x  ds ( e 1  e 3 ).

  1. If ux 1 (^) x 2 x 3 e 1  x 1 x 2 e 2  x 1 e 3 , determine div u and curl u.
  2. Determine the constant a so that the vector

v   x 1  3 x 2  e 1  x 2  2 x 3  e 2  x 1  ax 3  e 3

is solenoidal.

  1. Show that curl v  2 ω (see also Problem 9 in §1.1).
  2. Verify the identities (1.6.25-26).
  3. Use (1.6.14) to derive the Nabla operator in cylindrical coordinates (1.6.30).
  4. Derive Eqn. (1.6.34), the curl of a vector and the Laplacian of a scalar in the

cylindrical coordinates.

  1. Derive (1.6.38), the gradient, divergence and Laplacian in spherical coordinates.

12. Show that the directional derivative D v  ( u )of the scalar-valued function of a vector

 ( u ) u  u , in the direction v , is 2 u  v.

  1. Show that the directional derivative of the functional

 

l l

dx pxvxdx dx

d v Uvx EI

0 0

2

2

2

( )( ) 2

in the direction of  ( x )is given by

 

l l

dx px xdx dx

d x

dx

d vx EI

0 0

2

2

2

2

( ) ()