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Rotational Dynamics

Rotational Dynamics
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4 Rotational Dynamics - Internal Motion II
4.1 Measuring Rotational Motion

So far we have looked at the linear and vibrational motion of molecules. we
will now turn to the third form of molecular dynamics, which is to be found in
rotational motion. This is far and away the most difficult form of motion to
analyse, so we will only examine it in a restricted form, that of rigid body
rotating about a fixed axis. For such a system the atoms making up the
molecule follow circular trajectories in a plane perpendicular to the
rotational axis. In other words every atom will rotate in the plane, i.e. it
exhibits two dimensional rotational motion.

As was pointed out at the beginning of this course, in the absence of any
external forces the axis of rotation must pass through the centre of mass.
What we will do now is to derive the centre of mass precisely.

4.1.1The Centre of Mass

Imagine a molecule consisting of j atoms, each of which has a force
Fj acting on it. The subscript j simply identifies the atom
under consideration. This force is of course equal to the atom's mass, mj,
times the acceleration it experiences, d2rj/dt2.

Rotational Dynamics Mi116
(4.1.1).

The total force, F, on the molecule is then the vector sum of
these individual forces.

Rotational Dynamics Mi117
(4.1.2).

Now F is equal to the total external force on the molecule, since
Newton's third law tells us that all the forces exerted by atoms within the
molecule on each other must cancel out; equal and opposite reactions. This
then only leaves the forces exerted on the atoms by external sources.

Now if we symbolise the molecule's mass by M, we can re-express our equation
for the total external force on the molecule by

Rotational Dynamics Mi118
(4.1.3)

were R is the position vector of the point through which the
external forces effectively act, the centre of mass. The position of the
centre of mass is therefore given by


Rotational Dynamics Mi119
(4.1.4).

We are now in a position to be more specific about the utility of the centre of
mass. First, in the absence of any external forces Newton's first law tells us
that this point must be moving with constant velocity dR/dt. Now
the molecule may well be rotating under these conditions (an external agent
must set the rotation in train, but need not be present for the rotation to
continue). In such a case it is clear that this rotation must have the
centre of mass on the axis of rotation, since otherwise dR/dt
will not be constant. Indeed any internal motion in the absence of external
forces must have the centre of mass at this "still" point.

The corollary of all this is that if we use the centre of mass as the origin
for all our measurements of internal motion, such as rotational motion, we can
ignore the motion of the centre of mass itself. Indeed we have already used
this trick in our examination of SHM in a diatomic molecule.

4.1.2 Rotational Kinematics

As with linear motion we must develop the kinematic equations for circular
motion in order to be able to describe the dynamics of rotation. To do this it
is obviously not sensible to use the rectilinear co-ordinates x, y, z, figure
4.1.1.

Since the rotation is about a fixed axis the co-ordinates r and θ will
enable us to specify a particle's angular kinematics. Since we will only
consider a rigid body only the angle θ will vary with time. This means we
need only measure the rate of angular rotation, ω

Rotational Dynamics Mi120
(4.1.5)

and the rate of change of angular rotation, α

Rotational Dynamics Mi121
(4.1.6)

in order to describe the kinematics of such systems. If we measure θ in
radians then ω, the analogue of velocity, has units of radians per second
and α, the analogue of acceleration, has units of radians per second
squared.


Rotational Dynamics Mi122

Figure 4.1.1. Cylindrical co-ordinate system.

This analogue between one dimensional linear kinematics and angular kinematics,
i.e. that θ corresponds to x, ω corresponds to v and α
corresponds to a, makes it extremely easy to write down the kinematic equation
for motion under constant angular acceleration.

Rotational Dynamics Mi123
(4.1.7)


where the subscript zero indicates the value of the appropriate quantity has
been measured at t = 0.

Of course θ, ω and α are actually vectors since they must be
able to indicate the direction of the rotational motion. The sensible place to
put the vectors θ, ω and α
is on the axis of rotation. Having done this the only remaining
decision to be made is in which direction the vectors should point. By
convention we use the right hand screw rule to determine the direction in which
the vectors point, figure 4.1.2.

In the figure the direction of θ and ω
have been determined as follows. The particle is rotating anti-clockwise, if we
were to turn a right handed screw in the same sense it would travel in the
positive z direction. This is the direction in which the vectors must therefore
point by the right hand screw rule. We show α pointing in
the opposite direction, which means that the particle's angular velocity is
slowing down.


Rotational Dynamics Mi124

Figure 4.1.2. Determining the direction of rotation vectors.

In calculations we will want to be able to relate the angular velocity and
acceleration to the instantaneous linear velocity and acceleration of a
particle, figure 4.1.3.


Rotational Dynamics Mi125

Figure 4.1.3. Relating angular and linear kinematic quantities.

The derivation of the relationships between v, at,
ar and ω and α is given
in [[section]]4.1.3, we simply quote the results here and explain their
meaning. The instantaneous velocity is given by

Rotational Dynamics Mi126
(4.1.Cool.

The order of the vector cross product multiplication, ensures that
v points in the correct direction. Remember that the magnitude of
v = ωrsinθ, where θ is the angle between the vectors
ω and r. This means that v is simply ω
times the perpendicular distance from the axis of rotation to the particle. So
even though it make sense to put the origin for the position vector at the
centre of mass, for the purposes of these calculations, it suffices to ensure
that the origin is somewhere along the axis of rotation.

The radial and tangential accelerations are given by

Rotational Dynamics Mi127
(4.1.9).

Once again the magnitude of the tangential acceleration is equal to α
times the perpendicular distance from the rotation axis to the particle and the
radial or centripetal (in towards the centre) acceleration is equal to
ω2 times the perpendicular distance from the axis of rotation
to the particle. More importantly, even if the rate of rotation is constant
there is still a radial or centripetal acceleration. This must be so, because
we are forcing the particle to deviate from a straight path, which according to
Newton's first law can only be done by applying a force and hence imparting an
acceleration.

4.1.3 Relating Angular and Linear Velocity and Acceleration.

In order to examine the dynamics of rotational motion in a molecule we need to
determine the instantaneous acceleration and velocity of the constituent atoms.
We find the appropriate relations in the following manner.


Rotational Dynamics Mi128

Figure 4.1.4. Radial and transverse components in a rotating system.

Figure 4.1.4 shows a particle rotating in a circular path about the z axis in
the x-y plane at a constant radius r. We define two units vectors
er and eθ pointing in the radial and
transverse or tangential directions. So the rectilinear position vector,
r, is given by

r = er r (4.1.10)

and hence the instantaneous velocity of, v, is given by

Rotational Dynamics Mi129
(4.1.11).

Now looking at our vector diagram we can see that to convert this into an
angular velocity ω, we can take advantage of the fact
that

Δer =Δθ (4.1.12),

where we define angles in radians, and the angle is small enough, which it will
be for an instantaneous measurement. Now examination of the vector diagram
should convince you that this change in the radial vector actually points along
the transverse direction and hence we get

Rotational Dynamics Mi130
(4.1.13)

and hence

v = eθ ωr (4.1.14).

To find an expression for the acceleration we simply differentiate this
expression

Rotational Dynamics Mi131
(4.1.15),

but dω/dt is simply the angular acceleration α and you can show, in
the same way that we previously did for der/dt that

Rotational Dynamics Mi132
(4.1.16),

which gives us

a = eθ αr - er
ω2r (4.1.17).

This shows us that the acceleration has a tangential and radial component. The
tangential acceleration at is simply proportional to the angular
acceleration. However, even if α is zero there is a radial acceleration
ar, directed towards the axis of rotation (the negative sign).
The acceleration is called the centripetal acceleration and is present even at
constant angular velocity, because we have to apply a force in order to make a
particle deviate from straight line motion (Newton's first law). In the case of
circular motion at constant angular velocity, the instantaneous rectilinear
velocity is changing in direction, but not magnitude.

We have yet to express the angular kinematic terms as vectors, which we will
need to do in order to understand forces and momenta in rotating systems, since
these are of course vectorial. Let us deal with the instantaneous velocity and
angular velocity first.

The magnitude of the velocity is given by

v = ωr (4.1.18).

Since v and r are vectors and ω should also
be a vector we can see that the only appropriate combination is the vector
cross product, the only remaining ambiguity being the order of the
multiplication. By convention the right hand rule is used, giving us

v = ωxr
(4.1.19).

Remember that this makes the magnitude of v times the sine of the
angle between the vectors w and r. This means that
the magnitude of the velocity is equal to the angular velocity times the radial
distance between the axis of rotation and the moving particle. The radial and
tangential acceleration then follow

at = α xr
(4.1.20)
ar = ω x v (4.1.21).

4.2 Torque and Angular Momentum

We now have kinematic equations for rotational motion, so we are equipped to
look at the dynamics of rotation. What we will find is that there are direct
parallels between the equations of linear dynamics and those for rotational
dynamics. This is not a great surprise, since rotational dynamics is in fact
only a re-expression of linear dynamics in a rotating frame. Those analogues
are summarised below.

Linear Dynamics Rotational Dynamics
v / ω

a / α

m / I

F = ma / τ =
Iα

p = mv / L =
Iω

dWlin = F * ds / dWrot =
τ * dθ

Klin = 1/2 mv2 / Krot = 1/2 Iω2.


Let us start by looking at the rotational analogue of force, the torque (from
torquere, the Latin for twist).

4.2.1 Defining the Torque and the Moment of Inertia

Everyday experience tells us that the action which causes an extended object to
rotate depends both on the magnitude of the applied force and the distance from
the axis of rotation. If you want to push open a door, you apply the force at
the edge of the door furthest from the hinge. In this way you maximise the
turning effectiveness of your push or pull. If you try opening the door by
applying a force close to the hinge you will find the effort required is far
greater. Clearer the further away you are from the axis of rotation the greater
the effect of a given force. So we would guess that the torque, τ, is
related to the force, F, by

τ = rF (4.2.1),

where r is the perpendicular distance from the axis of rotation to the point at
which the force was applied.

So far we have not determined the vectorial nature of the torque. We can
determine this when we note that only the component of force acting
tangential, Ft, to the direction of rotation is used to cause the
rotation, figure 4.2.1. Returning to the example of a door, this is simply
saying that if you apply the force along the door face you will not make it
turn at all, whereas if you apply the force at right angles to the door face
you maximise the efficiency with which you turn it.


Rotational Dynamics Mi133

Figure 4.2.1. Only the component of the force perpendicular to
r, Ft is used in turning
the particle about the axis of rotation.


This means we would now conclude that

τ = rF sinθ (4.2.2),

where θ is the angle between the position vector and the force vector,
figure 4.2.1. Putting this into vectorial language

τ = rxF (4.2.3)

and the vectorial construction once again follows the right hand rule. Of
course in a molecular calculation the total torque, Τ, is the
sum of the torque on each atom


Rotational Dynamics Mi134
(4.2.4),

where the subscript j identifies the jth atom. Clearly the value of the torque
will in general depend on the location we choose as the origin of our
co-ordinate system. It is best therefore to choose the centre of mass as the
origin for our measurements, although it is well to note that in conditions
where the net force on the molecule is zero, i.e. in conditions where the
external forces only cause rotational motion, the value of the total torque is
equivalent from whatever point the measurements are made.

Since we now have the rotational analogue of the force, we will derive the
equation which would be analogous to F = ma.
Consider the case of a torque applied to a mass, m, at a distance r from the
axis of rotation, where θ = π/2.


Rotational Dynamics Mi135

Figure 4.2.2. Deriving the moment of inertia.

In this case the magnitude of the torque is

τ = rF (4.2.5),

but the applied force, F, is equal to the particle's mass times the tangential
acceleration (since r is constant). Therefore

τ = rmat (4.2.6),

but at = αr and therefore

τ = mr2α (4.2.7).

Now mr2 is called the moment of inertia, I, which is the rotational
analogue of the inertial mass in linear motion. In other words the larger the
moment of inertia the harder it is to get the object to change its angular
velocity. In full vectorial form we have

τ = I α (4.2.Cool

and if you check you can see that this expression is consistent with the
direction of vector cross product r x F .

In all the cases of interest to us there will be more than one mass to consider
in calculations of the effect of a torque applied to a molecule, so we must
generalise the moment of inertia for a system of connected masses (atoms)

Rotational Dynamics Mi136
(4.2.9),

where rj is the perpendicular distance of the jth atom to the axis of
rotation.

4.2.2 Turning a Molecule - The Dipole in an Electrostatic Field

A dipolar molecule in the presence of an electrostatic field will, in general,
experience a torque. We will calculate this torque for a diatomic dipolar
molecule in a uniform electrostatic field, figure 4.2.3.


Rotational Dynamics Mi137

Figure 4.2.3. An electrostatic dipole in a uniform electric field. The
distance between the dipole charges is 2l.


There is no net force on the dipole, but there is a torque. We will determine
the torque exerted by the field on each charge, measured about the centre of
mass, using the fact that the magnitude of the torque is given by the product
of the distance to the charge and the tangential force. The distance to the
centre of mass is given by (2.1.1) and hence we find the total torque
Τ to be

Rotational Dynamics Mi138
(4.2.10).

The torque vector is into the paper, since the turning action is clockwise and
a right handed screw would travel in this direction. Noting that
cos(π/2-θ) = sinθ, (4.2.10) reduces to

Rotational Dynamics Mi139
(4.2.11)

and we note that 2lq is the magnitude of the dipole moment, which
suggests that the torque is the vector product of P and the field
E. The appropriate order of vector product is

Rotational Dynamics Mi140
(4.2.12)

and indeed this is always the torque on an electrostatic dipole in a uniform
electric field.

The torque on the dipole depends on sinθ. This means that the force is
zero at θ = 0 and π, i.e. the dipole is in equilibrium with
P parallel and anti-parallel to E. The difference
in these two positions, is that only the parallel state is in stable
equilibrium.

4.2.3 Defining the Angular Momentum

We now derive the most important rotational quantity in dynamics, the angular
momentum, L, the analogue of linear momentum. Now we already know
that F = dp/dt so we should have exactly such a
correspondence between the torque and the angular momentum, i.e.

Rotational Dynamics Mi141
(4.2.13).

This expresses the fact that the total angular momentum of a molecule (found by
summing the individual momenta of the constituent atoms) is constant unless an
external torque is applied. In other words we have identified an important
conservation law, that in the absence of any external torques, the angular
momentum of an isolated system is always conserved. Put into mathematical
terms

Rotational Dynamics Mi142
(4.2.14),

where Lij is the initial angular momentum of the jth atom and
Lfj is the final momentum of the jth atom.

Since the torque τ = r x F we
anticipate that L = r x p. We can
check this by re-expressing τ = dL/dt as

Rotational Dynamics Mi143
(4.2.15)

and we can confirm the validity of our expression relating torque and angular
momentum by doing the differentiation

Rotational Dynamics Mi144
(4.2.16)

and noting that v x v must be zero, which returns
us to the original expression and confirms that the angular momentum is given
by

L = r x p (4.2.17).

Now we can derive the analogue of p = mv, which we
anticipate will be L = Iω, for the angular
momentum. For simplicity, but without loss of generality, we set
r in the rotational plane of the particle. Recalling that
v = ω x r and substituting into
our expression for L, we get L = r x
(mω x r). This has a magnitude
mr2ω and inspection of the vector diagram, figure 4.2.4, shows
that the resultant vector points in the same direction as
ω, hence

L = Iω (4.2.18).

So we now see that, as we would have expected, the analogy between linear
momentum p = mv, and angular momentum is exact (
with I and ω replacing m and v).


Rotational Dynamics Mi145

Figure 4.2.4. The vectorial construction used to determine
l = Iω.

4.2.4 Dipole Oscillations

We have seen how a diatomic molecule stretched along its long axis will
oscillate. We now show that a dipolar molecule in the presence of an electric
field may also execute rotational oscillations.

We return to the example given in [[section]]4.2.2 and note that in order to
perturb the dipole away from the stable equilibrium position at θ = 0 we
would have to apply a torque, τa, equal but opposite to the
torque due to the field

Rotational Dynamics Mi146
(4.2.19).

According to (4.2.13) this applied torque is equal to the rate of change in
angular momentum, L. Since the bond length does not change,
neither can the moment of inertia I, so dL/dt = I
dω/dt = I d2θ/dt2
and hence we have

Rotational Dynamics Mi147
(4.2.20),

where I have removed the vector notation since α and
θ point along the same axis. When the perturbation is small
sinθ ~ θ and hence we have

Rotational Dynamics Mi148
(4.2.21)

which is a very simple second order differential equation, the solution of
which is θ = θ0sin(ωt+φ), where ω =
[[radical]](PE/I) and θ0 is the angular amplitude. In other words we have
simple harmonic oscillations whose period does not depend on the amplitude
θ0.

4.3 Rotational Energetics

4.3.1 Rotational Work, Potential and Kinetic Energy

Finally we will look at the energetics involved in rotating a molecule.
Continuing our analogies to linear dynamics, the work done in rotating a
molecule through an angle dθ by the action of an external
torque will be given by

dWrot =τ *dθ (4.3.1),

which is directly analogues to the definition of work for a linear
displacement, with the force being replaced by torque and linear displacement
being replaced by angular displacement.

By extension we may then also deduce that the potential energy associated with
rotating the molecule is given by

dUrot = -τ *dθ (4.3.2).

The kinetic energy of a particle of mass m moving in a straight line is 1/2
mv2. If the particle moves in a circle we know that v = ωr and
hence we would expect the rotational kinetic energy to be

Krot = 1/2 mω2r2 = 1/2 Iω2
(4.3.3)

and once again the moment of inertia replaces the inertial mass and ω
replaces v.

We now have the means to solve dynamical problems in rotation using the
conservation of energy and the conservation of angular momentum.

4.3.4 Energy of the Oscillating Dipole

Let us return to the case of a dipole in a uniform electric field
[[section]]4.2.2 and determine the energetics of the small rotational
oscillations. We first determine the potential energy of the dipole at an angle
θ away from stable equilibrium. A torque would be needed to hold the
dipole at the angle θ which was equal and opposite to the torque produced
by the field, i.e. the holding torque would be -PEsinθ. Hence the
potential energy is given by

Rotational Dynamics Mi149
(4.3.4).

For small perturbations from equilibrium sinθ ~ θ. Using this
approximation in the integral gives the following relationship

Rotational Dynamics Mi150
(4.3.5).

The total energy of the system will include the kinetic energy, 1/2
2. Hence the total energy H is given by

Rotational Dynamics Mi151
(4.3.6)

which has exactly the same mathematical form as the total energy of the simple
harmonic oscillator (see equation (3.1.11)). So as we have already seen in
[[section]] 4.2.4, the dipole will execute simple harmonic oscillations with
period T = 2π [[radical]](I/PE).

4.3.2 The Oscillating and Rotating Diatomic Molecule

In general molecules will have translational, vibrational and rotational
motion. Since the translational motion can be de coupled from the internal
ones, we will now examine a simple case of a homonuclear, diatomic molecule
which is both rotating and vibrating. To simplify the problem we have the
molecule rotating orthogonally to its molecular axis and vibrating along it,
figure 4.3.1.


Rotational Dynamics Mi152

Figure 4.3.1. The rotating and vibrating diatomic molecule.

No external forces are applied during the vibrational movement of the atoms
from the radial distance r1 to r2. Therefore the initial and final angular
momenta, L1 and L2 respectively, must be equal. However, changing the radial
separation of the atoms alters the moment of inertia. Hence according to the
relationship L = Iω, ω must alter, from ω1 to ω2 to
preserve the value of L. For atoms of equal mass, m we then have

Rotational Dynamics Mi153
(4.3.7)

which re-arranges to give

Rotational Dynamics Mi154
(4.3.Cool

where we have omitted the vectorial notation, since the direction of rotation
does not alter. Clearly since r1>r2, we have that ω2>ω1. In
other words as the atoms come closer together the rotation rate speeds up and
as they part company the rotation rate slows down.

It is interesting to note that although the angular momentum is conserved, we
can show that the rotational kinetic energy, K, is not.

Rotational Dynamics Mi155
(4.3.9),

where K2 is the kinetic energy at position r2 and K1 is that at r1. We simplify
this expression by noting that since the angular momentum is conserved we may
substitute for ω2 by L/2mr2, to give

Rotational Dynamics Mi156
(4.3.10)

which is true for r1
Rotational Dynamics Mi157
r2.

This is actually not too mystifying when you think about it, since moving the
atoms inwards takes work. In other words the total energy is conserved, we have
just forgotten to take into account the change in potential energy.

The work can be found as follows. An inward radial force, magnitude F, must be
exerted to keep the atoms moving in a circular path. This force is equal to the
centripetal acceleration times the mass of the atom. For one atom

F = mω2r (4.3.11).

Now as the atoms are pulled in the force and displacement are in the same
direction and so the work done on one atom is simply

Rotational Dynamics Mi158
(4.3.12),

but ω varies with r so we will substitute for ω again using the
invariant L= 2mr2ω (in our case). The potential energy change
is the negative of the work and remembering that there are two atoms we get

Rotational Dynamics Mi159
(4.3.13).

So we now have (U2 - U1) + (K2 - K1) = 0 as required!

The diatomic molecule will clearly change its rate of rotation exactly in time
with the natural frequency of the vibrational oscillations. The motions are
coupled.



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