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Physics 3309 Homework 13
Chapter 11
11-27.
Initially:
Thus
(1)
From Eq. (11.102)
Since , we have
(2)
From Eq. (11.131)
(2) becomes
(3)
From (1), we may construct the following triangle
from which
Substituting into (3) gives
11-29. When the motion is vertical q = 0. Then, according to Eqs. (11.153) and (11.154),
(1)
and using Eq. (11.159), we see that
(2)
Also, when q = 0 (and ), the energy is [see Eq. (11.158)]
(3)
Furthermore, referring to Eq. (11.160),
(3)
If we wish to examine the behavior of the system near q = 0 in order to determine the conditions for stability, we can use the values of , , and E¢ for q = 0 in Eq. (11.161). Thus,
(5)
Changing the variable to z = cos q and rearranging, Eq. (5) becomes
(6)
The questions concerning stability can be answered by examining this expression. First, we note that for physically real motion we must have . Now, suppose that the top is spinning very rapidly, i.e., that is large. Then, the term in the square brackets will be negative. In such a case, the only way to maintain the condition is to have z = 1, i.e., q = 0. Thus, the motion at q = 0 will be stable as long as
(7)
or,
(8)
Suppose now that the top is set spinning with q = 0 but with sufficiently small that the condition in Eq. (8) is not met. Any small disturbance away from q = 0 will then give a negative value and q will continue to increase; i.e., the motion is unstable. In fact, q will continue until z reaches a value that again makes the square brackets equal to zero. This is a turning point for the motion and nutation between z = 1 and will result.
From this discussion it is evident that there exists a critical value for the angular velocity, , such that for the motion is stable and for there is nutation:
(9)
If the top is set spinning with and q = 0, the motion will be stable. But as friction slows the top, the critical angular velocity will eventually be reached and nutation will set in. This is the case of the “sleeping top.”
Chapter 12
12-1.
The equations of motion are
(1)
We attempt a solution of the form
(2)
Substitution of (2) into (1) yields
(3)
In order for a non-trivial solution to exist, the determinant of coefficients of and must vanish. This yields
(4)
from which we obtain
(5)
This result reduces to for the case (compare Eq. (12.7)].
If were held fixed, the frequency of oscillation of would be
(6)
while in the reverse case, would oscillate with the frequency
(7)
Comparing (6) and (7) with the two frequencies, and , given by (5), we find
(8)
so that
(9)
Similarly,
(10)
so that
(11)
If , then the ordering of the frequencies is
12-7.
We define the coordinates and as in the diagram. Including the constant downward gravitational force on the masses results only in a displacement of the equilibrium positions and does not affect the eigenfrequencies or the normal modes. Therefore, we write the equations of motion without the gravitational terms:
(1)
Assuming a harmonic time dependence for and in the usual way, we obtain
(2)
Solving the secular equation, we find the eigenfrequencies to be
(3)
Substituting these frequencies into (2), we obtain for the eigenvector components
(4)
For the initial conditions , the normal coordinates are
(5)
Therefore, when , and the system oscillates in Mode 1, the antisymmetrical mode. When , and the system oscillates in Mode 2, the symmetrical mode.
When mass 2 is held fixed, the equation of motion of mass 1 is
(6)
and the frequency of oscillation is
(7)
When mass 1 is held fixed, the equation of motion of mass 2 is
(8)
and the frequency of oscillation is
(9)
Comparing these frequencies with and we find
Thus, the coupling of the oscillators produces a shift of the frequencies away from the uncoupled frequencies, in agreement with the discussion at the end of Section 12.2.
12-9. The general solutions for and are given by Eqs. (12.10). For the initial conditions we choose oscillator 1 to be displaced a distance D from its equilibrium position, while oscillator 2 is held at , and both are released from rest:
(1)
Substitution of (1) into Eq. (12.10) determines the constants, and we obtain
(2)
(3)
where
(4)
As an example, take ; vs. is plotted below for this case.
It is possible to find a rotation in configuration space such that the projection of the system point onto each of the new axes is simple harmonic.
By inspection, from (2) and (3), the new coordinates must be
(5)
(6)
These new normal axes correspond to the description by the normal modes. They are represented by dashed lines in the graph of the figure.
12-17.
Following the procedure outlined in section 12.6:
Thus
Thus we must solve
This reduces to
or
If the first term is zero, then we have
If the second term is zero, then
which leads to
To get the normal modes, we must solve
For k = 1 this gives:
Substituting for each value of r gives
Doing the same for k = 2 and 3 yields
The equations
can thus be written as
We get the normal modes by solving these three equations for , , :
and
The normal mode motion is as follows
12-19. With the given expression for U, we see that has the form
(1)
The kinetic energy is
(2)
so that is
(3)
The secular determinant is
(4)
Thus,
(5)
This equation is of the form (with )
(6)
which has a double root if and only if
(7)
Therefore, (5) will have a double root if and only if
(8)
This equation is satisfied only if
(9)
Consequently, there will be no degeneracy unless the three coupling coefficients are identical.
12-23. The total energy of the r-th normal mode is
(1)
where
(2)
Thus,
(3)
In order to calculate and , we must take the squares of the real parts of and :
(4)
so that
(5)
Also
(6)
so that
(7)
Expanding the squares in and , and then adding, we find
Thus,
(8)
So that the total energy associated with each normal mode is separately conserved.
For the case of Example 12.3, we have for Mode 1
(9)
Thus,
(10)
Therefore,
(11)
But
(12)
so that
(13)
which is recognized as the value of the potential energy at t = 0. [At t = 0, , so that the total energy is .]
At this point, you can go to the 3309 page,
the UH Space Physics Group
Web Site, or my personal Home Page.
Edgar A. Bering, III ,
Edgar A. Bering, III , <eabering@uh.edu>
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