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PC235 Winter 2013

Classical Mechanics

Assignment #9 Solutions

#1 (10 points) JRT Prob. 11.2

A massless spring (force constant k1) is suspended from the ceiling,

with a mass m1 hanging from its lower end. A second massless spring (force

constant k2) is suspended from m1, and a second mass m2 is suspended from

the second spring’s lower end. Assuming that the masses move only in a vertical direction and using coordinates y1 and y2 measured from the masses’

equilibrium positions, show that the equations of motion can be written in the matrix form M¨y = −Ky, where y is the 2 × 1 column made up of y1

and y2. Find the matrices M and K.

Solution

Let ˆy1 and ˆy2 be the extensions of the two springs from their unstretched

lengths and y10 and y20 be their values at equilibrium. The displacements

from equilibrium are

y1 = ˆy1− y10 and y2 = ˆy2− y20. (1)

The net downward forces on the two masses are

F1 = m1g − k1yˆ1 + k2(ˆy2− ˆy1) and F2 = m2g − k2(ˆy2− ˆy1), (2)

and thus the conditions for equilibrium are

m1g = k1y10= k2(y20− y10) and m2g = k2(y20− y10). (3)

Now, applying Newton’s 2nd law and using eq. (1) to eliminate ˆy1 and ˆy2

from eq. (2), we find that

m1y¨1 = F1 = m1g − k1(y1+ y10) + k2[y2− y1+ (y20− y10)] (4)

= −k1y1+ k2(y2− y1) (5)

(the equilibrium condition is used to eliminate several terms in the last line.) Similarly,

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The last two results combine to give the matrix equation M¨y= −Ky, where M= m1 0 0 m2  and K = k1+ k2 −k2 −k2 k2  . (7) #2 (15 points) JRT Prob. 11.10

(a) Write down the equations of motion corresponding to eq. (11.2) for the case of two equal-mass carts with three identical springs, but with each cart subjected to a linear resistive force −bv (same coefficient b for both carts).

(b) Show that if you change variables to the normal coordinates ξ1 = 12(x1+

x2) and ξ2 = 12(x1 − x2), the equations of motion for ξ1 and ξ2 are

uncoupled.

(c) Write down the general solutions for the normal coordinates and hence for x1 and x2 (assume that b is small, so that the oscillations are

un-derdamped.)

(d) Find x1(t) and x2(t) for the initial conditions x1(0) = A and x2(0) =

v1(0) = v2(0) = 0, and plot them for 0 ≤ t ≤ 10π using the values

A = k = m = 1, b = 0.1. Solution

(a) As in section 5.4, we define β = b/2m and ω2

0 = k/m. Then, the

equations of motion are

¨

x1 = −2β ˙x1− 2ω20x1+ ω02x2

¨

x2 = −2β ˙x2+ ω20x1− 2ω02x2.

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(b) If you take first the sum and then the difference of these two equations, you will get the uncoupled equations

¨

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(c) The equation for ξ1 is exactly the equation (5.28) that we found for

a single damped oscillator, and has the solution (5.37), which we can rewrite as

ξ1(t) = e−βt(B1cos ω1t + C1sin ω1t), where ω1 =

q ω2

0 − β2 (10)

ξ2(t) = e−βt(B2cos ω2t + C2sin ω2t), where ω2 =

q 3ω2

0 − β2. (11)

The expressions for x1(t) and x2(t) follow at once by adding and

sub-tracting these expressions for ξ1(t) and ξ2(t).

(d) The given initial conditions imply that ξ1(0) = ξ2(0) = A/2, with

both derivatives zero. Therefore, B1 = B2 = A2, C1 = βA/2ω1, and

C2 = βA/2ω2, from which we can write down

ξ1(t) = A 2e −βt  cos ω1t + β ω1 sin ω1t  (12) ξ2(t) = A 2e −βt  cos ω2t + β ω2 sin ω2t  . (13)

The sum and difference of these two functions give us x1(t) and x2(t),

which are plotted below.

0 5 10 15 20 25 30 −1 −0.5 0 0.5 1 t x 1 0 5 10 15 20 25 30 −1 −0.5 0 0.5 1 t x 2

Fig. 1: x1(t) and x2(t) for question #2

#3 (15 points) JRT Prob. 11.18

Two equal masses m are constrained to move without friction, one on the positive x axis and one on the positive y axis. They are attached to two identical springs (force constant k) whose other ends are attached to the origin. In addition, the two masses are connected to each other by a third spring of force constant k′. The springs are chosen so that the system is

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in equilibrium with all three springs relaxed (length equal to unstretched length). What are the normal frequencies? Find and describe the normal modes. Consider only small displacements from equilibrium.

y x L L O k k k’

Fig. 2: Geometry for Question #3

Solution

Let the equilibrium length of the first 2 springs be L and that of the one that connects the two masses be √2L. Let x and y be the displacements of the two masses from their equilibrium positions; these will be our two generalized coordinates. The total KE is T = 1

2m( ˙x

2+ ˙y2) and the total PE

is U = 12k(x2 + y2) + 1 2k′z

2, where z is the extension of the diagonal spring

(which is a function of x and y; that will take a bit of work to figure out). Since we are interested only in small oscillations, we can write

z =p(L + x)2+ (L + y)22L ≈ p2L2+ 2L(x + y) −2L (14)

= √2Lp1 + (x + y)/L − 1(15) ≈ √2L ·1

2(x + y)/L, (16) where for the last expression on the first line we dropped terms higher than 1st order in x and y and for the final expression we used the binomial expan-sion for the square root. Therefore, we can write z2 = (x + y)2/2, and the

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total PE is U = 1 2k(x 2+ y2) + 1 4k ′(x + y)2 = 1 2  k + k ′ 2  x2+  k + k ′ 2  y2+ k′xy  . (17) Writing down Lagrange’s equations for x and y leads to

M = m 0 0 m  and K = k + k′ 2 k′ 2 k′ 2 k + k′ 2  . (18)

Next, we set det(K − ω2M) = 0, or (mω2

− k)(mω2− k − k′) = 0. Thus, the

normal frequencies are

ω1 =

r k

m and ω2 =

r k + k′

m . (19)

For the first normal mode, solving (K − ω2

1M)a = 0 gives a1 = −a2; the

masses oscillate with equal amplitudes but out of step. In this mode, the diagonal spring’s length remains constant (at least in the small-oscillation approximation), which is why k′ is irrelevant to ω

1. For the second normal

mode, we have a1 = a2. Here, the masses move with equal amplitudes and

both in step (both x and y increase together and decrease together). In this mode, the diagonal spring does stretch and compress; this extra contribution to the PE increases the frequency of oscillations.

#4 (10 points) JRT Prob. 11.26

A bead of mass m is threaded on a frictionless circular wire hoop of radius R and mass m. The hoop is suspended at the point A and is free to swing in its own vertical plane as shown in Fig. 11.20 of the text. Using the angles φ1 and

φ2 as generalized coordinates, solve for the normal frequencies of small

oscil-lations, and find and describe the motion in the corresponding normal modes.

Solution

The moment of inertia of the hoop about its edge is I = 2mR2, so its kinetic

energy is T1 = 1 2I ˙φ 2 1 = mR2φ˙21. (20)

The velocity of the bead is (for small oscillations) the sum of the velocity of the bead relative to the hoop’s center and the velocity of the hoop’s center

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relative to the pivot point. Thus, the bead’s speed is equal to R ˙φ1+ ˙φ2

 . The total kinetic energy is therefore

T = 1 2mR 23 ˙φ2 1+ 2 ˙φ1φ˙2+ ˙φ22  . (21)

The total potential energy is

U = U1+ U2 (22)

= mgR (1 − cos φ1) + mgR [(1 − cos φ1) + (1 − cos φ2)] (23)

≈ 12mgR 2φ21+ φ22

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(we attribute the entire mass of the hoop to a point at its CM). Therefore, the matrices are

M= mR2 3 1 1 1  and K = mR2ω20 2 0 0 1  , (25) where ω2

0 = g/R. Setting the determinant of K − ω2M to zero, we find the

normal frequencies ω1 = 1 √ 2ω0 and ω2 = √ 2ω0. (26)

The first leads to the normal mode where the angles oscillate in phase with equal amplitudes. The second leads to the normal mode where the angles oscillate 180 degrees out of phase with the amplitude of φ2 twice that of φ1.

#5 (10 points) JRT Prob. 11.31

Consider a frictionless rigid horizontal hoop of radius R. Onto this hoop I thread three beads with masses 2m, m, and m, and, between the beads, three identical springs, each with force constant k. Solve for the three normal fre-quencies and find and describe the three normal modes.

Solution

This problem is best solved using Lagrangian methods. The masses are con-strained to move along a circular arc of radius R. Therefore, the speed of

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mass i is R ˙φi, and the total kinetic energy is T = 1 2  2mR ˙φ1 2 + mR ˙φ2 2 + mR ˙φ3 2 (27) = 1 2mR 22 ˙φ2 1+ ˙φ22+ ˙φ23  . (28)

The three springs contribute to the potential energy. We have U = 1 2kR 2(φ 1− φ2)2+ (φ2− φ3)2 + (φ3− φ1)2  (29) = kR2 φ21+ φ22 + φ23− φ1φ2− φ2φ3− φ3φ1 . (30)

The Lagrangian is then

L = T − U (31) = 1 2mR 22 ˙φ2 1+ ˙φ22+ ˙φ23  − kR2 φ21+ φ22+ φ23− φ1φ2− φ2φ3− φ3φ(32)1 .

This leads to the Lagrange’s equations ∂L ∂φ1 = d dt ∂L ∂ ˙φ1 = −kR2(2φ1− φ2− φ3) = 2mR2φ¨1 (33) ∂L ∂φ2 = d dt ∂L ∂ ˙φ2 = −kR2(−φ1+ 2φ2− φ3) = mR2φ¨2 (34) ∂L ∂φ3 = d dt ∂L ∂ ˙φ3 = −kR2(−φ1− φ2+ 2φ3) = mR2φ¨3. (35)

We can immediately cancel out the R2 terms from all equations. Then, the

equations become M ¨φ= −Kφ, where M=   2m 0 0 0 m 0 0 0 m   and K =   2k −k −k −k 2k −k −k −k 2k  . (36)

We then need to find all ω such that det(K−ω2M) = 0. We start by dividing

this matrix by m and making the substitution k/m = ω2 0 = 1: K− ω2M =   2k − 2mω2 −k −k −k 2k − mω2 −k −k −k 2k − mω2   (37) =   2(1 − ω2) −1 −1 −1 2 − ω2 −1 −1 −1 2 − ω2  . (38)

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The characteristic equation is found by setting the determinant of this matrix to zero. The algebra proceeds as follows:

det(K − ω2M) = (2 − 2ω2)(2 − ω2)2− 1 + 1 −(2 − ω2) − 1 − 1 1 + (2 − ω2) = (2 − 2ω2)3 − 4ω2+ ω4 − (2 − ω2 ) − 1 − 1 − (2 − ω2) = (2 − 2ω2)3 − 4ω2+ ω4 − 6 + 2ω2 = −2(ω6− 5ω4+ 6ω2) = 0 (39) This produces the characteristic equation ω6

− 5ω4+ 6ω2 = 0. Since there is

no constant term on the left-hand side, one “obvious” normalized frequency is ω1 = 0. Factoring this solution out gives us the quadratic equation ω4−

5ω2+ 6 = 0, which gives usω

2 =p2k/m and ω3 =p3k/m. By substituting

ω1 = 0 into the equation (K − ω2M)a = 0, we find that a1 = a2 = a3. That

is, the masses move with constant speed around the hoop at their equilibrium separation (and hence none of the springs are ever stretched or compressed -thus the zero frequency). For ω2, we find thata1 = −a2 = −a3; here, mass 1

oscillates in one direction while the other two oscillate in the other direction (all amplitudes being equal). For ω3,a1 = 0 and a2 = −a3. Here, the heavier

mass is stationary while the other two oscillate with equal amplitudes and completely out of phase. These solutions are similar to those found for the linear triatomic molecule in the class notes.

#6 (5 points) JRT Prob. 10.15

(a) Write down the integral for the moment of inertia of a uniform cube of side a and mass M , rotating about an edge, and show that it is equal to 2

3M a

2. (1 point)

(b) If I balance this cube on an edge in unstable equilibrium on a rough table, it will eventually topple and rotate until it hits the table. By considering the energy of the cube, find its angular velocity just before it hits the table. (4 points)

Solution

(a) This is example 10.2 from the text. For a uniform solid cube rotating around its edge, I = 23M a2.

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(b) The initial energy of the cube is pure PE, since there is no motion. Recall that we calculate the PE of a continuous body by the equivalent notion that its entire mass is located at its CM. The CM of a cube is at its center, which is a height a/√2 above the table when the cube is at equilibrium on its edge. Just before it hits the table, its CM is a/2 above the table. Thus, the change in PE is

∆U = M g  a √ 2 − a 2  = M ga 2 ( √ 2 − 1). (40) This energy has all been converted into rotational kinetic energy, T =

1 2Iω 2. Therefore, 1 2Iω 2 = 1 3M a 2ω2 = M ga 2 ( √ 2 − 1) (41)

which is solved to give

ω =r 3g

2a( √

2 − 1). (42)

#7 (10 points) JRT Prob. 10.16

Find the moment of inertia for a uniform cube of mass M and edge a as in Problem 10.15, and then do the following: The cube is sliding with velocity v along a flat horizontal frictionless table when it hits a straight very low step perpendicular to v, and the leading edge comes abruptly to rest.

(a) By considering which quantities are conserved before, during, and af-ter the brief collision, find the cube’s angular velocity just afaf-ter the collision.

(b) Find the minimum speed v for which the cube rolls over after hitting the step.

Solution

(a) The moment of inertia for this cube as it rotates about its edge is shown in example 10.2 (and required in the previous problem); it is I = 23M a2. During the collision, it is incorrect to assume that kinetic

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energy is conserved (it might be an inelastic collision). However, angu-lar momentum is always conserved; in particuangu-lar the component of L about the edge of the step, which we call Ly (see attached figure). We

find that Ly = X mαrα×v = MR×v = M  a √ 2  v sin 5π 4  = −M av2 (43) (the negative sign simply indicates that L is directed into the page). Immediately after the collision, the cube is rotating, and we have

Ly = Iω0 =

2 3M a

2ω

0, (44)

where the subscript on ω0 indicates that this is the angular velocity

immediately after the collision; ω will decrease over time as the cube tips. Equating these two expressions for Ly (that is, conserving angular

momentum), we find that ω0 = 3v4a. This tells us the angular frequency

of the initial rotation as a function of the initial velocity of the cube. (b) To continue this problem, realize that we are running problem

JRT10-15 in reverse. There, we balanced the cube on its edge (with ω = 0 initially), and calculated ω at the point where it fell on its side. Here, we wish to start with an (unknown) angular velocity that results in ω = 0 at the tipping point. Therefore, we rewrite our velocity as a function of ω0, and substitute ω0 =

q

3g(√2−1)

2a from that assignment

solution. The resulting velocity is

v = s

8ga(√2 − 1)

3 . (45)

#8 (5 points) JRT Prob. 10.23

Consider a rigid plane body or “lamina,” such as a flat piece of sheet metal, rotating about a point O in the body. If we choose axes so that the lamina lies in the xy plane, which elements of the inertia tensor are auto-matically zero? Prove that Izz = Ixx+ Iyy.

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Fig. 3: Geometry of question #7

Since the whole body lies in the plane z = 0, the four products of inertia involving z are all zero: Ixz = Iyz = Izx = Izy = 0. For the same reason,

Ixx+Iyy = X mα(yα2+zα2)+ X mα(zα2+x2α) = X mα(x2α+yα2) = Izz. (46) #9 (10 points)

A rectangular “brick” of mass M is positioned with one corner at the origin and with side lengths a, b, and c in the x−, y−, and z−directions, respec-tively.

(a) Calculate the inertia tensor I with respect to the origin. (10 points) (b) Suppose that the brick is rotating with angular velocity ω, about the

y−axis. Find the resulting angular momentum L. (3 points)

(c) Discuss whether or not ˆx, ˆy, and ˆz constitute a set of principal axes for the brick. (2 points)

Solution

(a) Note that this is essentially Example 10.2 from the text. We just need to change the limits of integration to account for the fact that we hae a rectangular brick and not a cube. We’ll start with Ixx. Noting that

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Fig. 4: Geometry for Question #9 ̺ = M/V = M/(abc), we have Ixx = Z a 0 dx Z b 0 dy Z c 0 dz̺ y2+ z2 (47) = M a abc Z b 0 dy Z c 0 dz y2+ z2 (48) = M a abc Z b 0 dy  y2z +1 3z 3 c 0 (49) = M a abc Z b 0 dy cy2+1 3c 3 (50) = M ac abc  1 3y 3+ 1 3c 2y b 0 (51) = M ac abc  1 3b 3+ 1 3c 2b  (52) = M 3 b 2+ c2 . (53)

The other two moments of inertia are Iyy = M3 (a2+ c2) and Izz = M

3 (c

2+ a2), as can be found using the same equation (or by observing

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As for the products of inertia, we have Ixy = − Z a 0 dx Z b 0 dy Z c 0 dz̺xy = − M c abc Z a 0 dx Z b 0 dy xy (54) = −M cabc Z a 0 dx 1 2xy 2 b 0 = −M cabc Z a 0 dx 1 2xb 2  (55) = −M cabc  14x2b2 a 0 = −M cabc  14a2b2  = −14M ab. (56) By observing the symmetries inherent to the problem (and by recall-ing that the inertia matrix must be symmetric), we find that Iyx =

−Mab/4, Ixz = Izx = −Mac/4, and Iyz = Izy = −Mbc/4. Therefore,

the inertia matrix can be written

I = M 12   4 (b2 + c2) −3ab −3ac −3ab 4 (a2 + c2) −3bc −3ac −3bc 4 (a2 + b2)  . (57)

It is easy to verify that if the brick is changed to a cube - that is, if a = b = c, I takes the same form as in example 10.2 of the text. (b) This particular angular momentum can be written ω = (0, ω, 0).

There-fore, L = Iω =  −M ωab4 ,M ω (a 2+ c2) 3 , − M ωbc 4  . (58)

(c) Since rotation about the y−axis does not produce an angular momen-tum L parallel to ω, it is clear that x, ˆˆ y, and ˆz do not constitute a set of principal axes for the brick. You can also claim that this is the case because of the non-zero off-diagonal elements of I.

#10 (10 points) JRT Prob. 10.27

Find the inertia tensor for a uniform, thin hollow cone, such as an ice-cream cone, of mass M , height h, and base radius R, spinning about its pointed end.

Solution

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points on the cone can be described by the two cylindrical coordinates ρ and φ (you can use z and φ instead, but it’s very slightly less convenient). Refer to the figure below, and imagine dividing the surface into strips as shown, and then dividing the strips into small increments of angle dφ. Then, the element of area is dA = (dρ/ sin α)(ρ dφ), where α is the half-angle of the cone. The moment about the z axis is therefore

Izz = Z σ(x2+ y2)dA = σ Z R 0 Z 2π 0 ρ2ρ dρ dφ sin α = σπR4 2 sin α, (59) since the φ integral evaluates to 2π and the ρ integral evaluates to R4/4.

The area of the cone is A = πR2/ sin α (you can check this by performing

the integral A = R

dA). Therefore, σπR2/ sin α = M , the total mass. All

together, we have Izz = M R2/2.

The other two moments, Ixx and Iyy, must be identical by symmetry. For

the first of these,

Ixx =

Z

σ(y2+ z2)dA. (60)

The first term here is the same as the second term in Izz. Since the two terms

in Izz are equal (again, by symmetry), we conclude that the first term in Ixx

is equal to Izz/2. In the second term of Ixx we can replace z by ρh/R, from

which we see that the second term in Ixx is h2/R2 times Izz. All together,

we find that Ixx = Iyy =  1 2 + h2 R2  Izz = 1 4M (R 2 + 2h2). (61)

Finally, all of the off-diagonal terms in I are zero by rotational symmetry about the z axis (as was the case with the solid cone). Therefore,

I = M 4   (R2+ 2h2) 0 0 0 (R2+ 2h2) 0 0 0 2R2  . (62) #11 (10 points) JRT Prob. 10.36

A rigid body consists of three equal masses (m) fastened at the posi-tions (a, 0, 0), (0, a, 2a), and (0, 2a, a).

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Fig. 5: Geometry of question #10

(b) Find the principal moments and a set of orthogonal principal axes. Solution

(a) The three masses are equal (m1 = m2 = m3 = m) and their positions

are r1 = a(1, 0, 0), r2 = a(0, 1, 2), r3 = a(0, 2, 1). Therefore,

Ixx = X mα(yα2 + zα2) = ma2(0 + 5 + 5) = 10ma2 (63) Iyy = X mα(x2α+ z 2 α) = ma 2(1 + 4 + 1) = 6ma2 (64) Izz = X mα(x2α+ y 2 α) = ma 2(1 + 1 + 4) = 6ma2 (65) Ixy = − X mαxαyα = −ma2(0 + 0 + 0) = 0 (66) Ixz = − X mαxαzα = −ma2(0 + 0 + 0) = 0 (67) Iyz = − X mαyαzα= −ma2(0 + 2 + 2) = −4ma2. (68) That is, I= 2ma2   5 0 0 0 3 −2 0 −2 3  . (69)

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(b) The characteristic equation is

det(I − λ1) = (10ma2 − λ)2(2ma2− λ) = 0. (70) Therefore, the principal moments areλ1 = λ2 = 10ma2andλ3 = 2ma2.

If we set λ = 10ma2, the equation (I−λ1)ω = 0 yields three equations:

0 = 0, ω2+ ω3 = 0, and ω2+ ω3 = 0. This tells us that ω2 = −ω3, and

that the two normalized eigenvectors corresponding to λ = 10ma2 are

e1 = (1, 0, 0), and e2 =

1 √

2(0, 1, −1) (71)

(note that any two perpendicular directions in the plane defined by e1

and e2 are also suitable principal axes.)

Setting λ = 2ma2, the equation (I − λ1)ω = 0 yields three equations,

ω1 = 0, ω2− ω3 = 0, and −ω2+ ω3 = 0. When normalized, this defines

the principal axis

e3 =

1 √

References

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