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Mechanical Vibrations in SI Units

Singiresu S. Rao

Chapter 6

Multi degree-of Freedom Systems - all with Video Answers

Educators


Chapter Questions

01:57

Problem 1

Derive the equations of motion, using Newton's second law of motion, for each of the systems shown in Figs. $6.18-6.22$.

James Kiss
James Kiss
Numerade Educator
01:57

Problem 2

Derive the equations of motion, using Newton's second law of motion, for each of the systems shown in Figs. $6.18-6.22$.

James Kiss
James Kiss
Numerade Educator
02:47

Problem 3

Derive the equations of motion, using Newton's second law of motion, for each of the systems shown in Figs. $6.18-6.22$.

James Kiss
James Kiss
Numerade Educator
03:05

Problem 4

Derive the equations of motion, using Newton's second law of motion, for each of the systems shown in Figs. $6.18-6.22$.

James Kiss
James Kiss
Numerade Educator
02:32

Problem 5

Derive the equations of motion, using Newton's second law of motion, for each of the systems shown in Figs. $6.18-6.22$.

James Kiss
James Kiss
Numerade Educator
05:06

Problem 6

A car is modeled as shown in Fig. 6.23 . Derive the equations of motion using Newton's second law of motion.

James Kiss
James Kiss
Numerade Educator
02:09

Problem 7

The equations of motion derived using the displacements of the masses, $x_{1}, x_{2},$ and $x_{3}$ as degrees of freedom in Fig. 6.12 (Example 6.10 ) lead to symmetric mass and stiffness matrices in Eq. (E.3) of Example $6.10 .$ Express the equations of motion, (E.3) of Example 6.10 , using $x_{1}, x_{2}-x_{1},$ and $x_{3}-x_{2}$ as degrees of freedom in the form:
$$[\bar{m}] \ddot{\vec{y}}+[\bar{k}] \vec{y}=\overrightarrow{0}$$ where $$\vec{y}=\left\{\begin{array}{l}
y_{1} \\
y_{2} \\
y_{3}
\end{array}\right\}$$
Show that the resulting mass and stiffness matrices $[m]$ and $[k]$ are nonsymmetric.

James Kiss
James Kiss
Numerade Educator
04:04

Problem 8

A simplified vibration analysis of an airplane considers bounce and pitch motions (Fig. $6.24(\mathrm{a})$ ). For this, a model consisting of a rigid bar (corresponding to the body of the airplane) supported on two springs (corresponding to the stiffnesses of the main and nose landing gears) as shown in Fig. $6.24(\mathrm{~b})$ is used. The analysis can be conducted using three different coordinate systems as shown in Figs. $6.24(\mathrm{c})-(\mathrm{e}) .$ Derive the equations of motion in the three coordinate systems and identify the type of coupling associated with each coordinate system.

James Kiss
James Kiss
Numerade Educator
02:41

Problem 9

Consider the two-degree-of-freedom system shown in Fig. 6.25 with $m_{1}=m_{2}=1$ and $k_{1}=k_{2}=4$. The masses $m_{1}$ and $m_{2}$ move on a rough surface for which the equivalent viscous damping constants can be assumed as $c_{1}=c_{2}=2$.
a. Derive the equations of motion of the system.
b. Find the natural frequencies and mode shapes of the undamped system.

James Kiss
James Kiss
Numerade Educator
03:22

Problem 10

For a simplified analysis of the vibration of an airplane in the vertical direction, a threedegree-of-freedom model, as shown in Fig. $6.26,$ can be used. The three masses indicate the masses of the two wings $\left(m_{1}=m_{3}=m\right)$ and the fuselage $\left(m_{2}=5 m\right) .$ The stiffnesses

James Kiss
James Kiss
Numerade Educator
02:28

Problem 11

A simplified model of the main landing gear system of a small airplane is shown in Fig. 6.27 with $m_{1}=100 \mathrm{~kg}, m_{2}=5000 \mathrm{~kg}, k_{1}=10^{4} \mathrm{~N} / \mathrm{m},$ and $k_{2}=10^{6} \mathrm{~N} / \mathrm{m}$
a. Find the equations of motion of the system.
b. Find the natural frequencies and the mode shapes of the system.

James Kiss
James Kiss
Numerade Educator
00:58

Problem 12

Derive the stiffness matrix of each of the systems shown in Figs. $6.18-6.23$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
01:06

Problem 13

Derive the stiffness matrix of each of the systems shown in Figs. $6.18-6.23$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
00:59

Problem 14

Derive the stiffness matrix of each of the systems shown in Figs. $6.18-6.23$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
01:11

Problem 15

Derive the stiffness matrix of each of the systems shown in Figs. $6.18-6.23$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
01:33

Problem 16

Derive the stiffness matrix of each of the systems shown in Figs. $6.18-6.23$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
01:35

Problem 17

Derive the stiffness matrix of each of the systems shown in Figs. $6.18-6.23$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
01:02

Problem 18

Derive the flexibility matrix of the system shown in Fig. 5.39 .

James Kiss
James Kiss
Numerade Educator
01:13

Problem 19

Derive the stiffness matrix of the system shown in Fig. 5.39 .

James Kiss
James Kiss
Numerade Educator
01:12

Problem 20

Derive the flexibility matrix of the system shown in Fig. 5.42 .

James Kiss
James Kiss
Numerade Educator
01:01

Problem 21

Derive the stiffness matrix of the system shown in Fig. 5.42 .

James Kiss
James Kiss
Numerade Educator
00:59

Problem 22

Derive the mass matrix of the system shown in Fig. 5.42 .

James Kiss
James Kiss
Numerade Educator
02:28

Problem 23

Find the flexibility and stiffness influence coefficients of the torsional system shown in Fig. $6.28 .$ Also write the equations of motion of the system.

James Kiss
James Kiss
Numerade Educator
02:28

Problem 24

Find the flexibility and stiffness influence coefficients of the system shown in Fig. $6.29 .$ Also, derive the equations of motion of the system.

James Kiss
James Kiss
Numerade Educator
02:15

Problem 25

An airplane wing, Fig. $6.30(\mathrm{a})$, is modeled as a three-degree-of-freedom lumped-mass system, as shown in Fig. $6.30(\mathrm{~b})$. Derive the flexibility matrix and the equations of motion of the wing by assuming that all $A_{i}=A,(E I)_{i}=E I, l_{i}=l$ and that the root is fixed.

James Kiss
James Kiss
Numerade Educator
01:04

Problem 26

Determine the flexibility matrix of the uniform beam shown in Fig. $6.31 .$ Disregard the mass of the beam compared to the concentrated masses placed on the beam and assume all $l_{i}=l$.

James Kiss
James Kiss
Numerade Educator
01:42

Problem 27

Derive the flexibility and stiffness matrices of the spring-mass system shown in Fig. 6.32 assuming that all the contacting surfaces are frictionless.

James Kiss
James Kiss
Numerade Educator
02:19

Problem 28

Derive the equations of motion for the tightly stretched string carrying three masses, as shown in Fig. 6.33 . Assume the ends of the string to be fixed.

James Kiss
James Kiss
Numerade Educator
01:14

Problem 29

Derive the equations of motion of the system shown in Fig. 6.34 .

James Kiss
James Kiss
Numerade Educator
02:16

Problem 30

Four identical springs, each having a stiffness $k,$ are arranged symmetrically at $90^{\circ}$ from each other, as shown in Fig. $2.65 .$ Find the influence coefficient of the junction point in an arbitrary direction.

James Kiss
James Kiss
Numerade Educator
01:51

Problem 31

Show that the stiffness matrix of the spring-mass system shown in Fig. $6.3(a)$ is a band matrix along the diagonal.

James Kiss
James Kiss
Numerade Educator
00:58

Problem 32

Derive the mass matrix of each of the systems shown in Figs. $6.18-6.22$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
01:03

Problem 33

Derive the mass matrix of each of the systems shown in Figs. $6.18-6.22$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
01:58

Problem 34

Derive the mass matrix of each of the systems shown in Figs. $6.18-6.22$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
01:03

Problem 35

Derive the mass matrix of each of the systems shown in Figs. $6.18-6.22$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
01:57

Problem 36

Derive the mass matrix of each of the systems shown in Figs. $6.18-6.22$ using the indicated coordinates.

James Kiss
James Kiss
Numerade Educator
02:21

Problem 37

The inverse mass influence coefficient $b_{i j}$ is defined as the velocity induced at point $i$ due to a unit impulse applied at point $j$. Using this definition, derive the inverse mass matrix of the system shown in Fig. $6.4(\mathrm{a})$.

James Kiss
James Kiss
Numerade Educator
01:42

Problem 38

For the four-story shear building shown in Fig. 6.35 , there is no rotation of the horizontal section at the level of floors. Assuming that the floors are rigid and the total mass is concentrated at the levels of the floors, derive the equations of motion of the building using (a) Newton's second law of motion and (b) Lagrange's equations.

James Kiss
James Kiss
Numerade Educator
02:13

Problem 39

Derive the equations of motion of the system shown in Fig. 6.36 by using Lagrange's equations with $x$ and $\theta$ as generalized coordinates.

James Kiss
James Kiss
Numerade Educator
02:58

Problem 40

Derive the equations of motion of the system shown in Fig. 5.12(a), using Lagrange's equations with (a) $x_{1}$ and $x_{2}$ as generalized coordinates and (b) $x$ and $\theta$ as generalized coordinates.

James Kiss
James Kiss
Numerade Educator
01:03

Problem 41

Derive the equations of motion of the system shown in Fig. 6.29 using Lagrange's equations.

James Kiss
James Kiss
Numerade Educator
05:40

Problem 42

Derive the equations of motion of the triple pendulum shown in Fig. 6.10 using Lagrange's equations.

James Kiss
James Kiss
Numerade Educator
05:30

Problem 43

When an airplane (see Fig. 6.37 (a)) undergoes symmetric vibrations, the fuselage can be idealized as a concentrated central mass $M_{0}$ and the wings can be modeled as rigid bars carrying end masses $M,$ as shown in Fig. $6.37(\mathrm{~b})$. The flexibility between the wings and the fuselage can be represented by two torsional springs of stiffness $k_{t}$ each.
(a) Derive the equations of motion of the airplane, using Lagrange's equations with $x$ and $\theta$ as generalized coordinates.
(b) Find the natural frequencies and mode shapes of the airplane.
(c) Find the torsional spring constant in order to have the natural frequency of vibration, in torsional mode, greater than $2 \mathrm{~Hz}$ when $M_{0}=1000 \mathrm{~kg}, M=500 \mathrm{~kg},$ and $l=6 \mathrm{~m}$

James Kiss
James Kiss
Numerade Educator
01:30

Problem 44

Use Lagrange's equations to derive the equations of motion of each of the systems shown in Figs. $6.18-6.22$

James Kiss
James Kiss
Numerade Educator
01:44

Problem 45

Use Lagrange's equations to derive the equations of motion of each of the systems shown in Figs. $6.18-6.22$

James Kiss
James Kiss
Numerade Educator
03:38

Problem 46

Use Lagrange's equations to derive the equations of motion of each of the systems shown in Figs. $6.18-6.22$

James Kiss
James Kiss
Numerade Educator
02:23

Problem 47

Use Lagrange's equations to derive the equations of motion of each of the systems shown in Figs. $6.18-6.22$

James Kiss
James Kiss
Numerade Educator
02:18

Problem 48

Use Lagrange's equations to derive the equations of motion of each of the systems shown in Figs. $6.18-6.22$

James Kiss
James Kiss
Numerade Educator
04:42

Problem 49

Set up the eigenvalue problem of Example 6.11 in terms of the coordinates $q_{1}=x_{1}, q_{2}=$ $x_{2}-x_{1}$, and $q_{3}=x_{3}-x_{2}$, and solve the resulting problem. Compare the results obtained with those of Example 6.11 and draw conclusions.

James Kiss
James Kiss
Numerade Educator
01:48

Problem 50

Derive the frequency equation of the system shown in Fig. 6.29 .

James Kiss
James Kiss
Numerade Educator
03:05

Problem 51

Find the natural frequencies and mode shapes of the system shown in Fig. $6.6(\mathrm{a})$ when $k_{1}=k, k_{2}=2 k, k_{3}=3 k, m_{1}=m, m_{2}=2 m,$ and $m_{3}=3 m .$ Plot the mode shapes.

James Kiss
James Kiss
Numerade Educator
02:30

Problem 52

Set up the matrix equation of motion and determine the three principal modes of vibration for the system shown in Fig. $6.6\left(\right.$ a) with $k_{1}=3 k, k_{2}=k_{3}=k, m_{1}=3 m,$ and $m_{2}=m_{3}=m$. Check the orthogonality of the modes found.

James Kiss
James Kiss
Numerade Educator
01:37

Problem 53

Find the natural frequencies of the system shown in Fig. 6.10 with $l_{1}=20 \mathrm{~cm}, l_{2}=30 \mathrm{~cm}$, $l_{3}=40 \mathrm{~cm}, m_{1}=1 \mathrm{~kg}, m_{2}=2 \mathrm{~kg},$ and $m_{3}=3 \mathrm{~kg} .$

James Kiss
James Kiss
Numerade Educator
04:00

Problem 54

(a) Find the natural frequencies of the system shown in Fig. 6.31 with $m_{1}=m_{2}=m_{3}=m$ and $l_{1}=l_{2}=l_{3}=l_{4}=l / 4 .$ (b) Find the natural frequencies of the beam when $m=10 \mathrm{~kg}, l=0.5 \mathrm{~m},$ the cross section is a solid circular section with diameter $2.5 \mathrm{~cm},$ and the material is steel. (c) Consider using a hollow circular, solid rectangular, or hollow rectangular cross section for the beam to achieve the same natural frequencies as in (b). Identify the cross section corresponding to the least weight of the beam.

James Kiss
James Kiss
Numerade Educator
00:59

Problem 55

The frequency equation of a three-degree-of-freedom system is given by
$$\left|\begin{array}{rrr}
\lambda-5 & -3 & -2 \\
-3 & \lambda-6 & -4 \\
-1 & -2 & \lambda-6
\end{array}\right|=0$$
Find the roots of this equation.

James Kiss
James Kiss
Numerade Educator
01:26

Problem 56

Determine the eigenvalues and eigenvectors of the system shown in Fig. 6.29 , taking $k_{1}=k_{2}=k_{3}=k_{4}=k$ and $m_{1}=m_{2}=m_{3}=m$.

James Kiss
James Kiss
Numerade Educator
01:34

Problem 57

Find the natural frequencies and mode shapes of the system shown in Fig. 6.29 for $k_{1}=k_{2}=k_{3}=k_{4}=k, m_{1}=2 m, m_{2}=3 m,$ and $m_{3}=2 m$

James Kiss
James Kiss
Numerade Educator
01:55

Problem 58

Find the natural frequencies and principal modes of the triple pendulum shown in Fig. 6.10 , assuming that $l_{1}=l_{2}=l_{3}=l$ and $m_{1}=m_{2}=m_{3}=m .$

James Kiss
James Kiss
Numerade Educator
01:34

Problem 59

Find the natural frequencies and mode shapes of the system considered in Problem 6.27 with $m_{1}=m, m_{2}=2 m, m_{3}=m, k_{1}=k_{2}=k,$ and $k_{3}=2 k$.

James Kiss
James Kiss
Numerade Educator
03:02

Problem 60

Show that the natural frequencies of the system shown in Fig. $6.6(a)$, with $k_{1}=3 k$, $k_{2}=k_{3}=k, \quad m_{1}=4 m, \quad m_{2}=2 m,$ and $m_{3}=m,$ are given by $\omega_{1}=0.46 \sqrt{k / m},$ $\omega_{2}=\sqrt{k / m}$, and $\omega_{3}=1.34 \sqrt{k / m}$. Find the eigenvectors of the system.

James Kiss
James Kiss
Numerade Educator
01:32

Problem 61

Find the natural frequencies of the system considered in Problem 6.28 with $m_{1}=2 m, m_{2}=m, m_{3}=3 m,$ and $l_{1}=l_{2}=l_{3}=l_{4}=l .$

James Kiss
James Kiss
Numerade Educator
01:04

Problem 62

Find the natural frequencies and principal modes of the torsional system shown in Fig. 6.28 for $(G J)_{i}=G J, i=1,2,3,4, J_{d 1}=J_{d 2}=J_{d 3}=J_{0}$, and $l_{1}=l_{2}=l_{3}=l_{4}=l$.

James Kiss
James Kiss
Numerade Educator
01:33

Problem 63

The mass matrix $[m]$ and the stiffness matrix $[k]$ of a uniform bar are
$$[m]=\frac{\rho A l}{4}\left[\begin{array}{lll}
1 & 0 & 0 \\
0 & 2 & 0 \\
0 & 0 & 1
\end{array}\right] \quad \text { and } \quad[k]=\frac{2 A E}{l}\left[\begin{array}{rrr}
1 & -1 & 0 \\
-1 & 2 & -1 \\
0 & -1 & 1
\end{array}\right]$$
where $\rho$ is the density, $A$ is the cross-sectional area, $E$ is Young's modulus, and $l$ is the length of the bar. Find the natural frequencies of the system by finding the roots of the characteristic equation. Also find the principal modes.

James Kiss
James Kiss
Numerade Educator
01:33

Problem 64

The mass matrix of a vibrating system is given by
$$[m]=\left[\begin{array}{lll}
1 & 0 & 0 \\
0 & 2 & 0 \\
0 & 0 & 1
\end{array}\right]$$
and the eigenvectors by
$$\left\{\begin{array}{r}
1 \\
-1 \\
1
\end{array}\right\}, \quad\left\{\begin{array}{l}
1 \\
1 \\
1
\end{array}\right\}, \quad \text { and } \quad\left\{\begin{array}{l}
0 \\
1 \\
2
\end{array}\right\}$$
Find the $[m]$ -orthonormal modal matrix of the system.

James Kiss
James Kiss
Numerade Educator
01:46

Problem 65

For the system shown in Fig. 6.38 , (a) determine the characteristic polynomial $\Delta\left(\omega^{2}\right)=\operatorname{det}\left|[k]-\omega^{2}[m]\right|,$ (b) plot $\Delta\left(\omega^{2}\right)$ from $\omega^{2}=0$ to $\omega^{2}=4.0$ (using increments $\Delta \omega^{2}=0.2$ ), and (c) find $\omega_{1}^{2}, \omega_{2}^{2}$, and $\omega_{3}^{2}$.

James Kiss
James Kiss
Numerade Educator
02:36

Problem 66

(a) Two of the eigenvectors of a vibrating system are known to be
$$\left\{\begin{array}{l}
0.2754946 \\
0.3994672 \\
0.4490562
\end{array}\right\} \quad \text { and } \quad\left\{\begin{array}{r}
0.6916979 \\
0.2974301 \\
-0.3389320
\end{array}\right\}$$
Prove that these are orthogonal with respect to the mass matrix
$$[m]=\left[\begin{array}{lll}
1 & 0 & 0 \\
0 & 2 & 0 \\
0 & 0 & 3
\end{array}\right]$$

James Kiss
James Kiss
Numerade Educator
03:09

Problem 67

Find the natural frequencies of the system shown in Fig. 6.18 for $m_{i}=m, i=1,2,3$.

James Kiss
James Kiss
Numerade Educator
03:09

Problem 68

Find the natural frequencies of the system shown in Fig. 6.19 with $m=1 \mathrm{~kg}, l=1 \mathrm{~m}$, $k=1000 \mathrm{~N} / \mathrm{m},$ and $c=100 \mathrm{~N}-\mathrm{s} / \mathrm{m}$.

James Kiss
James Kiss
Numerade Educator
01:03

Problem 69

Consider the eigenvalue problem
$$\left[[k]-\omega^{2}[m]\right] \vec{X}=\overrightarrow{0}$$
where
$$[k]=k\left[\begin{array}{ccc}
2 & -1 & 0 \\
-1 & 2 & -1 \\
0 & -1 & 1
\end{array}\right] \text { and }[m]=m\left[\begin{array}{ccc}
1 & 0 & 0 \\
0 & 1 & 0 \\
0 & 0 & 1
\end{array}\right]$$
Find the natural frequencies by finding the roots of the characteristic equation
$$\left|[m]^{-1}[k]-\omega^{2}[I]\right|=0$$
Compare your results with the ones obtained in Example 6.11 .

Sam Stansfield
Sam Stansfield
Numerade Educator
02:30

Problem 70

Find the eigenvalues and eigenvectors of the following matrix:
$$
[A]=\left[\begin{array}{cc}
8 & -1 \\
-4 & 4
\end{array}\right]
$$

Aman Gupta
Aman Gupta
Numerade Educator
01:29

Problem 71

Consider the eigenvalue problem
$$\left[[k]-\omega^{2}[m]\right] \vec{X}=\overrightarrow{0}$$
where
$$[m]=\left[\begin{array}{ll}
2 & 0 \\
0 & 1
\end{array}\right] \text { and }[k]=\left[\begin{array}{cc}
8 & -4 \\
-4 & 4
\end{array}\right]$$
Find the natural frequencies and mode shapes of the system:
a. by solving the equation $\left[[m]^{-1}[k]-\omega^{2}[I]\right] \vec{X}=\overrightarrow{0}$
b. by solving the equation $\left[-\omega^{2}[k]^{-1}[m]+[I]\right] \vec{X}=\overrightarrow{0}$
c. Compare the two sets of results and give your observations.

James Kiss
James Kiss
Numerade Educator
02:19

Problem 72

Consider the eigenvalue problem:
$$\omega^{2}\left[\begin{array}{ll}
1 & 0 \\
0 & 2
\end{array}\right]\left\{\begin{array}{l}
X_{1} \\
X_{2}
\end{array}\right\}=\left[\begin{array}{rr}
6 & -2 \\
-2 & 2
\end{array}\right]\left\{\begin{array}{l}
X_{1} \\
X_{2}
\end{array}\right\}$$
a. Find the natural frequencies and mode shapes of the system.
b. Change the coordinates in Eq. (E.1) as $X_{1}=Y_{1}$ and $X_{2}=3 Y_{2}$ and express the eigenvalue problem in terms of the eigenvector $\vec{Y}=\left\{\begin{array}{l}Y_{1} \\ Y_{2}\end{array}\right\}$, solve it, and find the natural frequencies and mode shapes.
c. Compare the results found in parts (a) and (b) and give your observations.

James Kiss
James Kiss
Numerade Educator
01:46

Problem 73

Consider the eigenvalue problem:
$$\lambda[m] \vec{X}=[k] \vec{X}$$
where
$$[m]=\left[\begin{array}{ll}
1 & 0 \\
0 & 4
\end{array}\right], \quad[k]=\left[\begin{array}{rr}
8 & -2 \\
-2 & 2
\end{array}\right], \quad \text { and } \quad \lambda=\omega^{2}$$
Equation (E.1) can be expressed as
$$[D] \vec{X}=\lambda \vec{X}$$
where
$$[D]=\left([m]^{\frac{1}{2}}\right)^{-1}[k]\left([m]^{\frac{1}{2}}\right)^{-1}$$
is called the mass normalized stiffness matrix. Determine the mass normalized stiffness matrix and use it to find the eigenvalues and orthonormal eigenvectors of the problem stated in Eq. (E.1).

James Kiss
James Kiss
Numerade Educator
01:09

Problem 73

A symmetric positive definite matrix, such as the mass matrix of a multidegree-of-freedom system, $[m]$, can be expressed as the product of a lower triangular matrix, $[L],$ and an upper triangular matrix, $[L]^{T},$ as $$[m]=[L][L]^{T}$$
using a procedure known as the Choleski method [6.18]. For a mass matrix of order $3 \times 3$, Eq. (E.1) becomes
$$\left[\begin{array}{lll}
m_{11} & m_{12} & m_{13} \\
m_{12} & m_{22} & m_{23} \\
m_{13} & m_{23} & m_{33}
\end{array}\right]=\left[\begin{array}{ccc}
L_{11} & 0 & 0 \\
L_{21} & L_{22} & 0 \\
L_{31} & L_{32} & L_{33}
\end{array}\right]\left[\begin{array}{ccc}
L_{11} & L_{21} & L_{31} \\
0 & L_{22} & L_{32} \\
0 & 0 & L_{33}
\end{array}\right]$$
By carrying out the multiplication of the matrices on the right-hand side of Eq. (E.2) and equating each of the elements of the resulting $3 \times 3$ matrix to the corresponding element of the matrix on the left-hand side of Eq. (E.2), the matrix $[L]$ can be identified. Using this procedure, decompose the matrix
$$[m]=\left[\begin{array}{lll}
4 & 2 & 1 \\
2 & 6 & 2 \\
1 & 2 & 8
\end{array}\right]$$
in the form $[L][L]^{T}$.

James Kiss
James Kiss
Numerade Educator
01:52

Problem 75

Find the natural frequencies and mode shapes of the system shown in Fig. 6.14 with $m_{1}=m, m_{2}=2 m, m_{3}=3 m,$ and $k_{1}=k_{2}=k$.

James Kiss
James Kiss
Numerade Educator
01:42

Problem 76

Find the modal matrix for the semidefinite system shown in Fig. 6.39 for $J_{1}=J_{2}=$ $J_{3}=J_{0}, k_{t 1}=k_{t},$ and $k_{t 2}=2 k_{t}$

James Kiss
James Kiss
Numerade Educator
02:01

Problem 77

Find the free-vibration response of the spring-mass system shown in Fig. 6.29 for $k_{i}=k(i=1,2,3,4), m_{1}=2 m, m_{2}=3 m, m_{3}=2 m$ for the initial conditions $x_{1}(0)=x_{10}$ and $x_{2}(0)=x_{3}(0)=\dot{x}_{1}(0)=\dot{x}_{2}(0)=\dot{x}_{3}(0)=0$.

James Kiss
James Kiss
Numerade Educator
02:55

Problem 78

Find the free-vibration response of the triple pendulum shown in Fig. 6.10 for $l_{i}=l(i=1,2,3)$ and $m_{i}=m(i=1,2,3)$ for the initial conditions $\theta_{1}(0)=\theta_{2}(0)=0,$
$\theta_{3}(0)=\theta_{30}, \dot{\theta}_{i}(0)=0(i=1,2,3)$.

James Kiss
James Kiss
Numerade Educator
02:53

Problem 79

Find the free-vibration response of the tightly stretched string shown in Fig. 6.33 for $m_{1}=2 m, m_{2}=m, m_{3}=3 m,$ and $l_{i}=l(i=1,2,3,4) .$ Assume the initial conditions as $x_{1}(0)=x_{3}(0)=0, x_{2}(0)=x_{20}, \dot{x}_{i}(0)=0(i=1,2,3)$.

James Kiss
James Kiss
Numerade Educator
03:27

Problem 80

Find the free-vibration response of the spring-mass system shown in Fig. $6.6(\mathrm{a})$ for $k_{1}=k, k_{2}=2 k, k_{3}=3 k, m_{1}=m, m_{2}=2 m,$ and $m_{3}=3 m$ corresponding to the initial conditions $\dot{x}_{1}(0)=\dot{x}_{10}, x_{i}(0)=0(i=1,2,3),$ and $\dot{x}_{2}(0)=\dot{x}_{3}(0)=0$.

James Kiss
James Kiss
Numerade Educator
03:07

Problem 81

Find the free-vibration response of the spring-mass system shown in Fig. 6.32 for $m_{1}=m, m_{2}=2 m, m_{3}=m, k_{1}=k_{2}=k,$ and $k_{3}=2 k$ corresponding to the initial conditions $\dot{x}_{3}(0)=\dot{x}_{30},$ and $x_{1}(0)=x_{2}(0)=x_{3}(0)=\dot{x}_{1}(0)=\dot{x}_{2}(0)=0$.

James Kiss
James Kiss
Numerade Educator
02:39

Problem 82

In the freight car system shown in Fig. $6.14,$ the first car acquires a velocity of $\dot{x}_{0}$ due to an impact. Find the resulting free vibration of the system. Assume $m_{i}=m(i=1,2,3)$ and $k_{1}=k_{2}=k$.

James Kiss
James Kiss
Numerade Educator
02:44

Problem 83

Find the free-vibration response of a three-degree-of-freedom system governed by the equation
$$10\left[\begin{array}{lll}
1 & 0 & 0 \\
0 & 1 & 0 \\
0 & 0 & 1
\end{array}\right] \ddot{\vec{x}}(t)+100\left[\begin{array}{rrr}
2 & -1 & 0 \\
-1 & 2 & -1 \\
0 & -1 & 1
\end{array}\right] \vec{x}(t)=\overrightarrow{0}$$
Assume the initial conditions as $x_{i}(0)=0.1$ and $\dot{x}_{i}(0)=0 ; i=1,2,3$. Note: The natural frequencies and mode shapes of the system are given in Examples 6.11 and 6.12 .

James Kiss
James Kiss
Numerade Educator
02:44

Problem 84

Using modal analysis, determine the free-vibration response of a two-degree-of-freedom system with equations of motion
$$2\left[\begin{array}{ll}
1 & 0 \\
0 & 1
\end{array}\right] \ddot{\vec{x}}(t)+8\left[\begin{array}{rr}
2 & -1 \\
-1 & 2
\end{array}\right] \vec{x}(t)=\overrightarrow{0}$$
with initial conditions
$$
\vec{x}(0)=\left\{\begin{array}{l}
1 \\
0
\end{array}\right\}, \quad \dot{\vec{x}}(0)=\left\{\begin{array}{l}
0 \\
1
\end{array}\right\}
$$

James Kiss
James Kiss
Numerade Educator
03:48

Problem 85

Consider the free-vibration equations of an undamped two-degree-of-freedom system:
$$[m] \ddot{\vec{x}}+[k] \vec{x}=\overrightarrow{0}$$
with
$$[m]=\left[\begin{array}{ll}
1 & 0 \\
0 & 4
\end{array}\right] \text { and }[k]=\left[\begin{array}{rr}
8 & -2 \\
-2 & 2
\end{array}\right]$$
a. Find the orthonormal eigenvectors using the mass normalized stiffness matrix.
b. Determine the principal coordinates of the system and obtain the modal equations.

James Kiss
James Kiss
Numerade Educator
01:45

Problem 86

For the two-degree-of-freedom system considered in Problem $6.85,$ find the free-vibration response, $x_{1}(t)$ and $x_{2}(t),$ using the modal equations derived in Problem 6.85 for the following initial conditions: $x_{1}(0)=2, x_{2}(0)=3, \dot{x}_{1}(0)=\dot{x}_{2}(0)=0$.

James Kiss
James Kiss
Numerade Educator
02:14

Problem 87

Find the free-vibration response of the three-degree-of-freedom airplane model considered in Problem 6.10 for the following data: $m=5000 \mathrm{~kg}, l=5 \mathrm{~m}, E=7 \mathrm{GPa}, I=8 \times 10^{-6} \mathrm{~m}^{4}$. Assume that the initial conditions correspond to that of a gust which results in $x_{1}(0)=0$, $x_{2}(0)=0.1 \mathrm{~m}, x_{3}(0)=0, \dot{x}_{1}(0)=\dot{x}_{2}(0)=\dot{x}_{3}=0$.

James Kiss
James Kiss
Numerade Educator
02:44

Problem 88

The free-vibration solution of a two-degree-of-freedom system can be determined by solving the equations
$$[m] \ddot{\vec{x}}+[k] \vec{x}=\overrightarrow{0}$$
with $\vec{x}=\left\{\begin{array}{l}x_{1}(t) \\ x_{2}(t)\end{array}\right\},$ using the initial conditions
$$\vec{x}(t=0)=\vec{x}_{0}=\left\{\begin{array}{l}
x_{10} \\
x_{20}
\end{array}\right\} \quad \text { and } \quad \dot{\vec{x}}(t=0)=\dot{\vec{x}}=\left\{\begin{array}{l}
\dot{x}_{10} \\
\dot{x}_{20}
\end{array}\right\} .$$
If $\omega_{1}$ and $\omega_{2}$ are the natural frequencies and $\vec{u}_{1}$ and $\vec{u}_{2}$ are the mode shapes of the system obtained from the solution of the characteristic equation
$$\left[[m] s^{2}+[k]\right] \vec{u}=\overrightarrow{0}$$
with $s=\pm \omega_{1}, \pm \omega_{2}$ (characteristic roots), the solution of Eq. (E.1), $\vec{x}(t),$ can be found as a linear combination of different solutions as:
$$\vec{x}(t): \quad C_{1} \vec{u}_{1} e^{-i \omega_{1} t}+C_{2} \vec{u}_{1} e^{+i \omega_{1} t}+C_{3} \vec{u}_{2} e^{-i \omega_{2} t}+C_{4} \vec{u}_{2} e^{+i \omega_{2} t}$$
where $C_{i}, i=1,2,3,4,$ are constants. Show that the solution in Eq. (E.3) can be expressed, in equivalent form, as
$$\vec{x}(t)=A_{1} \sin \left(\omega_{1} t+\phi_{1}\right) \vec{u}_{1}+A_{2} \sin \left(\omega_{2} t+\phi_{2}\right) \vec{u}_{2}$$
where $A_{1}, A_{2}, \phi_{1},$ and $\phi_{2}$ are constants.

Sam Stansfield
Sam Stansfield
Numerade Educator
01:58

Problem 89

Determine the amplitudes of motion of the three masses in Fig. 6.40 when a harmonic force $F(t)=F_{0} \sin \omega t$ is applied to the lower left mass with $m=1 \mathrm{~kg}, k=1000 \mathrm{~N} / \mathrm{m}, F_{0}=5 \mathrm{~N},$ and $\omega=10 \mathrm{rad} / \mathrm{s}$ using the mode superposition method.

James Kiss
James Kiss
Numerade Educator
03:20

Problem 90

(a) Determine the natural frequencies and mode shapes of the torsional system shown in Fig. 6.11 for $k_{t 1}=k_{t 2}=k_{t 3}=k_{t}$ and $J_{1}=J_{2}=J_{3}=J_{0} .$ (b) If a torque $M_{t 3}(t)=$
$M_{t 0} \cos \omega t,$ with $M_{t 0}=500 \mathrm{~N}-\mathrm{m}$ and $\omega=100 \mathrm{rad} / \mathrm{s},$ acts on the generator $\left(J_{3}\right),$ find the amplitude of each component. Assume $M_{t 1}=M_{t 2}=0, k_{t}=100 \mathrm{~N}-\mathrm{m} / \mathrm{rad},$ and $J_{0}=1 \mathrm{~kg}-\mathrm{m}^{2}$.

James Kiss
James Kiss
Numerade Educator
01:48

Problem 91

Using the results of Problems 6.24 and $6.56,$ determine the modal matrix $[X]$ of the system shown in Fig. 6.29 and derive the uncoupled equations of motion.

James Kiss
James Kiss
Numerade Educator
02:38

Problem 92

An approximate solution of a multidegree-of-freedom system can be obtained using the mode acceleration method. According to this method, the equations of motion of an undamped system, for example, are expressed as
$$\vec{x}=[k]^{-1}(\vec{F}-[m] \ddot{\vec{x}})$$
and $\ddot{\vec{x}}$ is approximated using the first $r$ modes $(r<n)$ as
$$\underset{n \times 1}{\ddot{\vec{x}}}=[X] \underset{n \times r}{\vec{q}}$$
Since $\left([k]-\omega_{i}^{2}[m]\right) \vec{X}^{(i)}=\overrightarrow{0},$ Eq. $($ E.1 $)$ can be written as
$$\vec{x}(t)=[k]^{-1} \vec{F}(t)-\sum_{i=1}^{r} \frac{1}{\omega_{i}^{2}} \vec{X}^{(i)} \ddot{q}_{i}(t)$$
Find the approximate response of the system described in Example 6.19 (without damping), using the mode acceleration method with $r=1$.

James Kiss
James Kiss
Numerade Educator
03:48

Problem 93

Determine the response of the system in Problem 6.51 to the initial conditions $x_{1}(0)=1$, $\dot{x}_{1}(0)=0, x_{2}(0)=2, \dot{x}_{2}(0)=1, x_{3}(0)=1,$ and $\dot{x}_{3}(0)=-1 .$ Assume $k / m=1$.

James Kiss
James Kiss
Numerade Educator
02:02

Problem 94

Show that the initial conditions of the generalized coordinates $q_{i}(t)$ can be expressed in terms of those of the physical coordinates $x_{i}(t)$ in modal analysis as
$$
\vec{q}(0)=[X]^{T}[m] \vec{x}(0), \quad \dot{\vec{q}}(0)=[X]^{T}[m] \dot{\vec{x}}(0).
$$

James Kiss
James Kiss
Numerade Educator
01:40

Problem 95

A simplified model of a bicycle with its rider is shown in Fig. $6.41 .$ Find the vertical motion of the rider when the bicycle hits an elevated road, as shown in the figure.

James Kiss
James Kiss
Numerade Educator
02:55

Problem 96

Find the response of the triple pendulum shown in Fig. 6.10 for $l_{i}=0.5 \mathrm{~m}(i=1,2,3)$ and $m_{i}=1 \mathrm{~kg}(i=1,2,3)$ when a moment, in the form of a rectangular pulse of magnitude $0.1 \mathrm{~N}-\mathrm{m}$ and duration $0.1 \mathrm{~s}$, is applied along the direction of $\theta_{3}$. Assume that the pendulum is at rest at $t=0$.

James Kiss
James Kiss
Numerade Educator
03:17

Problem 97

Find the response of the spring-mass system shown in Fig. $6.6\left(\right.$ a) for $k_{1}=k, k_{2}=2 k$, $k_{3}=3 k, m_{1}=m, m_{2}=2 m,$ and $m_{3}=3 m$ with $k=10^{4} \mathrm{~N} / \mathrm{m}$ and $m=2 \mathrm{~kg}$ when a force, in the form of a rectangular pulse of magnitude $1000 \mathrm{~N}$ and duration $0.25 \mathrm{~s}$, is applied to mass $m_{1}$ in the direction of $x_{1}$.

James Kiss
James Kiss
Numerade Educator
02:58

Problem 98

Consider a two-degree-of-freedom system with the equations of motion $[m] \overrightarrow{\vec{x}}+[k] \vec{x}=\vec{f}(t)$ with
$$[m]=\left[\begin{array}{ll}
1 & 0 \\
0 & 4
\end{array}\right], \quad[k]=\left[\begin{array}{rr}
8 & -2 \\
-2 & 2
\end{array}\right], \quad \text { and } \quad \vec{f}(t)=\left\{\begin{array}{l}
f_{1}(t) \\
f_{2}(t)
\end{array}\right\}$$
a. Derive the modal equations for the forced-vibration response of the system.
b. Determine the conditions to be satisfied by $f_{1}(t)$ and $f_{2}(t)$ in order to influence both the modes.

James Kiss
James Kiss
Numerade Educator
01:23

Problem 99

Find the steady-state response of the system shown in Fig. 6.17 with $k_{1}=k_{2}=k_{3}=k_{4}$ $=100 \mathrm{~N} / \mathrm{m}, c_{1}=c_{2}=c_{3}=c_{4}=1 \mathrm{~N}-\mathrm{s} / \mathrm{m}, m_{1}=m_{2}=m_{3}=1 \mathrm{~kg}, F_{1}(t)=F_{0} \cos \omega t$ $F_{0}=10 \mathrm{~N},$ and $\omega=1 \mathrm{rad} / \mathrm{s}$. Assume that the spring $k_{4}$ and the damper $c_{4}$ are connected to a rigid wall at the right end. Use the mechanical impedance method described in Section 5.6 for solution.

James Kiss
James Kiss
Numerade Educator
02:46

Problem 100

An airplane wing, Fig. $6.42(\mathrm{a})$, is modeled as a twelve-degree-of-freedom lumped-mass system as shown in Fig. $6.42(\mathrm{~b})$. The first three natural mode shapes, obtained experimentally, are given below.

James Kiss
James Kiss
Numerade Educator
00:58

Problem 101

Using MATLAB, find the eigenvalues and eigenvectors of a system with mass and stiffness matrices given in Example 6.13 .

James Kiss
James Kiss
Numerade Educator
02:00

Problem 102

Using MATLAB, find and plot the free-vibration response of the system described in Problem 6.79 for the following data: $x_{20}=0.5, P=100, l=5, m=2$.

James Kiss
James Kiss
Numerade Educator
02:14

Problem 103

Using the MATLAB function ode23, find and plot the forced-vibration response of the system described in Problem 6.89 .

James Kiss
James Kiss
Numerade Educator
01:09

Problem 104

Using the MATLAB function roots, find the roots of the following equation:
$$
f(x)=x^{12}-2=0
$$

James Kiss
James Kiss
Numerade Educator
01:29

Problem 105

Find the forced-vibration response of a viscously damped three-degree-of-freedom system with equations of motion:
$$10\left[\begin{array}{ccc}1 & 0 & 0 \\ 0 & 2 & 0 \\ 0 & 0 & 3\end{array}\right] \ddot{\vec{x}}(t)+5\left[\begin{array}{rrr}3 & -1 & 0 \\ -1 & 4 & -3 \\ 0 & -3 & 3\end{array}\right] \dot{\vec{x}}(t)+20\left[\begin{array}{rrr}7 & -3 & 0 \\ -3 & 5 & -2 \\ 0 & -2 & 2\end{array}\right] \vec{x}(t)=\left\{\begin{array}{l}5 \cos 2 t \\ 0 \\ 0\end{array}\right\}$$
Assume zero initial conditions.

James Kiss
James Kiss
Numerade Educator
01:51

Problem 106

Using the MATLAB function ode23, solve Problem 6.99 and plot $x_{1}(t), x_{2}(t),$ and $x_{3}(t)$.

James Kiss
James Kiss
Numerade Educator
01:05

Problem 107

Using Program7.m, generate the characteristic polynomial corresponding to the matrix
$$
[A]=\left[\begin{array}{lll}
5 & 3 & 2 \\
3 & 6 & 4 \\
1 & 2 & 6
\end{array}\right]
$$

James Kiss
James Kiss
Numerade Educator
01:58

Problem 108

Using Program8 $\cdot \mathrm{m},$ find the steady-state response of a three-degree-of-freedom system with the following data:
$$\begin{aligned}
\omega_{1} &=25.076 \mathrm{rad} / \mathrm{s}, \quad \omega_{2}=53.578 \mathrm{rad} / \mathrm{s}, \quad \omega_{3}=110.907 \mathrm{rad} / \mathrm{s} \\
\zeta_{i} &=0.001, \quad i=1,2,3
\end{aligned}$$
$$
\begin{array}{l}
{[m]=\left[\begin{array}{ccc}
41.4 & 0 & 0 \\
0 & 38.8 & 0 \\
0 & 0 & 25.88
\end{array}\right], \quad[e v]=\left[\begin{array}{lll}
1 & 1.0 & 1.0 \\
1.303 & 0.860 & -1.000 \\
1.947 & -1.685 & 0.183
\end{array}\right]} \\
\vec{F}(t)=\left\{\begin{array}{l}
F_{1}(t) \\
F_{2}(t) \\
F_{3}(t)
\end{array}\right\}=\left\{\begin{array}{l}
5000 \cos 5 t \\
10000 \cos 10 t \\
20000 \cos 20 t
\end{array}\right\}
\end{array}
$$

James Kiss
James Kiss
Numerade Educator
03:54

Problem 109

Find and plot the response, $x_{1}(t)$ and $x_{2}(t),$ of a system with the following equations of motion:
$$\left[\begin{array}{ll}
5 & 0 \\
0 & 2
\end{array}\right]\left\{\begin{array}{l}
\ddot{x}_{1} \\
\ddot{x}_{2}
\end{array}\right\}+\left[\begin{array}{cc}
0.5 & -0.6 \\
-0.6 & 0.8
\end{array}\right]\left\{\begin{array}{c}
\dot{x}_{1} \\
\dot{x}_{2}
\end{array}\right\}+\left[\begin{array}{cc}
20 & -2 \\
-2 & 2
\end{array}\right]\left\{\begin{array}{l}
x_{1} \\
x_{2}
\end{array}\right\}=\left\{\begin{array}{l}
1 \\
0
\end{array}\right\} \sin 2 t \quad \text { (E.1) }$$
using the initial conditions:
$$\vec{x}(t=0)=\left\{\begin{array}{c}
0.1 \\
0
\end{array}\right\} \mathrm{m} \quad \text { and } \quad \dot{\vec{x}}(t=0)=\left\{\begin{array}{l}
0 \\
1
\end{array}\right\} \mathrm{m} / \mathrm{s}$$
Solve the differential equations, (E.1), numerically using a suitable MATLAB function.

James Kiss
James Kiss
Numerade Educator
04:42

Problem 110

Write a computer program for finding the eigenvectors using the known eigenvalues in Eq. (6.61). Find the mode shapes of Problem 6.57 using this program.

James Kiss
James Kiss
Numerade Educator
05:53

Problem 111

Write a computer program for generating the $[m]$ -orthonormal modal matrix $[X]$. The program should accept the number of degrees of freedom, the normal modes, and the mass matrix as input. Solve Problem 6.64 using this program.

Morgan Cheatham
Morgan Cheatham
Numerade Educator
01:01

Problem 112

The equations of motion of an undamped system in SI units are given by
$$\left[\begin{array}{lll}
2 & 0 & 0 \\
0 & 2 & 0 \\
0 & 0 & 2
\end{array}\right] \ddot{\vec{x}}+\left[\begin{array}{rrr}
16 & -8 & 0 \\
-8 & 16 & -8 \\
0 & -8 & 16
\end{array}\right] \vec{x}=\left\{\begin{array}{c}
10 \sin \omega t \\
0 \\
0
\end{array}\right\}$$
Using subroutine MODAL, find the steady-state response of the system when $\omega=5 \mathrm{rad} / \mathrm{s}$.

James Kiss
James Kiss
Numerade Educator
04:44

Problem 113

Find the response of the system in Problem 6.112 by varying $\omega$ between $1 \mathrm{rad} / \mathrm{s}$ and $10 \mathrm{rad} / \mathrm{s}$ in increments of $1 \mathrm{rad} / \mathrm{s}$. Plot the graphs showing the variations of magnitudes of the first peaks of $x_{i}(t), i=1,2,3,$ with respect to $\omega$.

James Kiss
James Kiss
Numerade Educator
01:27

Problem 114

Find the natural frequencies of vibration and the corresponding mode shapes of the beam shown in Fig. 6.9 using the mass matrix
$$[m]=\left[\begin{array}{ccc}
m_{1} & 0 & 0 \\
0 & m_{2} & 0 \\
0 & 0 & m_{3}
\end{array}\right] \equiv m\left[\begin{array}{ccc}
1 & 0 & 0 \\
0 & 1 & 0 \\
0 & 0 & 1
\end{array}\right]$$
and the flexibility matrix given by Eq. (E.4) of Example 6.6 .

James Kiss
James Kiss
Numerade Educator
02:18

Problem 115

A heavy machine tool mounted on the first floor of a building, Fig. $6.43(\mathrm{a})$, has been modeled as a three-degree-of-freedom system as indicated in Fig. 6.43(b). (a) For $k_{1}=875 \mathrm{kN} / \mathrm{m}$, $k_{2}=87 \mathrm{kN} / \mathrm{m}, k_{3}=350 \mathrm{kN} / \mathrm{m}, c_{1}=c_{2}=c_{3}=2000 \mathrm{~N}-\mathrm{s} / \mathrm{m}, m_{f}=8700 \mathrm{~kg}, m_{b}=1800 \mathrm{~kg},$ $m_{h}=350 \mathrm{~kg}$, and $F(t)=4000 \cos 60 t \mathrm{~N},$ find the steady-state vibration of the system using the mechanical impedance method described in Section 5.6. (b) If the maximum response of the machine tool head $\left(x_{3}\right)$ has to be reduced by $25 \%,$ how should the stiffness of the mounting $\left(k_{2}\right)$ be changed? (c) Is there any better way of achieving the goal stated in (b)? Provide details.

James Kiss
James Kiss
Numerade Educator
01:48

Problem 116

Figure 6.44 shows a model of an automobile including the masses of the automobile, seat and body, and head and neck of the passenger. The suspension system of the automobile is modeled by two linear springs $k_{1}$ and $k_{2}$ with the wheels assumed to have negligible mass. The head and neck are connected to the seat by a linear spring $\left(k_{3}\right)$ and a torsional spring $\left(k_{t}\right)$, while the seat and body is connected to the automobile using a linear spring $k_{4}$. Derive the equations of motion of the system when the automobile hits a rigid wall at a linear velocity $v$. Assume that the head is at a height of $h$ above the mass $m_{2}$ concentrated at the pivot point $P$ when the automobile is at rest. Discuss the suitability of the model for predicting the injury to the head during the impact.

Narayan Hari
Narayan Hari
Numerade Educator
02:29

Problem 117

It is proposed to transport a precision electronic equipment of weight $\mathrm{W}_{1}=5000 \mathrm{~N}$ by a trailer. The electronic equipment is placed in the trailer on a rubber mount of stiffness $k_{1}=10,000 \mathrm{~N} / \mathrm{m}$. The trailer's leaf springs have a total stiffness of $k_{2}=50,000 \mathrm{~N} / \mathrm{m}$ and the tires have a total stiffness of $k_{3}=20,000 \mathrm{~N} / \mathrm{m}$. The trailer body has a weight of $\mathrm{W}_{2}=2500 \mathrm{~N}$ and the unsprung weight is $\mathrm{W}_{3}=1000 \mathrm{~N}$. Due to road repairs, the trailer encounters a step change of $0.1 \mathrm{~m}$ in the level of the road as shown in Fig. $6.45($ a). By modeling the trailer-electronic equipment system as two- and three-degree-of-freedom systems as shown, respectively, in Figs. $6.45(\mathrm{~b})$ and (c), determine the maximum displacement, velocity, and accelerations experienced by the electronic equipment in each case. Suggest a method of reducing the maximum acceleration of the electronic equipment by 25 percent.

James Kiss
James Kiss
Numerade Educator