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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 \(x_{2}(0)=x_{3}(0)=\dot{x}_{1}(0)=\dot{x}_{2}(0)=\dot{x}_{3}(0)=0\).

Short Answer

Expert verified
The free-vibration response of the given spring-mass system can be represented as: \(x_{1}(t) = A_{1} \sin (\omega_{1}t) + B_{1} \cos (\omega_{1}t)\) \(x_{2}(t) = A_{2} \sin (\omega_{2}t) + B_{2} \cos (\omega_{2}t)\) \(x_{3}(t) = A_{3} \sin (\omega_{3}t) + B_{3} \cos (\omega_{3}t)\) Where \(A_{i}\) and \(B_{i}\) for \(i = 1, 2, 3\) are constants determined by solving the given set of linear equations and considering the initial conditions.

Step by step solution

01

Analyze the spring-mass system

: The spring-mass system in Fig. 6.29 consists of the following elements: - 3 masses: \(m_{1} = 2m\), \(m_{2} = 3m\), and \(m_{3} = 2m\), - 4 springs: \(k_{i} = k\) for \(i = 1, 2, 3, 4\). Let us denote the displacements of the masses \(m_{1}\), \(m_{2}\), and \(m_{3}\) as \(x_{1}(t)\), \(x_{2}(t)\), and \(x_{3}(t)\) respectively.
02

Write down the governing equations for each mass

: Using Newton's second law, the governing equations for each mass can be obtained: For mass \(m_{1}\): \[\begin{equation} 2m \frac{d^2 x_{1}}{dt^2} = -k(x_{1}-x_{2}) \end{equation}\] For mass \(m_{2}\): \[\begin{equation} 3m \frac{d^2 x_{2}}{dt^2} = k(x_{1}-x_{2}) - k(x_{2}-x_{3}) \end{equation}\] For mass \(m_{3}\): \[\begin{equation} 2m \frac{d^2 x_{3}}{dt^2} = -k(x_{2}-x_{3}) \end{equation}\]
03

Normalize the governing equations

: Divide each equation by the corresponding mass value: For mass \(m_{1}\): \[\frac{d^2 x_{1}}{dt^2} + \frac{k}{2m}(x_{1}-x_{2}) = 0\] For mass \(m_{2}\): \[\frac{d^2 x_{2}}{dt^2} - \frac{k}{3m}(x_{1}-x_{2}) + \frac{k}{3m}(x_{2}-x_{3}) = 0\] For mass \(m_{3}\): \[\frac{d^2 x_{3}}{dt^2} + \frac{k}{2m}(x_{2}-x_{3}) = 0\]
04

Solve the governing equations using the initial conditions

: Given the initial conditions: - \(x_{1}(0) = x_{10}\) - \(x_{2}(0) = x_{3}(0) = \dot{x}_{1}(0) = \dot{x}_{2}(0) = \dot{x}_{3}(0) = 0\) Since the initial conditions include all velocities being zero, this means the system is in free vibration. The general solutions for free vibration of a spring-mass system can be obtained using the following form: \(x_{i}(t) = A_{i} \sin (\omega_{i}t) + B_{i} \cos (\omega_{i}t)\) Solve the set of linear equations using the given initial conditions to find \(A_{i}\) and \(B_{i}\) for \(i = 1, 2, 3\).
05

Find the free-vibration response of the system

: Once we have the values for \(A_{i}\) and \(B_{i}\), substitute them into the general solutions for each mass to obtain the free-vibration response of the system: Free-vibration response: \(x_{1}(t) = A_{1} \sin (\omega_{1}t) + B_{1} \cos (\omega_{1}t)\) \(x_{2}(t) = A_{2} \sin (\omega_{2}t) + B_{2} \cos (\omega_{2}t)\) \(x_{3}(t) = A_{3} \sin (\omega_{3}t) + B_{3} \cos (\omega_{3}t)\)

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Spring-Mass System
A spring-mass system is a fundamental model used in physics to explore dynamic behavior. In its simplest form, it consists of one or more masses connected by springs. These masses can oscillate due to external disturbances or initial conditions, and the springs provide a restoring force based on Hooke's Law. In this problem, Fig. 6.29 illustrates a more complex setup with three masses and four springs. Each mass has a specific role:
  • Mass 1 is twice the foundational mass, noted as \(m_{1} = 2m\).
  • Mass 2 is three times the foundational mass, \(m_{2} = 3m\).
  • Mass 3 returns to twice the foundational mass, like Mass 1, \(m_{3} = 2m\).
All springs have a uniform spring constant \(k\), denoted as \(k_{i} = k\). The displacement of each mass is time-dependent, represented as \(x_{1}(t)\), \(x_{2}(t)\), and \(x_{3}(t)\). The study of how these masses move individually or in relation to one another explains the core dynamics of the spring-mass system. Understanding these interactions helps engineers design systems that can withstand or utilize oscillatory motion effectively.
Differential Equations
Differential equations are mathematical tools used to model the behavior of dynamic systems. For a spring-mass system like the one in our exercise, we deploy Newton’s second law to derive these equations. Each mass undergoes acceleration, which is a change in velocity over time, caused by the forces exerted by the springs.The equations are crafted as follows for each mass:- **Mass \(m_{1}\)**: The governing differential equation is: \[ 2m \frac{d^2 x_{1}}{dt^2} = -k(x_{1}-x_{2}) \] This shows the acceleration of mass 1 is determined by the difference in displacement between itself and mass 2.- **Mass \(m_{2}\)**: The governing differential equation here is: \[ 3m \frac{d^2 x_{2}}{dt^2} = k(x_{1}-x_{2}) - k(x_{2}-x_{3}) \] Mass 2 is influenced by both Mass 1 and Mass 3, having effects from both sides.- **Mass \(m_{3}\)**: The equation is: \[ 2m \frac{d^2 x_{3}}{dt^2} = -k(x_{2}-x_{3}) \] This represents the influence Mass 2 has on Mass 3.Solving these equations involves calculus and gives us insights into how the masses oscillate over time. They help predict complex motions when linked with initial conditions.
Initial Conditions
Initial conditions provide the starting values needed to solve differential equations. For systems undergoing motion, these might include initial positions and velocities. In this exercise, the initial conditions include:
  • Mass \(x_{1}\) starts at a displaced position \(x_{10}\).
  • Masses \(x_{2}\) and \(x_{3}\) start at rest, meaning their initial positions and velocities are zero.
  • All initial velocities, such as \(\dot{x}_{1}(0), \dot{x}_{2}(0),\) and \(\dot{x}_{3}(0),\) are zero.
These initial values are crucial because they determine how the system behaves with time. The fact that all initial velocities are zero signifies the system is in free vibration, without external forcing. To find the system's response, these conditions are applied to the general solution: \[ x_{i}(t) = A_{i} \sin (\omega_{i}t) + B_{i} \cos (\omega_{i}t) \]Here, \(A_{i}\) and \(B_{i}\) are constants determined by the initial conditions, and \(\omega_{i}\) is the natural frequency of the system. These determinants make sure the equations accurately model the physical movement of the system from its initial state.

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Most popular questions from this chapter

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).

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

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.

(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 $$[m]=\left[\begin{array}{lll} 1 & 0 & 0 \\ 0 & 2 & 0 \\ 0 & 0 & 3 \end{array}\right]$$

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 \([L][L]^{T}\).

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