A rigid rod of length \(L\), and mass \(m_{a}\) is connected to a rigid base of mass \(m_{b}\) through a torsional spring of stiffness \(k_{T}\) as shown. The base sits on an elastic support of stiffness \(k\) as indicated. Derive the equations of motion of the system using Lagrange's equations.

Short Answer

Expert verified
Answer: The equation of motion for the given system is \[\left(m_a + m_b\right)\ddot{\theta} = \left(k_T + \frac{kL^2}{4}\right)\theta\].

Step by step solution

01

1. Determine the Kinetic Energy (T) of the System

We start by finding the kinetic energy of the system, which consists of two parts: kinetic energy of the rod and kinetic energy of the base. For the rod: Half of the rod's mass, \(m_a\), is concentrated at a distance of L/2 from the axis of rotation. Its angular velocity is \(\dot{\theta}\). Therefore, the kinetic energy of the rod can be written as: \[T_{rod} = \frac{1}{2} m_a\left(\frac{L}{2}\right)^2 \dot{\theta}^2\] For the base: The linear velocity of the center of mass of the base, \(v_{base}\), can be written as: \[v_{base} = \frac{L}{2} \dot{\theta}\] Hence, the kinetic energy of the base is: \[T_{base} = \frac{1}{2} m_b v_{base}^2 = \frac{1}{2} m_b \left(\frac{L}{2}\dot{\theta}\right)^2\] The total kinetic energy of the system is the sum of these two parts: \[T = T_{rod} + T_{base}\]
02

2. Determine the Potential Energy (V) of the System

The potential energy of the system comes from the torsional spring and the elastic support. For the torsional spring: The potential energy stored in the torsional spring with stiffness \(k_T\) is given by: \[V_{spring} = \frac{1}{2} k_{T} \theta^2\] For the elastic support: The displacement of the base with respect to the support is \(\frac{L}{2}\theta\), and the potential energy stored in the elastic support with stiffness \(k\) is given by: \[V_{support} = \frac{1}{2} k\left(\frac{L}{2}\theta\right)^2\] The total potential energy of the system is the sum of these two parts: \[V = V_{spring} + V_{support}\]
03

3. Write the Lagrangian of the System (L)

The Lagrangian of the system is the difference between the kinetic energy and potential energy: \[ L = T - V\] Substitute the expressions for the kinetic and potential energies into the Lagrangian equation: \[ L = \left(\frac{1}{2} m_a\left(\frac{L}{2}\right)^2 \dot{\theta}^2 + \frac{1}{2} m_b \left(\frac{L}{2}\dot{\theta}\right)^2\right) - \left(\frac{1}{2} k_{T} \theta^2 + \frac{1}{2} k\left(\frac{L}{2}\theta\right)^2\right) \]
04

4. Derive the Equations of Motion using Lagrange's Equations

For a single degree-of-freedom system like ours, where the generalized coordinate is \(\theta\), the Lagrange's equation is given by: \[\frac{d}{dt}\frac{\partial L}{\partial \dot{\theta}} - \frac{\partial L}{\partial \theta} = 0\] Now, compute the required partial derivatives, substitute the expressions, and solve the equation to obtain the equations of motion: From the Lagrangian expression, we have: \[\frac{\partial L}{\partial \dot{\theta}} = 2 \cdot \frac{1}{2} m_a\left(\frac{L}{2}\right)^2 \dot{\theta} + 2 \cdot \frac{1}{2} m_b \left(\frac{L}{2}\dot{\theta}\right)\left(\frac{L}{2}\right)\] And, \[\frac{\partial L}{\partial \theta} = -k_{T}\theta - k\left(\frac{L}{2}\theta\right)\left(\frac{L}{2}\right)\] Now compute the time derivative of \(\frac{\partial L}{\partial \dot{\theta}}\): \[\frac{d}{dt}\frac{\partial L}{\partial \dot{\theta}} = m_a\left(\frac{L}{2}\right)^2 \ddot{\theta} + m_b \left(\frac{L}{2}\right)^2 \ddot{\theta}\] Substitute the expressions for the partial derivatives and their time derivatives into Lagrange's equation: \[(m_a\left(\frac{L}{2}\right)^2 + m_b\left(\frac{L}{2}\right)^2) \ddot{\theta} = k_{T}\theta + k\left(\frac{L}{2}\right)^2\theta\] Finally, the equation of motion for the given problem can be written as: \[\left(m_a + m_b\right)\ddot{\theta} = \left(k_T + \frac{kL^2}{4}\right)\theta\] This is the derived equation of motion for the given system using Lagrange's equations.

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Most popular questions from this chapter

Consider an aircraft traveling at constant altitude and speed as it undergoes tight periodic rolling motion of the fuselage. Let the wings be modeled as equivalent rigid bodies with torsional springs of stiffness \(k_{T}\) at the fuselage wall. In addition, let each wing possess moment of inertia \(I_{c}\) about its respective connection point and let the fuselage of radius \(R\) have moment of inertia \(I_{o}\) about its axis. Derive the equations of rolling motion for the aircraft.

A square raft of mass \(m\) and side \(L\) sits in water of specific gravity \(\gamma_{w}\). A uniform vertical line force of intensity \(P\) acts downward at a distance \(a\) left of center of the span. (a) Use Lagrange's equations to derive the 2-D equations of motion of the raft. (b) Check your answers using Newton's Laws of Motion.

Use Lagrange's equations to derive the equation of motion of the simple pendulum.

Three identical rigid disks, each of mass \(m\) and radius \(R\), are attached at their centers to an elastic shaft of area polar moment of inertia \(J\) and shear modulus \(G\). The ends of the rod are embedded in rigid supports as shown. The spans between the disks and between the disks and the supports are each of length \(L\). Derive the equations of angular motion for the system if the disks are subjected to the twisting moments \(M_{1}, M_{2}\) and \(M_{3}\), respectively.

Use Lagrange's equations to derive the equations of motion for the triple pendulum whose bobs are subjected to horizontal forces \(F_{1}, F_{2}\) and \(F_{3}\), respectively.

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