Develop the theory of the normal-mode torsional vibrations of a rod of length \(l\) having free ends. Show how to express an arbitrary vibration as a sum of normal-mode vibrations. Show how to evaluate the normal-mode amplitudes from an initial configuration \(\phi(x)\) and an initial velocity \(\partial \phi(x) / \partial t\).

Short Answer

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Based on the given step-by-step solution, provide a short answer describing how to express an arbitrary vibration as a sum of normal-mode vibrations and evaluate the normal-mode amplitudes for a rod of length \(l\) subject to torsional vibrations. An arbitrary torsional vibration of a rod can be expressed as a sum of normal-mode vibrations as follows: \(\phi(x,t) = \sum_{n=1}^\infty A_n \sin(\frac{n \pi x}{l}) \cos(\omega_n t)\) Here, \(A_n\)s are the normal-mode amplitudes, which can be evaluated using the initial configuration \(\phi(x)\) and initial velocity \(\frac{\partial \phi(x)}{\partial t}\) through the expression: \(A_n = \frac{2}{l} \int_0^l \phi(x) \sin(\frac{n \pi x}{l}) dx\)

Step by step solution

01

Governing Equation of Motion

We begin by deriving the equation governing the torsional vibrations of a rod with free ends. For a rod of length \(l\) subject to torsional vibrations, we have the equation of motion: \(\frac{\partial^2 \phi(x,t)}{\partial t^2} = c^2 \frac{\partial^2 \phi(x,t)}{\partial x^2}\) where \(\phi(x,t)\) is the angular displacement of the rod at position \(x\) and time \(t\) and \(c\) is the speed of torsional waves in the material. This is a partial differential equation that can be solved by separation of variables.
02

Solving for Normal Modes

Next, we need to solve the equation of motion for the normal modes. To do this, we introduce a separation of variables ansatz: \(\phi(x,t) = X(x) T(t)\) Substituting this ansatz into the governing equation of motion yields: \(X(x) \frac{d^2 T(t)}{dt^2} = c^2 T(t) \frac{d^2 X(x)}{dx^2}\) Dividing both sides by \(c^2 XT\), we get: \(\frac{1}{c^2 T(t)} \frac{d^2 T(t)}{dt^2} = \frac{1}{X(x)} \frac{d^2 X(x)}{dx^2}\) Since the left side depends only on time and the right side depends only on position, they must be equal to a constant. We denote this constant as \(-\omega^2\): \(\frac{1}{c^2 T(t)} \frac{d^2 T(t)}{dt^2} = \frac{1}{X(x)} \frac{d^2 X(x)}{dx^2} = -\omega^2\) Solving these two ordinary differential equations with the conditions \(X(0)=X(l)=0\), we find the normal modes: \(X_n(x) = \sin(\frac{n \pi x}{l})\) \(T_n(t) = \cos(\omega_n t)\) where the index \(n\) enumerates the modes and the frequencies \(\omega_n\) are given by: \(\omega_n = c \frac{n \pi}{l}\)
03

Expressing an Arbitrary Vibration as a Sum of Normal Modes

We can now express an arbitrary torsional vibration as a sum of normal-mode vibrations: \(\phi(x,t) = \sum_{n=1}^\infty A_n \sin(\frac{n \pi x}{l}) \cos(\omega_n t)\) where the \(A_n\)s are the normal-mode amplitudes.
04

Evaluating the Normal-Mode Amplitudes

Finally, we need to evaluate the normal-mode amplitudes given the initial configuration \(\phi(x)\) and initial velocity \(\frac{\partial \phi(x)}{\partial t}\). At \(t=0\), we have: \(\phi(x) = \sum_{n=1}^\infty A_n \sin(\frac{n \pi x}{l})\) and \(\frac{\partial \phi(x)}{\partial t} = \sum_{n=1}^\infty A_n \omega_n \sin(\frac{n \pi x}{l})\) To evaluate the normal-mode amplitudes, we can use the orthogonality of the sine functions and integrate both sides over the interval \([0, l]\): \(A_n = \frac{2}{l} \int_0^l \phi(x) \sin(\frac{n \pi x}{l}) dx\) In conclusion, this is how we develop the theory of normal-mode torsional vibrations of a rod of length \(l\) having free ends. We show how to express an arbitrary vibration as a sum of normal-mode vibrations and how to evaluate the normal-mode amplitudes from an initial configuration \(\phi(x)\) and an initial velocity \(\frac{\partial \phi(x)}{\partial t}\).

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Most popular questions from this chapter

Show that the frequencies for the transverse vibrations of a bar of length \(l\) clamped at one end and free at the other may be found from the equation \(\cosh m \cos m=-1\), in which \(m=n l .\) Verify that the smallest root is \(m_{1}=1.875\).

A long slender rod is vibrating in its fundamental longitudinal mode. It is desired to raise its frequency 1 percent by drilling holes of equal depth in each end of the rod. The holes are to have an area equal to one-fourth the cross-sectional area of the rod. How deep should the holes be drilled? How will their presence affect the first few overtones?

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Show that a longitudinal wave on a slender rod exerts an average force $$ \bar{F}_{x}=\bar{E}_{1}=\frac{1}{c} \bar{P}=c g_{x} $$ when it is absorbed. Hint: See Sec. 1.11.

Consider the resonating exponential horn of Prob. \(4.3 .1\), with \(n=1\). Let the ratio of diameters at the two ends be 10. Sketch the amplitude of the oscillatory strain along the horn and find the location and value of its maximum. Then evaluate (numerically) the "figure of merit" $$ \phi=\frac{\text { velocity amplitude at small end }}{\left(c_{b}\right)(\text { maximum strain amplitude })} $$ By (4.1.9), this quantity is unity for a uniform rod \((\alpha=0)\). The value of \(\phi\) for a horn shows that a greater velocity amplitude can be attained with a given material than for a uniform rod. How big can the figure of merit get for horns of large diameter ratio? Answer: 30 percent of length from small end; \(\phi=1.99 ; \phi_{\max }=2.72\).

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