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The wave equation describing the transverse vibrations of a stretched membrane under tension \(T\) and having a uniform surface density \(\rho\) is $$ T\left(\frac{\partial^{2} u}{\partial x^{2}}+\frac{\partial^{2} u}{\partial y^{2}}\right)=\rho \frac{\partial^{2} u}{\partial t^{2}} $$ Find a separable solution appropriate to a membrane stretched on a frame of length \(a\) and width \(b\), showing that the natural angular frequencies of such a membrane are $$ \omega^{2}=\frac{\pi^{2} T}{\rho}\left(\frac{n^{2}}{a^{2}}+\frac{m^{2}}{b^{2}}\right) $$ where \(n\) and \(m\) are any positive integers.

Short Answer

Expert verified
The natural angular frequencies are \( \omega^2 = \frac{\pi^2 T}{\rho} \left( \frac{n^2}{a^2} + \frac{m^2}{b^2} \right) \).

Step by step solution

01

- Assume a Separable Solution

Assume a separable solution of the form \[ u(x, y, t) = X(x)Y(y)T(t) \]
02

- Substitute into the Wave Equation

Substitute the assumed solution into the wave equation: \[ T \frac{\text{d}^2 (X(x)Y(y)T(t))}{\text{d} x^2} + T \frac{\text{d}^2 (X(x)Y(y)T(t))}{\text{d} y^2} = \rho \frac{\text{d}^2 (X(x)Y(y)T(t))}{\text{d} t^2} \] Simplify to get: \[ XT \frac{\text{d}^2 Y}{\text{d} y^2} + YT \frac{\text{d}^2 X}{\text{d} x^2} = \rho X Y \frac{\text{d}^2 T}{\text{d} t^2} \]
03

- Separate Variables

Divide through by \(XYT\): \[ \frac{1}{X} \frac{\text{d}^2 X}{\text{d} x^2} + \frac{1}{Y} \frac{\text{d}^2 Y}{\text{d} y^2} = \frac{\rho}{T} \frac{1}{T} \frac{\text{d}^2 T}{\text{d} t^2} \] Set each part equal to a separation constant \( -\beta \): \[ \frac{1}{X} \frac{\text{d}^2 X}{\text{d} x^2} = -\beta^2, \;\frac{1}{Y} \frac{\text{d}^2 Y}{\text{d} y^2} = -\beta^2, \; \frac{\rho}{T} \frac{1}{T} \frac{\text{d}^2 T}{\text{d} t^2} = -\beta^2 \]
04

- Solve the Spatial Equations

Solve for \(X(x)\) and \(Y(y)\): \[ \frac{\text{d}^2 X}{\text{d} x^2} + \beta^2 X = 0 \] The general solution: \[ X(x) = A \sin(\beta x) + B \cos(\beta x) \] Apply boundary conditions for a membrane: \[ X(0) = 0 \Rightarrow B = 0, \; X(a) = 0 \Rightarrow A \sin( \beta a) = 0 \Rightarrow \beta a = n\pi \text{ leading to } \beta = \frac{n\pi}{a} \; Y(y) = C \sin(\gamma y) + D \cos(\gamma y) \Rightarrow \gamma = \frac{m\pi}{b} \]
05

- Solve the Time Equation

Solve for \(T(t)\): \[ \frac{\rho}{T} \frac{\text{d}^2 T}{\text{d} t^2} + \beta^2 T = 0 \] leading to: \[ \frac{\text{d}^2 T}{\text{d} t^2} + \frac{T}{\rho} \left( \frac{n^2 \pi^2}{a^2} + \frac{m^2 \pi^2}{b^2} \right) = 0 \] The natural angular frequencies are: \[ \omega^2 = \frac{T\pi^2}{\rho} \left( \frac{n^2}{a^2} + \frac{m^2}{b^2} \right) \]

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Key Concepts

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

Separable Solution
A separable solution is a method used to simplify partial differential equations. This involves assuming the solution can be written as a product of functions, each depending on a single variable. For the wave equation describing the transverse vibrations of a stretched membrane, we assume the solution in the form:
ewline \( u(x, y, t) = X(x)Y(y)T(t) \).
ewline This assumption allows the complex problem to be broken down into simpler, solvable ordinary differential equations (ODEs) for each component function. By substituting this form into the original wave equation and then separating variables, we can treat and solve each spatial and temporal part individually. This process also makes it easier to apply boundary conditions and find specific solutions.
Boundary Conditions
Boundary conditions are constraints necessary for solving differential equations completely. They are usually defined by the physical setup of the problem. For a membrane stretched on a frame of length \(a\) and width \(b\):
ewline \[ X(0) = 0, \quad X(a) = 0, \quad Y(0) = 0, \quad Y(b) = 0 \].
ewline These conditions imply that the membrane is fixed at its edges. Applying these to the general solutions \(X(x) = A \sin(\beta x) + B \cos(\beta x)\) and \(Y(y) = C \sin(\gamma y) + D \cos(\gamma y)\) simplifies the equations and specifies the allowable values of \(\beta\) and \( \gamma \):
ewline
  • \( \beta a = n\pi\) implying \(\beta = \(n\pi/a\)\) \
  • \( \gamma b = m\pi\) implying \(\gamma = m\pi/b\) \
where \(n\) and \(m\) are positive integers. These boundary conditions help in arriving at unique solutions for the spatial parts of the wave equation.
Natural Angular Frequencies
Natural angular frequencies characterize the inherent vibration modes of the system. For the membrane described by the wave equation, once we solve for the spatial part as \(X(x) = \sin(\frac{n\pi x}{a})\) and \(Y(y) = \sin(\frac{m\pi y}{b})\), we consider the time-dependent part. The time-dependent ODE takes the form:
ewline \[ \frac{\text{d}^2 T}{\text{d} t^2} + \omega^2 T = 0 \].
ewline Solving this leads to expressions that determine the natural angular frequencies \( \omega \):
ewline \[ \omega^2 = \frac{T\pi^2}{\rho}\left( \frac{n^2}{a^2} + \frac{m^2}{b^2} \right) \].
ewline These frequencies are crucial in understanding how the membrane vibrates naturally. The values of \(n\) and \(m\) determine the specific modes of vibration, showcasing how the geometry and tension of the membrane influence its dynamic behavior.
Transverse Vibrations
Transverse vibrations refer to motions where particles of the medium (in this case, the membrane) move perpendicular to the direction of the wave propagation. For the membrane described by the wave equation, the vibrations are governed by the wave equation:
ewline \[ T\left( \frac{\partial^2 u}{\partial x^2} + \frac{\partial^2 u}{\partial y^2} \right) = \rho \frac{\partial^2 u}{\partial t^2} \].
ewline Here, \(u(x, y, t)\) represents the displacement of the membrane in the direction perpendicular to its surface. The transverse nature means that when waves travel, for example, along the x-axis, the displacement occurs along the z-axis (out of the plane).
ewline This sort of vibration is critical in analyzing the behavior of stretched membranes, such as drumheads, and can be visually and physically observed as peaks and troughs perpendicular to the surface.

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Most popular questions from this chapter

(a) Find the form of the solution of Laplace's equation in plane polar coordinates \(\rho, \phi\) that takes the value \(+1\) for \(0<\phi<\pi\) and the value \(-1\) for \(-\pi<\phi<0\) when \(\rho=a\) (b) For a point \((x, y)\) on or inside the circle \(x^{2}+y^{2}=a^{2}\), identify the angles \(\alpha\) and \(\beta\) defined by $$ \alpha=\tan ^{-1} \frac{y}{a+x} \quad \text { and } \quad \beta=\tan ^{-1} \frac{y}{a-x} $$ Show that \(u(x, y)=(2 / \pi)(\alpha+\beta)\) is a solution of Laplace's equation that satisfies the boundary conditions given in (a). (c) Deduce a Fourier series expansion for the function $$ \tan ^{-1} \frac{\sin \phi}{1+\cos \phi}+\tan ^{-1} \frac{\sin \phi}{1-\cos \phi} $$.

(a) Show that the gravitational potential due to a uniform disc of radius \(a\) and mass \(M\), centred at the origin, is given for \(ra\) by $$ \frac{G M}{r}\left[1-\frac{1}{4}\left(\frac{a}{r}\right)^{2} P_{2}(\cos \theta)+\frac{1}{8}\left(\frac{a}{r}\right)^{4} P_{4}(\cos \theta)-\cdots\right] $$ where the polar axis is normal to the plane of the disc. (b) Reconcile the presence of a term \(P_{1}(\cos \theta)\), which is odd under \(\theta \rightarrow \pi-\theta\), with the symmetry with respect to the plane of the disc of the physical system. (c) Deduce that the gravitational field near an infinite sheet of matter of constant density \(\rho\) per unit area is \(2 \pi G \rho\).

A membrane is stretched between two concentric rings of radii \(a\) and \(b(b>a)\). If the smaller ring is transversely distorted from the planar configuration by an amount \(c|\phi|,-\pi \leq \phi \leq \pi\), show that the membrane then has a shape given by $$ u(\rho, \phi)=\frac{c \pi}{2} \frac{\ln (b / \rho)}{\ln (b / a)}-\frac{4 c}{\pi} \sum_{m \text { odd }} \frac{a^{m}}{m^{2}\left(b^{2 m}-a^{2 m}\right)}\left(\frac{b^{2 m}}{\rho^{m}}-\rho^{m}\right) \cos m \phi $$.

A conducting cube has as its six faces the planes \(x=\pm a, y=\pm a\) and \(z=\pm a\), and contains no internal heat sources. Verify that the temperature distribution $$ u(x, y, z, t)=A \cos \frac{\pi x}{a} \sin \frac{\pi z}{a} \exp \left(-\frac{2 \kappa \pi^{2} t}{a^{2}}\right) $$ obeys the appropriate diffusion equation. Across which faces is there heat flow? What is the direction and rate of heat flow at the point \((3 a / 4, a / 4, a)\) at time \(t=a^{2} /\left(\kappa \pi^{2}\right) ?\)

The motion of a very viscous fluid in the two-dimensional (wedge) region \(-\alpha<\) \(\phi<\alpha\) can be described in ( \(\rho, \phi\) ) coordinates by the (biharmonic) equation $$ \nabla^{2} \nabla^{2} \psi \equiv \nabla^{4} \psi=0 $$ together with the boundary conditions \(\partial \psi / \partial \phi=0\) at \(\phi=\pm \alpha\), which represents the fact that there is no radial fluid velocity close to either of the bounding walls because of the viscosity, and \(\partial \psi / \partial \rho=\pm \rho\) at \(\phi=\pm \alpha\), which imposes the condition that azimuthal flow increases linearly with \(r\) along any radial line. Assuming a solution in separated-variable form, show that the full expression for \(\psi\) is $$ \psi(\rho, \phi)=\frac{\rho^{2}}{2} \frac{\sin 2 \phi-2 \phi \cos 2 \alpha}{\sin 2 \alpha-2 \alpha \cos 2 \alpha} $$.

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