Show that the most general solution of the wave equation (5.1.8) consisting of plane waves traveling in the direction of the unit vector \(\mathbf{n}\) is given by $$ p=f_{1}\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right)+f_{2}\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right), $$ where \(f_{1}\) and \(f_{2}\) are arbitrary functions.

Short Answer

Expert verified
#short_Answer# The given function, \(p=f_{1}\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right)+f_{2}\left(\mathbf{n}\cdot \mathbf{r}+c_{f} t\right)\), does satisfy the wave equation (5.1.8) and represents the most general solution consisting of plane waves traveling in the direction of the unit vector \(\mathbf{n}\), with \(f_1\) and \(f_2\) being arbitrary functions.

Step by step solution

01

Compute the first and second derivatives of \(p\) with respect to \(t\)

First, we need to compute the first and second time-derivatives of \(p\). Since \(f_1\) and \(f_2\) are arbitrary functions and only depend on the arguments inside the parenthesis, we can write: $$ \frac{\partial p}{\partial t} = -c_{f} f_{1}'\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right) + c_{f} f_{2}'\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right), $$ $$ \frac{\partial^2 p}{\partial t^2} = c_{f}^2 f_{1}''\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right) + c_{f}^2 f_{2}''\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right), $$ where \(f_1'\) and \(f_2'\) are the first derivatives of \(f_1\) and \(f_2\), and \(f_1''\) and \(f_2''\) are the second derivatives of \(f_1\) and \(f_2\), respectively.
02

Compute the Laplacian of \(p\)

Next, we need to compute the Laplacian of pressure wave \(p\), which is given by the double derivative with respect to each spatial coordinate: $$ \nabla^2 p = \nabla \cdot \nabla p = \nabla \cdot\left(\mathbf{n} f_{1}'\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right)-\mathbf{n} f_{2}'\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right)\right). $$ Since \(\mathbf{n}\) is a constant vector, we can rewrite the expression as: $$ \nabla^2 p =\nabla \cdot \left[f_{1}'\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right) \mathbf{n} - f_{2}'\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right) \mathbf{n}\right]. $$ Now, using the property \(\nabla \cdot (f \mathbf{A}) = f \nabla \cdot \mathbf{A} + \mathbf{A} \cdot (\nabla f)\), where \(f\) is a scalar function and \(\mathbf{A}\) is a vector field, we have: $$ \nabla^2 p =\left[f_{1}'\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right) + f_{2}'\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right)\right] \nabla \cdot \mathbf{n} + \nabla\left[f_{1}'\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right) - f_{2}'\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right)\right] \cdot\mathbf{n}. $$ Since \(\nabla \cdot \mathbf{n} = 0\) as \(\mathbf{n}\) is a constant unit vector, we are left with: $$ \nabla^2 p= \nabla\left[f_{1}'\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right) - f_{2}'\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right)\right] \cdot\mathbf{n}. $$ Given that \(f_1'\) and \(f_2'\) only depend on the arguments inside the parenthesis, we can rewrite the last term as: $$ \nabla^2 p= \left[ f_{1}''\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right) - f_{2}''\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right)\right] \mathbf{n} \cdot\mathbf{n}. $$ Since \(\mathbf{n}\cdot\mathbf{n}=1\), we have: $$ \nabla^2 p= f_{1}''\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right) - f_{2}''\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right). $$
03

Check if the given function satisfies the wave equation

Finally, we want to check if the given solution \(p\) satisfies the wave equation: $$ \frac{\partial^2 p}{\partial t^2} = c_{f}^2\nabla^2 p, $$ Plugging in our expressions for \(\frac{\partial^2 p}{\partial t^2}\) and \(\nabla^2 p\), we observe that they are indeed equal: $$ c_{f}^2 f_{1}''\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right) + c_{f}^2 f_{2}''\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right) = c_{f}^2\left[f_{1}''\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right) - f_{2}''\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right)\right]. $$
04

Conclusion

Therefore, the given function: $$ p=f_{1}\left(\mathbf{n} \cdot \mathbf{r}-c_{f} t\right)+f_{2}\left(\mathbf{n} \cdot \mathbf{r}+c_{f} t\right), $$ does indeed satisfy the wave equation (5.1.8) and represents the most general solution consisting of plane waves traveling in the direction of the unit vector \(\mathbf{n}\), with \(f_1\) and \(f_2\) being arbitrary functions.

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Most popular questions from this chapter

Each possible normal mode of oscillation of a distributed system constitutes a mechanical degree of freedom of the system. According to the classical equipartition-of-energy theorem, each oscillatory degree of freedom is to be assigned an average thermal energy of \(k T\), where \(k\) is Boltzmann's constant and \(T\) is the absolute temperature. Hence the internal thermal energy per unit volume of a monatomic gas should be \(E_{v}=n k T\), with \(n\) given by (5.7.11). For a mole of monatomic gas, kinetic theory tells us that the internal energy is \(E_{\mu}=\frac{3}{2} R T\), where \(R\) is the gas constant per mole. We can bring the two viewpoints into agreement by choosing a suitable value of \(\omega_{\max }\). Compute this value and show that the minimum wavelength is of the order of the mean spacing of the atoms in the gas.

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Show that the sound wave specified by $$ p(\mathbf{r}, t)=p_{m} \exp i(\mathbf{x} \cdot \mathbf{r}-\omega t) $$ satisfies the wave equation (5.3.1) and constitutes a plane wave traveling in the direction of the vector wave number \(\kappa\). Find an expression for the particle displacement \(\boldsymbol{\rho}\) and velocity \(\dot{e}\) in the wave. Verify that the wave is irrotational by computing \(\nabla \times\) e. Justify the use of the term "longitudinal" in referring to a plane sound wave, such as (5.3.20).

A satellite passes across the sky sending out radio signals at a constant but inaccurately known frequency \(\omega_{s}\). Assume that the satellite altitude is small compared to the earth's radius and hence that the trajectory can be considered to be a straight line at constant altitude above a flat earth. By beating the signals against a known standard frequency and measuring the difference frequency, an observer on the earth can accurately measure the received frequency, with its Doppler shift, as a function of time, with \(\cos \theta_{s}\) in \((5.8 .3)\) [or \((5.8 .5)\), with \(\gamma=1\), since \(v \ll c]\) ranging from 1 to \(-1\). Show how the observations can be made to yield a value of \(v\), the velocity of the satellite, and a value of \(D\), the closest distance of approach of the satellite. \(\dagger\)

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