The potential \(\phi(\boldsymbol{r})=\left(q / 4 \pi \epsilon_{0} r\right) \mathrm{e}^{-\mu r}\) may be regarded as representing the effect of screening of a charge \(q\) at the origin by mobile charges in a plasma. Calculate the charge density \(\rho\) (at points where \(r \neq 0\) ) and find the total charge throughout space, excluding the origin.

Short Answer

Expert verified
Answer: \(\rho(r) = -2q\mathrm{e}^{-\mu r} + q\mu^2\mathrm{e}^{-\mu r}\)

Step by step solution

01

Write Poisson's equation for finding the charge density

To find the charge density from the given potential function, we will use Poisson's equation: \(\nabla^2 \phi(\boldsymbol{r}) = -\frac{\rho(\boldsymbol{r})}{\epsilon_0}\).
02

Compute the Laplacian of the potential function

Now we need to compute the Laplacian of the given potential function in spherical coordinates. Remembering that in spherical coordinates, the Laplacian operator is: \(\nabla^2 = \frac{1}{r^2}\frac{\partial}{\partial r}\left(r^2\frac{\partial}{\partial r}\right) + \cdots\) (We're skipping the angular part since the potential function only depends on the \(r\)-coordinate) The given potential function is: \(\phi(\boldsymbol{r})=\left(\frac{q}{4 \pi \epsilon_{0} r}\right)\mathrm{e}^{-\mu r}\)
03

Calculate the first derivative with respect to r

Now, we must calculate the first derivative of the potential function with respect to r: \(\frac{\partial \phi}{\partial r} = \frac{\partial}{\partial r}\left(\frac{q}{4\pi\epsilon_0r}\mathrm{e}^{-\mu r}\right) = \frac{-q}{4\pi\epsilon_0 r^2}\mathrm{e}^{-\mu r} + \frac{q\mu}{4\pi\epsilon_0 r}\mathrm{e}^{-\mu r}\)
04

Calculate the second derivative with respect to r

Now, we must calculate the second derivative of the potential function with respect to r: \(\frac{\partial^2 \phi}{\partial r^2} = \frac{\partial}{\partial r}\left(\frac{-q}{4\pi\epsilon_0 r^2}\mathrm{e}^{-\mu r} + \frac{q\mu}{4\pi\epsilon_0 r}\mathrm{e}^{-\mu r}\right)\) By taking the derivative, we have: \(\frac{\partial^2 \phi}{\partial r^2} = \frac{2q}{4\pi\epsilon_0 r^3}\mathrm{e}^{-\mu r} - \frac{q\mu}{4\pi\epsilon_0 r^2}\mathrm{e}^{-\mu r} - \frac{q\mu}{4\pi\epsilon_0 r^2}\mathrm{e}^{-\mu r} + \frac{q\mu^2}{4\pi\epsilon_0 r}\mathrm{e}^{-\mu r}\)
05

Calculate the Laplacian

Now that we have obtained the second derivative, we will plug it into the Laplacian operator: \(\nabla^2\phi(r) = \frac{1}{r^2}\frac{\partial}{\partial r}\left(r^2\frac{\partial \phi}{\partial r}\right) = \frac{1}{r^2}\left(4\pi r^2\frac{\partial^2 \phi}{\partial r^2}\right)\) Simplifying, we get: \(\nabla^2\phi(r) = \frac{2q}{\epsilon_0}\mathrm{e}^{-\mu r} - \frac{q\mu^2}{\epsilon_0}\mathrm{e}^{-\mu r}\)
06

Calculate the charge density

Now we can use Poisson's equation to find the charge density: \(-\frac{\rho(r)}{\epsilon_0} = \frac{2q}{\epsilon_0}\mathrm{e}^{-\mu r} - \frac{q\mu^2}{\epsilon_0}\mathrm{e}^{-\mu r}\) Solving for \(\rho(r)\), we get: \(\rho(r) = -2q\mathrm{e}^{-\mu r} + q\mu^2\mathrm{e}^{-\mu r}\)
07

Find the total charge throughout space excluding the origin

To find the total charge throughout space, excluding the origin, we will integrate the charge density over the volume of the space: \(Q = \int_{0}^{\infty}\int_{0}^{\pi}\int_{0}^{2\pi}\rho(r)r^2\sin(\theta)drd\theta d\phi\) Here, we're using the fact that \(Q = \int_{V}\rho(r)dV\) where V is the volume of space. Now integrating, we let the theta and phi integrals go from 0 to pi and 0 to 2pi respectively. This results in \(4\pi\) as the factor for those integrals. The integration with respect to r would give us the remaining part: \(Q = 4\pi\int_{0}^{\infty}(-2q\mathrm{e}^{-\mu r} + q\mu^2\mathrm{e}^{-\mu r}) r^2 dr\) Now, we need to integrate the two parts separately: \(Q = 4\pi\left(-2q\int_{0}^{\infty}r^2\mathrm{e}^{-\mu r} dr + q\mu^2\int_{0}^{\infty}r^2\mathrm{e}^{-\mu r} dr\right)\) Using integration by parts and evaluating the integrals, we find that they diverge. Thus, the total charge in space excluding the origin is infinite.

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Most popular questions from this chapter

Two small identical uniform spheres of density \(\rho\) and radius \(r\) are orbiting the Earth in a circular orbit of radius \(a\). Given that the spheres are just touching, with their centres in line with the Earth's centre, and that the only force between them is gravitational, show that they will be pulled apart by the Earth's tidal force if \(a\) is less than \(a_{c}=\) \(2\left(\rho_{\mathrm{E}} / \rho\right)^{1 / 3} R_{\mathrm{E}}\), where \(\rho_{\mathrm{E}}\) is the mean density of the Earth and \(R_{\mathrm{E}}\) its radius. (This is an illustration of the existence of the Roche limit, within which small planetoids would be torn apart by tidal forces. The actual limit is larger than the one found here, because the spheres themselves would be distorted by the tidal force, thus enhancing the effect. It is \(a_{\mathrm{c}}=2.45\left(\rho_{\mathrm{E}} / \rho\right)^{1 / 3} R_{\mathrm{E}} .\) For the mean density of the Moon, for example, \(\rho=3.34 \times 10^{3} \mathrm{~kg} \mathrm{~m}^{-3}\), this gives \(\left.a_{\mathrm{c}}=2.89 R_{\mathrm{E}} \cdot\right)\)

Show that the work done in bringing two charges \(q_{1}\) and \(q_{2}\), initially far apart, to a separation \(r_{12}\) is \(q_{1} q_{2} / 4 \pi \epsilon_{0} r_{12}\). Write down the corresponding expression for a system of many charges. Show that the energy stored in the charge distribution is $$ V=\frac{1}{2} \sum_{j} q_{j} \phi_{j}\left(\boldsymbol{r}_{j}\right) $$ where \(\phi_{j}\left(\boldsymbol{r}_{j}\right)\) is the potential at \(\boldsymbol{r}_{j}\) due to all the other charges. Why does a factor of \(\frac{1}{2}\) appear here, but not in the corresponding expression for the potential energy in an external potential \(\phi(\boldsymbol{r}) ?\)

Find the potential and electric field at points on the axis of symmetry of a uniformly charged flat circular disc of charge \(q\) and radius \(a\). What happens to the field if we keep the charge per unit area \(\sigma=q / \pi a^{2}\) fixed, and let \(a \rightarrow \infty\) ?

Suppose that at some time the Moon had been ocean-covered and rotating relative to the Earth. Find the ratio between the heights of the tides raised on the Moon by the Earth and on the Earth by the Moon. (The Moon's radius is \(R_{\mathrm{M}}=0.27 R_{\mathrm{E}}\).) Estimate how high the tides on the Moon would have been when the Earth-Moon distance was \(10 R_{\mathrm{E}}\).

*Show that the moment of the solar tidal force \(m \boldsymbol{g}_{\mathrm{S}}\) on an Earth satellite is $$m \boldsymbol{r} \wedge \boldsymbol{g}_{\mathrm{S}}=\frac{3 G M_{\mathrm{S}} m}{a_{\mathrm{S}}^{5}}\left(\boldsymbol{r} \cdot \boldsymbol{a}_{\mathrm{S}}\right)\left(\boldsymbol{r} \wedge \boldsymbol{a}_{\mathrm{S}}\right)$$ where \(a_{\mathrm{S}}\) is the position vector of the Sun relative to the Earth. Consider the effect on the Moon, whose orbit is inclined at \(\alpha=5^{\circ}\) to the ecliptic (the Earth's orbital plane). Introduce axes \(i\) and \(j\) in the plane of the ecliptic, with \(\boldsymbol{i}\) in the direction where the Moon's orbit crosses it. Write down the positions of the Sun and Moon, relative to Earth, as functions of time. By averaging both over a month and over a year (i.e., over the positions in their orbits of both bodies), show that the moment leads to a precession of the Moon's orbital plane, at a precessional angular velocity $$ \boldsymbol{\Omega}=-\frac{3 \varpi^{2}}{4 \omega} \cos \alpha \boldsymbol{k} $$ where \(\varpi\) is the Earth's orbital angular velocity. Compute the precessional period. (Note that this calculation is only approximately correct.)

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