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The cylindrical surface \(\rho=8 \mathrm{~cm}\) contains the surface charge density, \(\rho_{S}=\) \(5 e^{-20|z|} \mathrm{nC} / \mathrm{m}^{2} .(a)\) What is the total amount of charge present? \((b)\) How much electric flux leaves the surface \(\rho=8 \mathrm{~cm}, 1 \mathrm{~cm}

Short Answer

Expert verified
\(Φ_E = 5 (8\,\mathrm{cm}) k \left[ \frac{1}{20} (e^{-80} - e^{-20}) \right] (60^\circ)\) \(Φ_E = 40 k \left[ \frac{1}{20} (e^{-80} - e^{-20}) \right] (60^\circ)\) Thus, the electric flux leaving the surface within the specified limits for z and φ is given by \(40 k \left[ \frac{1}{20} (e^{-80} - e^{-20}) \right] (60^\circ)\).

Step by step solution

01

Surface Charge Density Expression

First, we need to write down the surface charge density expression given in the problem. The surface charge density is given as: \(\rho_S = 5 e^{-20|z|} \mathrm{nC/m^2}\)
02

Calculate Total Charge Present

To find the total charge present on the cylindrical surface, we need to integrate the surface charge density over the entire surface. For a cylindrical surface, the surface area dA can be written as: \(dA = \rho d\phi dz\) The total charge can be calculated by integrating over the entire surface area: \(Q = \int\int \rho_S dA = \int\int 5 e^{-20|z|} d(\rho d\phi dz)\) Since \(\rho\) is constant (8 cm), we integrate with respect to \(\phi\) from 0 to \(2\pi\), and z from \(-\infty\) to \(\infty\). \(Q = 5\rho \int_{0}^{2\pi} d\phi \int_{-\infty}^{\infty} e^{-20|z|} dz\) Now, let's separate the integral into two parts: \(Q = 5\rho \int_{0}^{2\pi} d\phi \left[\int_{-\infty}^{0} e^{20z} dz + \int_{0}^{\infty} e^{-20z} dz\right]\) Let's evaluate these integrals: \(Q = 5\rho \int_{0}^{2\pi} d\phi \left[ \frac{1}{20}(e^{20z}\big|_{-\infty}^{0} - e^{-20z}\big|_{0}^{\infty})\right]\) \(Q = 5\rho \int_{0}^{2\pi} d\phi \left[\frac{1}{20}(1 + 1)\right]\) Finally, we can evaluate the integral: \(Q = \frac{1}{2} \rho \int_{0}^{2\pi} 5 d\phi\) \(Q = \frac{1}{2} \rho (10\pi) = 40\pi \mathrm{nC}\) So, the total amount of charge present on the cylindrical surface is \(40\pi\) nC.
03

Calculate Electric Flux

Next, we need to calculate the electric flux leaving the surface within the specified limits for z and φ. Electric flux is given by: \(Φ_E = \int\int \mathbf{E} \cdot d\mathbf{A}\) \(\rho_S = 5 e^{-20|z|}\) nC/m² is the surface charge density and the electric field is proportional to the surface charge density, so we can write: \(\mathbf{E} \cdot d\mathbf{A} = k \rho_S dA\), where k is a constant. Now we need to integrate this expression within the given limits: \(Φ_E = \rho k \int_{1 \mathrm{cm}}^{5\mathrm{cm}} dz \int_{30^\circ}^{90^\circ} 5 e^{-20|z|} d\phi\) The integral is separable, and we can calculate it as: \(Φ_E = 5\rho k \int_{1 \mathrm{cm}}^{5\mathrm{cm}} e^{-20z} dz \int_{30^\circ}^{90^\circ} d\phi\) Solving the integrals, we get: \(Φ_E = 5\rho k \left[ \frac{1}{20} (e^{-20(5\,\mathrm{cm}-1\, \mathrm{cm})} - e^{-20(1\,\mathrm{cm})})\right]\left[(90^\circ - 30^\circ)\right]\) \(Φ_E = 5\rho k \left[ \frac{1}{20} (e^{-80} - e^{-20}) \right] (60^\circ)\) To compute the final answer, we plug in the value for \(\rho\): MessageLookup

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Key Concepts

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

Surface Charge Density
Surface charge density is a critical concept in electromagnetism that deals with the amount of charge per unit area on a surface. In our cylindrical surface problem, the surface charge density is represented by the variable \(\rho_S\) and is given by the expression \(\rho_S = 5 e^{-20|z|} \mathrm{nC/m^2}\). This depicts how charge density varies with the distance along the z-axis in an exponential manner, decreasing as you move away from the center. When calculating the total charge present, we integrate this density over the entire surface area to account for every portion of charge across the surface. This integral is essential for understanding how much charge is distributed over the cylindrical surface and provides the groundwork for calculating electric properties like potential and field strength around the surface.

To enhance understanding, consider surface charge density similar to the coating of paint on a surface – where the density would indicate how thickly the paint is laid out over each unit area. In our case, it's the 'paint' of electric charge across our cylindrical surface.
Electric Flux
Electric flux is a measure of how much electric field passes through a given area. It's an important concept which helps understand how fields interact with surfaces. The mathematical representation of electric flux \(\Phi_E\) is integral to our problem, where we need to find the quantity of electric flux leaving a specified part of the charge-carrying surface.

In the context of our exercise, electric flux is proportional to the surface charge density. By integrating the surface charge density over a certain part of the surface area, using the formula \(\Phi_E = \int\int \mathbf{E} \cdot d\mathbf{A}\), we calculate the electric flux emanating from the surface within given z and φ limits. The concept can be visualized like the flow of water through a net; the water represents the electric field, while the net embodies the specific surface area through which we assess the flow.
Cylindrical Coordinates
Cylindrical coordinates are a means of describing the position of a point in a 3D space, particularly suited for objects with cylindrical symmetry, much like the surface in our problem. The system uses three values: the radial distance from the origin \(\rho\), the azimuthal angle \(\phi\) around the z-axis, and the height \(z\) along the z-axis.

For the problem at hand, we don't vary the radial distance \(\rho\) as it's given as 8 cm, but we do consider the variation in \(z\) along the height and \(\phi\) around the axis to find out the charge and flux within certain sections of the cylindrical surface. By using cylindrical coordinates, we inherently tailor the calculation processes such as integration, to the shape and symmetry of the object we're examining, thus simplifying our computations. It's akin to choosing the right tool for the job, ensuring efficiency and precision in our calculations.

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Most popular questions from this chapter

Calculate \(\nabla \cdot \mathbf{D}\) at the point specified if \((a) \mathbf{D}=\left(1 / z^{2}\right)\left[10 x y z \mathbf{a}_{x}+\right.\) \(\left.5 x^{2} z \mathbf{a}_{y}+\left(2 z^{3}-5 x^{2} y\right) \mathbf{a}_{z}\right]\) at \(P(-2,3,5) ;(b) \mathbf{D}=5 z^{2} \mathbf{a}_{\rho}+10 \rho z \mathbf{a}_{z}\) at \(P\left(3,-45^{\circ}, 5\right) ;(c) \mathbf{D}=2 r \sin \theta \sin \phi \mathbf{a}_{r}+r \cos \theta \sin \phi \mathbf{a}_{\theta}+r \cos \phi \mathbf{a}_{\phi}\) at \(P\left(3,45^{\circ},-45^{\circ}\right) .\)

A certain light-emitting diode (LED) is centered at the origin with its surface in the \(x y\) plane. At far distances, the LED appears as a point, but the glowing surface geometry produces a far-field radiation pattern that follows a raised cosine law: that is, the optical power (flux) density in watts \(/ \mathrm{m}^{2}\) is given in spherical coordinates by $$ \mathbf{P}_{d}=P_{0} \frac{\cos ^{2} \theta}{2 \pi r^{2}} \mathbf{a}_{r} \quad \text { watts } / \mathrm{m}^{2} $$ where \(\theta\) is the angle measured with respect to the direction that is normal to the LED surface (in this case, the \(z\) axis), and \(r\) is the radial distance from the origin at which the power is detected. \((a)\) In terms of \(P_{0}\), find the total power in watts emitted in the upper half-space by the LED; (b) Find the cone angle, \(\theta_{1}\), within which half the total power is radiated, that is, within the range \(0<\theta<\theta_{1} ;\) ( \(c\) ) An optical detector, having a \(1-\mathrm{mm}^{2}\) cross-sectional area, is positioned at \(r=1 \mathrm{~m}\) and at \(\theta=45^{\circ}\), such that it faces the \(\mathrm{LED}\). If one milliwatt is measured by the detector, what (to a very good estimate) is the value of \(P_{0}\) ?

Suppose that the Faraday concentric sphere experiment is performed in free space using a central charge at the origin, \(Q_{1}\), and with hemispheres of radius a. A second charge \(Q_{2}\) (this time a point charge) is located at distance \(R\) from \(Q_{1}\), where \(R>>a .(a)\) What is the force on the point charge before the hemispheres are assembled around \(Q_{1} ?\) (b) What is the force on the point charge after the hemispheres are assembled but before they are discharged? ( \(c\) ) What is the force on the point charge after the hemispheres are assembled and after they are discharged? ( \(d\) ) Qualitatively, describe what happens as \(Q_{2}\) is moved toward the sphere assembly to the extent that the condition \(R>>a\) is no longer valid.

Use Gauss's law in integral form to show that an inverse distance field in spherical coordinates, \(\mathbf{D}=A a_{r} / r\), where \(A\) is a constant, requires every spherical shell of \(1 \mathrm{~m}\) thickness to contain \(4 \pi A\) coulombs of charge. Does this indicate a continuous charge distribution? If so, find the charge density variation with \(r\).

In a region in free space, electric flux density is found to be $$ \mathbf{D}=\left\\{\begin{array}{lr} \rho_{0}(z+2 d) \mathbf{a}_{z} \mathrm{C} / \mathrm{m}^{2} & (-2 d \leq z \leq 0) \\ -\rho_{0}(z-2 d) \mathbf{a}_{z} \mathrm{C} / \mathrm{m}^{2} & (0 \leq z \leq 2 d) \end{array}\right. $$ Everywhere else, \(\mathbf{D}=0 .\left(\right.\) a) Using \(\nabla \cdot \mathbf{D}=\rho_{v}\), find the volume charge density as a function of position everywhere. (b) Determine the electric flux that passes through the surface defined by \(z=0,-a \leq x \leq a,-b \leq y \leq b\). (c) Determine the total charge contained within the region \(-a \leq x \leq a\), \(-b \leq y \leq b,-d \leq z \leq d .(d)\) Determine the total charge contained within the region \(-a \leq x \leq a,-b \leq y \leq b, 0 \leq z \leq 2 d\).

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