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Question: A point charge $q$ is fixed at origin. The electric flux passing through infinite surface at $x=a$ a...

A point charge qq is fixed at origin. The electric flux passing through infinite surface at x=ax=a and parallel to yzy-z plane is qnϵ0\frac{q}{n\epsilon_0}. Find nn.

Answer

2

Explanation

Solution

The problem asks us to find the value of nn if the electric flux passing through an infinite surface at x=ax=a (parallel to the yzy-z plane) due to a point charge qq fixed at the origin is given as qnϵ0\frac{q}{n\epsilon_0}.

1. Understanding Electric Flux and Gauss's Law: According to Gauss's Law, the total electric flux through any closed surface enclosing a charge qq is given by Φtotal=qϵ0\Phi_{total} = \frac{q}{\epsilon_0}. This flux emanates radially outwards from the point charge in all directions.

2. Solid Angle Concept: The total solid angle subtended by all directions around a point charge is 4π4\pi steradians. The electric flux through any surface is proportional to the solid angle subtended by that surface at the charge's location. Φ=q4πϵ0Ω\Phi = \frac{q}{4\pi\epsilon_0} \Omega, where Ω\Omega is the solid angle.

3. Analyzing the Given Surface: The surface is an infinite plane located at x=ax=a and parallel to the yzy-z plane. The point charge qq is at the origin (0,0,0)(0,0,0). This infinite plane divides the entire space into two half-spaces: one where x<ax < a and another where x>ax > a. Assuming a>0a > 0 (as suggested by the diagram), the charge is located in the half-space x<ax < a. All electric field lines originating from the charge and directed towards the positive x-axis (i.e., into the half-space x>0x>0) will pass through this infinite plane at x=ax=a.

4. Solid Angle Subtended by an Infinite Plane: An infinite plane, when viewed from a point not on the plane, subtends a solid angle of 2π2\pi steradians. This is because the plane essentially "cuts" space into two equal halves. The field lines going into one of these halves will pass through the plane. In this case, the plane at x=ax=a intercepts all the electric field lines that are directed into the x>0x>0 half-space. The solid angle corresponding to this half-space (or this infinite plane) from the origin is 2π2\pi steradians.

5. Calculating the Electric Flux: Since the solid angle subtended by the infinite plane at the origin is Ω=2π\Omega = 2\pi, the electric flux passing through it is: Φ=q4πϵ0Ω=q4πϵ0(2π)\Phi = \frac{q}{4\pi\epsilon_0} \Omega = \frac{q}{4\pi\epsilon_0} (2\pi) Φ=q2ϵ0\Phi = \frac{q}{2\epsilon_0}

6. Comparing with the Given Flux: The problem states that the electric flux is qnϵ0\frac{q}{n\epsilon_0}. Comparing our calculated flux with the given expression: q2ϵ0=qnϵ0\frac{q}{2\epsilon_0} = \frac{q}{n\epsilon_0} From this, we can clearly see that n=2n=2.

Alternative Method (Direct Integration): The electric field due to a point charge qq at the origin at a point (x,y,z)(x,y,z) is given by: E=q4πϵ0rr3=q4πϵ0xi^+yj^+zk^(x2+y2+z2)3/2\vec{E} = \frac{q}{4\pi\epsilon_0} \frac{\vec{r}}{|\vec{r}|^3} = \frac{q}{4\pi\epsilon_0} \frac{x\hat{i} + y\hat{j} + z\hat{k}}{(x^2+y^2+z^2)^{3/2}} For the surface at x=ax=a, the differential area vector is dA=dydzi^d\vec{A} = dy dz \hat{i}. The electric flux Φ\Phi is given by EdA\iint \vec{E} \cdot d\vec{A}: Φ=y=z=(q4πϵ0ai^+yj^+zk^(a2+y2+z2)3/2)(dydzi^)\Phi = \iint_{y=-\infty}^{\infty} \int_{z=-\infty}^{\infty} \left( \frac{q}{4\pi\epsilon_0} \frac{a\hat{i} + y\hat{j} + z\hat{k}}{(a^2+y^2+z^2)^{3/2}} \right) \cdot (dy dz \hat{i}) Φ=qa4πϵ0y=z=dydz(a2+y2+z2)3/2\Phi = \frac{qa}{4\pi\epsilon_0} \iint_{y=-\infty}^{\infty} \int_{z=-\infty}^{\infty} \frac{dy dz}{(a^2+y^2+z^2)^{3/2}} To evaluate this integral, convert to polar coordinates in the yzy-z plane: let y=Rcosθy = R\cos\theta, z=Rsinθz = R\sin\theta, so y2+z2=R2y^2+z^2 = R^2 and dydz=RdRdθdy dz = R dR d\theta. The limits are RR from 00 to \infty and θ\theta from 00 to 2π2\pi. Φ=qa4πϵ002πdθ0RdR(a2+R2)3/2\Phi = \frac{qa}{4\pi\epsilon_0} \int_{0}^{2\pi} d\theta \int_{0}^{\infty} \frac{R dR}{(a^2+R^2)^{3/2}} The integral with respect to θ\theta is 2π2\pi. For the integral with respect to RR: let u=a2+R2u = a^2+R^2, so du=2RdRdu = 2R dR. 0RdR(a2+R2)3/2=a212u3/2du=12[u1/21/2]a2=[u1/2]a2=[1u]a2\int_{0}^{\infty} \frac{R dR}{(a^2+R^2)^{3/2}} = \int_{a^2}^{\infty} \frac{1}{2} u^{-3/2} du = \frac{1}{2} \left[ \frac{u^{-1/2}}{-1/2} \right]_{a^2}^{\infty} = \left[ -u^{-1/2} \right]_{a^2}^{\infty} = \left[ -\frac{1}{\sqrt{u}} \right]_{a^2}^{\infty} =(limu1u1a2)=(01a)=1a= -\left( \lim_{u\to\infty} \frac{1}{\sqrt{u}} - \frac{1}{\sqrt{a^2}} \right) = -\left( 0 - \frac{1}{a} \right) = \frac{1}{a} Substitute these results back into the flux equation: Φ=qa4πϵ0(2π)(1a)=q2ϵ0\Phi = \frac{qa}{4\pi\epsilon_0} (2\pi) \left( \frac{1}{a} \right) = \frac{q}{2\epsilon_0} Comparing this with qnϵ0\frac{q}{n\epsilon_0}, we find n=2n=2.

The final answer is 2\boxed{2}.

Explanation of the solution: The total electric flux from a point charge qq is q/ϵ0q/\epsilon_0. An infinite plane passing through space effectively divides the space into two halves. Since the charge is located on one side of the plane, and the plane extends infinitely, it intercepts exactly half of the total electric field lines emanating from the charge. Therefore, the electric flux passing through the infinite plane is half of the total flux, i.e., 12qϵ0\frac{1}{2} \frac{q}{\epsilon_0}. Comparing this with the given flux qnϵ0\frac{q}{n\epsilon_0}, we find n=2n=2.