JEE Challenger
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Magnitude of Induced Electric Field in Changing Magnetic Field

Comprehension Passage

Consider a point charge QQ moving along a circular orbit with radius RR within the x−yx-y plane at an angular velocity ω\omega. This setup may be treated as equivalent to a current loop carrying a steady current Qω2π\frac{Q\omega}{2\pi}. A uniform magnetic field parallel to the positive zz-axis is then turned on, increasing at a uniform rate from 00 to BB over a duration of one second. Assume the orbit's radius stays constant. Applying this magnetic field induces an electromotive force (emf) along the orbit, defined as the work performed by the induced electric field to move a unit positive charge along the loop. Furthermore, for an orbiting charge, its magnetic dipole moment is directly proportional to its angular momentum via a proportionality constant γ\gamma.

Find the magnitude of the electric field induced in the orbit at any instant during the period in which the magnetic field is changing.

Options

A

BR4\frac{BR}{4}

B

BR2\frac{BR}{2}

Correct
C

BRBR

D

2BR2BR

Step-by-Step Solution

To find the magnitude of the electric field induced in the circular orbit during the period in which the magnetic field is changing, we use Faraday's Law of Electromagnetic Induction.

1. Rate of Change of Magnetic Field

The magnetic field increases at a uniform rate from 00 to BB over a duration of Δt=1 second\Delta t = 1\text{ second}. Therefore, the rate of change of the magnetic field with respect to time, dBdt\frac{dB}{dt}, is: dBdt=B−01=B\frac{dB}{dt} = \frac{B - 0}{1} = B

2. Magnetic Flux Through the Orbit

The circular orbit has a constant radius RR. The area enclosed by the circular path is: A=πR2A = \pi R^2

Since the magnetic field is uniform and perpendicular to the x−yx-y plane (parallel to the zz-axis), the magnetic flux ΦB\Phi_B through the loop is: ΦB=B⋅A=B(πR2)\Phi_B = B \cdot A = B (\pi R^2)

The rate of change of magnetic flux is given by: dΦBdt=AdBdt=πR2B\frac{d\Phi_B}{dt} = A \frac{dB}{dt} = \pi R^2 B

3. Induced Electromotive Force (emf) and Induced Electric Field

According to Faraday's Law, the magnitude of the induced electromotive force (E\mathcal{E}) around the circular orbit is equal to the rate of change of magnetic flux: E=∣−dΦBdt∣=πR2B\mathcal{E} = \left| -\frac{d\Phi_B}{dt} \right| = \pi R^2 B

The induced emf is also defined as the line integral of the induced electric field E⃗\vec{E} along the circular loop: E=∮E⃗⋅dl⃗\mathcal{E} = \oint \vec{E} \cdot d\vec{l}

Due to cylindrical symmetry, the magnitude of the induced electric field EE is constant at every point along the circular path of radius RR, and its direction is tangential to the path. Thus: E=E∮dl=E(2πR)\mathcal{E} = E \oint dl = E (2\pi R)

4. Equating both Expressions for Induced emf

E(2πR)=πR2BE (2\pi R) = \pi R^2 B

Solving for EE: E=πR2B2πR=BR2E = \frac{\pi R^2 B}{2\pi R} = \frac{BR}{2}

Thus, the magnitude of the induced electric field at any instant during this time interval is BR2\frac{BR}{2}.

Correct Option: B