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A point charge causes an electric flux of \(-2 \times 10^4 \mathrm{Nm}^2 \mathrm{C}^{-1}\) to pass through a spherical Gaussian surface of 8.0 cm radius, centred on the charge. The value of the point charge is : [JEE Main 2025]
(Given \(\epsilon_0=8.85 \times 10^{-12} \mathrm{C}^2 \mathrm{~N}^{-1} \mathrm{~m}^{-2}\) )
(b) Given an electric flux \(\phi=-2 \times 10^4 \mathrm{Nm}^2 \mathrm{C}^{-1}\) through a spherical Gaussian surface with a radius of \(8.0 \mathrm{~cm}(r=0.08 \mathrm{~m})\), we are to find the value of the point charge \(Q\).
According to Gauss’s Law: \(\phi=\frac{Q}{\varepsilon_0}\)
Where \(\varepsilon_0=8.85 \times 10^{-12} \mathrm{C}^2 \mathrm{~N}^{-1} \mathrm{~m}^{-2}\).
Rearranging the equation to solve for \(Q\), we have:
\(
Q=\phi \varepsilon_0
\)
Substituting the given values:
\(
Q=-2 \times 10^4 \times 8.85 \times 10^{-12}
\)
Calculating this yields:
\(
Q=-17.7 \times 10^{-8} \mathrm{C}
\)
Thus, the value of the point charge is \(Q=-17.7 \times 10^{-8} \mathrm{C}\).
An electric dipole is placed at a distance of 2 cm from an infinite plane sheet having positive charge density \(\sigma_0\). Choose the correct option from the following. [JEE Main 2025]
(c) We know, electric field due to uniformly charged infinite plane sheet,
\(
E=\frac{\sigma_0}{2 \varepsilon_0}
\)
\(
\vec{\tau}=\vec{{P}} \times \vec{{E}}
\)
The electric field is uniform, and there is no variation in the field across the dipole, meaning the torque on the dipole is zero.
Also, the dipole is in the minimum potential energy configuration when aligned with the electric field, and the net force on the dipole due to the uniform electric field is zero.
Therefore, the potential energy of the dipole is minimum, and the torque is zero.
An electric dipole of mass \(m\), charge \(q\), and length \(l\) is placed in a uniform electric field \(\vec{E}=E_0 \hat{i}\). When the dipole is rotated slightly from its equilibrium position and released, the time period of its oscillations will be : [JEE Main 2025]
(b) The torque acting on a dipole in a uniform electric field is:
\(
\begin{gathered}
\tau=p \times E \\
\tau=p E_0 \sin \theta
\end{gathered}
\)
\(
\text { Dipole moment: } p=q l
\)
\(
\tau=q l E_0 \sin \theta
\)
For small angles, \(\sin \theta \approx \theta\), so:
\(
\tau \approx q l E_0 \theta
\)
Using Newton’s second law for rotational motion:
\(
I \alpha=\tau
\)
\(\alpha=\frac{d^2 \theta}{d t^2}\) is the angular acceleration.
For a dipole (two point masses \(q\) separated by \(l\) ), the moment of inertia about the center is:
\(
I=m\left(\frac{l}{2}\right)^2+m\left(\frac{l}{2}\right)^2=2 m \frac{l^2}{4}=\frac{m l^2}{2}
\)
So the equation of motion becomes:
\(
\begin{aligned}
& \frac{m l^2}{2} \frac{d^2 \theta}{d t^2}=-q l E_0 \theta \\
& \frac{d^2 \theta}{d t^2}+\frac{2 q E_0}{m l} \theta=0
\end{aligned}
\)
This is the standard form of simple harmonic motion:
\(
\frac{d^2 \theta}{d t^2}+\omega^2 \theta=0
\)
where:
\(
\omega^2=\frac{2 q E_0}{m l}
\)
Thus, the angular frequency is:
\(
\omega=\sqrt{\frac{2 q E_0}{m l}}
\)
The time period of oscillation is given by:
\(
\begin{gathered}
T=\frac{2 \pi}{\omega} \\
T=2 \pi \sqrt{\frac{m l}{2 q E_0}}
\end{gathered}
\)
Match List-I with List-II
(d)
(A) \(\rightarrow 0\) (III)
(B) \(\rightarrow \frac{\sigma}{2 \varepsilon_0}\)
(C) \(\rightarrow \frac{\sigma \mathrm{R}^2}{\varepsilon_0 \mathrm{I}^2}\) (No row matching)
(D) \(\rightarrow \frac{\sigma}{\varepsilon_0}({I})\)
Three infinitely long wires with linear charge density \(\lambda\) are placed along the \(x\)-axis, \(y\)-axis and \(z\)-axis respectively. Which of the following denotes an equipotential surface? [JEE Main 2025]
(a) Electric field due to infinitely long wire
\(
\vec{E}=-\frac{2 k \lambda}{r} \hat{r}
\)
We know, \(V=-\int \vec{E} \cdot \overrightarrow{d r}\)
\(
\begin{aligned}
& =-\int \frac{-2 k \lambda}{r} \hat{r} \cdot \overrightarrow{d r} \\
& V=\int \frac{2 k \lambda}{r} d r=2 k \lambda \ln r+c
\end{aligned}
\)
Net potential due to all wires,
\(
\begin{aligned}
& V=v_1+v_2+v_3 \\
& =2 k \lambda \ln \left(\sqrt{x^2+y^2}\right)+2 k \lambda \ln \left(\sqrt{y^2+z^2}\right)+2 k \lambda \ln \left(\sqrt{z^2+x^2}\right)+c
\end{aligned}
\)
for equipotential surface, \(V=c\)
\(
\begin{aligned}
& \Rightarrow 2 k \lambda\left[\ln \left(\sqrt{x^2+y^2} \cdot \sqrt{y^2+z^2} \cdot \sqrt{z^2+x^2}\right)\right]=c \\
& \Rightarrow \sqrt{\left(x^2+y^2\right) \cdot\left(y^2+z^2\right) \cdot\left(z^2+x^2\right)}=c \\
& \Rightarrow\left(x^2+y^2\right)\left(y^2+z^2\right)\left(z^2+x^2\right)=c
\end{aligned}
\)
where, c = constant.
A particle of mass ‘ \(m\) ‘ and charge ‘ \(q\) ‘ is fastened to one end ‘ \(A\) ‘ of a massless string having equilibrium length \(l\), whose other end is fixed at point ‘ \(O^{\prime}\) ‘. The whole system is placed on a frictionless horizontal plane and is initially at rest. If uniform electric field is switched on along the direction as shown in the figure, then the speed of the particle when it crosses the \(x\)-axis is [JEE Main 2025]
(c)
Explanation:
To find the speed of the particle when it crosses the \(x\)-axis, we can use the concept of energy conservation. The work done by the electric field on the particle will be equal to the change in kinetic energy of the particle.
The force acting on the particle due to the electric field is given by \(F=q E\). The work done by this force when the particle moves a distance \(L\) is \(W=F \cdot d=q E \cdot L\).
The change in kinetic energy is given by \(\Delta K E=\frac{1}{2} m v^2-O=\frac{1}{2} m v^2\). Setting the work done equal to the change in kinetic energy gives us: \(q E \cdot L=\frac{1}{2} m v^2\).
Rearranging this equation to solve for \(v\) gives us: \(v=\sqrt{\frac{2 q E L}{m}}\). Therefore, the speed of the particle when it crosses the x-axis is \(v=\sqrt{\frac{2 q E L}{m}}\).
Step by Step Solution:
Step 1: Identify the forces acting on the particle. The only force acting on the particle is the electric force due to the electric field. which is \(F=q E\).
Step 2: Calculate the work done by the electric field when the particle moves a distance \(L\) : \(W=F \cdot d=q E \cdot L\).
Step 3: Use the work-energy principle: the work done is equal to the change in kinetic energy. Set the work done equal to the change in kinetic energy: \(q E \cdot L=\frac{1}{2} m v^2\).
Step 4: Rearrange the equation to solve for the speed \(v: v=\sqrt{\frac{2 q E L}{m}}\).
Final Answer: \(v=\sqrt{\frac{2 q E L}{m}}\)
A small uncharged conducting sphere is placed in contact with an identical sphere but having \(4 \times 10^{-8} \mathrm{C}\) charge and then removed to a distance such that the force of repulsion between them is \(9 \times 10^{-3} \mathrm{~N}\). The distance between them is (Take \(\frac{1}{4 \pi \epsilon_{\mathrm{o}}}\) as \(9 \times 10^9\) in SI units) [JEE Main 2025]
(b) Charge on one sphere: \(q_1=4 \times 10^{-8} \mathrm{C}\)
Force of repulsion: \(F=9 \times 10^{-3} \mathrm{~N}\)
Constant: \(k=\frac{1}{4 \pi \epsilon_{\mathrm{o}}}=9 \times 10^9 \frac{\mathrm{~N} \cdot \mathrm{~m}^2}{\mathrm{C}^2}\)
When two identical conducting spheres come into contact, the charge is evenly distributed between them.
Coulomb’s law: \(F=k \frac{\left|q_1 q_2\right|}{r^2}\)
Calculate the charge on each sphere after contact
When the uncharged sphere touches the charged sphere, the charge is distributed equally.
Each sphere will have a charge of:
\(q=\frac{q_1+0}{2}=\frac{4 \times 10^{-8} \mathrm{C}}{2}=2 \times 10^{-8} \mathrm{C}\)
Apply Coulomb’s law
The force between the spheres is given by:
\(F=k \frac{q^2}{r^2}\)
Where \(r\) is the distance between the spheres.
Solve for the distance \(r\)
Rearrange the formula to solve for \(r\) :
\(r^2=k \frac{q^2}{F}\)
\(r=\sqrt{k \frac{q^2}{F}}\)
\(
\begin{aligned}
&\text { Substitute the values and calculate } r\\
&\begin{aligned}
r & =\sqrt{\left(9 \times 10^9 \frac{\mathrm{~N} \cdot \mathrm{~m}^2}{\mathrm{C}^2}\right) \frac{\left(2 \times 10^{-8} \mathrm{C}\right)^2}{9 \times 10^{-3} \mathrm{~N}}} \\
r & =\sqrt{\left(9 \times 10^9\right) \frac{4 \times 10^{-16}}{9 \times 10^{-3}} \mathrm{~m}} \\
r & =\sqrt{4 \times 10^{-4}} \mathrm{~m} \\
r & =2 \times 10^{-2} \mathrm{~m} \\
r & =2 \mathrm{~cm}
\end{aligned}
\end{aligned}
\)
In the first configuration (1) as shown in the figure, four identical charges \(\left(q_0\right)\) are kept at the corners A, B, C and D of square of side length ‘ \(\boldsymbol{a}\) ‘. In the second configuration (2), the same charges are shifted to mid points \(G, E, H\) and \(F\), of the square. If \(K=\frac{1}{4 \pi \epsilon_0}\), the difference between the potential energies of configuration (2) and (1) is given by : [JEE Main 2025]
(d)
\(
\begin{gathered}
\mathrm{U}_1=\frac{4 \mathrm{Kq}_0^2}{\mathrm{a}}+\frac{2 \mathrm{Kq}_0^2}{\sqrt{2} \mathrm{a}}=\frac{\mathrm{Kq}_0^2}{\mathrm{a}}(4+\sqrt{2}) \\
\mathrm{U}_2=\frac{\mathrm{Kq}_0^2}{\left(\frac{\mathrm{a}}{\sqrt{2}}\right)}(4+\sqrt{2})=\frac{\mathrm{Kq}_0^2}{\mathrm{a}}(4 \sqrt{2}+2) \\
\mathrm{U}_2-\mathrm{U}_1=\frac{\mathrm{Kq}_0^2}{\mathrm{a}}(3 \sqrt{2}-2)
\end{gathered}
\)
Consider a parallel plate capacitor of area A (of each plate) and separation ‘ \(d\) ‘ between the plates. If \(E\) is the electric field and \(\varepsilon_0\) is the permittivity of free space between the plates, then potential energy stored in the capacitor is [JEE Main 2025]
(d)
\(
u=\frac{1}{2} \varepsilon_0 E^2
\)
The energy density of an electric field in free space is given by the expression above. For a parallel plate capacitor with plate area \(A\) and separation \(d\), the volume between the plates is
\(
V=A d
\)
Multiplying the energy density by the volume gives the total energy stored:
\(
U=u \times V=\frac{1}{2} \varepsilon_0 E^2 \times A d=\frac{1}{2} \varepsilon_0 E^2 A d
\)
Thus, the potential energy stored in the capacitor is
\(
\frac{1}{2} \varepsilon_0 E^2 A d
\)
Two point charges \(-4 \mu \mathrm{c}\) and \(4 \mu \mathrm{c}\), constituting an electric dipole, are placed at \((-9,0,0) \mathrm{cm}\) and \((9,0,0) \mathrm{cm}\) in a uniform electric field of strength \(10^4 \mathrm{NC}^{-1}\). The work done on the dipole in rotating it from the equilibrium through \(180^{\circ}\) is : [JEE Main 2025]
(d) The work done on an electric dipole in a uniform electric field when it is rotated from an angle \(\theta_1\) to an angle \(\theta_2\) is given by:
\(
W=-p E\left(\cos \theta_2-\cos \theta_1\right)
\)
where:
\(p=q \cdot d\) is the dipole moment,
\(E\) is the electric field strength,
\(\theta_1\) and \(\theta_2\) are the initial and final angles between the dipole moment and the electric field.
Given:
Charge \(q=4 \mu \mathrm{C}=4 \times 10^{-6} \mathrm{C}\)
Distance \(d=18 \mathrm{~cm}=0.18 \mathrm{~m}\)
Electric field \(E=10^4 \mathrm{~N} / \mathrm{C}\)
Initial angle \(\theta_1=0^{\circ}\) (aligned with the field, equilibrium position)
Final angle \(\theta_2=180^{\circ}\)
First, calculate the dipole moment \(p\) :
\(
p=q \cdot d=4 \times 10^{-6} \mathrm{C} \cdot 0.18 \mathrm{~m}=7.2 \times 10^{-7} \mathrm{Cm}
\)
Calculate the work done \(W\) :
\(
\begin{aligned}
& W=-p E\left(\cos 180^{\circ}-\cos 0^{\circ}\right) \\
& W=-7.2 \times 10^{-7} \mathrm{Cm} \cdot 10^4 \mathrm{~N} / \mathrm{C} \cdot(-1-1) \\
& W=7.2 \times 10^{-7} \mathrm{Cm} \cdot 10^4 \mathrm{~N} / \mathrm{C} \cdot 2 \\
& W=1.44 \times 10^{-2} \mathrm{~J}=14.4 \mathrm{~mJ}
\end{aligned}
\)
Two charges \(7 \mu \mathrm{c}\) and \(-4 \mu \mathrm{c}\) are placed at \((-7 \mathrm{~cm}, 0,0)\) and \((7 \mathrm{~cm}, 0,0)\) respectively. Given, \(\epsilon_0=8.85 \times 10^{-12} \mathrm{C}^2 \mathrm{~N}^{-1} \mathrm{~m}^{-2}\), the electrostatic potential energy of the charge configuration is : [JEE Main 2025]
(d) Charge \(q_1=7 \mu \mathrm{C}=7 \times 10^{-6} \mathrm{C}\) at \((-7 \mathrm{~cm}, 0,0)\).
Charge \(q_2=-4 \mu \mathrm{C}=-4 \times 10^{-6} \mathrm{C}\) at \((7 \mathrm{~cm}, 0,0)\).
Permittivity of free space \(\epsilon_0=8.85 \times 10^{-12} \mathrm{C}^2 \mathrm{~N}^{-1} \mathrm{~m}^{-2}\).
The electrostatic potential energy \(U\) between two point charges \(q_1\) and \(q_2\) separated by a distance \(r\) is given by \(U=\frac{1}{4 \pi e_0} \frac{q_1 q_2}{r}\).
Step 1: Calculate the distance \(r\) between the charges.
The coordinates of the charges are \((-0.07 \mathrm{~m}, 0,0)\) and \((0.07 \mathrm{~m}, 0,0)\).
The distance between them is \(r=0.07 \mathrm{~m}-(-0.07 \mathrm{~m})=0.14 \mathrm{~m}\).
Step 2: Calculate the electrostatic potential energy \(U\).
\(
\begin{aligned}
& U=\frac{1}{4 \pi e_0} \frac{q_1 q_2}{r} \\
& U=\frac{1}{4 \pi\left(8.85 \times 10^{-12} \mathrm{C}^2 \mathrm{~N}^{-1} \mathrm{~m}^{-2}\right)} \frac{\left(7 \times 10^{-6} \mathrm{C}\right)\left(-4 \times 10^{-6} \mathrm{C}\right)}{0.14 \mathrm{~m}} \\
& U=\left(8.99 \times 10^9 \mathrm{Nm}^2 \mathrm{C}^{-2}\right) \frac{-28 \times 10^{-12} \mathrm{C}^2}{0.14 \mathrm{~m}} \\
& U=\frac{-0.25172}{0.14} \mathrm{~J} \\
& U=-1.798 \mathrm{~J} \\
& U \approx-1.8 \mathrm{~J}
\end{aligned}
\)
The electrostatic potential energy of the charge configuration is approximately -1.8 J.
A point particle of charge \(Q\) is located at \(P\) along the axis of an electric dipole 1 at a distance \(r\) as shown in the figure. The point P is also on the equatorial plane of a second electric dipole 2 at a distance \(r\) . The dipoles are made of opposite charge q separated by a distance \(2 a\). For the charge particle at P not to experience any net force, which of the following correctly describes the situation? [JEE Main 2025]
(b)
\(
\begin{aligned}
& \frac{\mathrm{kq}}{(\mathrm{r}-\mathrm{a})^2}=\frac{\mathrm{kq}}{(\mathrm{r}+\mathrm{a})^2}+\frac{2 \mathrm{kq}}{\left(\mathrm{r}^2+\mathrm{a}^2\right)} \cos \theta \\
& \frac{1}{(\mathrm{r}-\mathrm{a})^2}=\frac{1}{(\mathrm{r}+\mathrm{a})^2}+\frac{2 \mathrm{a}}{\left(\mathrm{r}^2+\mathrm{a}^2\right)^{\frac{3}{2}}} \\
& \frac{1}{(\mathrm{r}-\mathrm{a})^2}-\frac{1}{(\mathrm{r}+\mathrm{a})^2}=\frac{2 \mathrm{a}}{\left(\mathrm{r}^2+\mathrm{a}^2\right)^{\frac{3}{2}}} \\
& \frac{4 \mathrm{ra}}{\left(\mathrm{r}^2-\mathrm{a}^2\right)^2}=\frac{2 \mathrm{a}}{\left(\mathrm{r}^2+\mathrm{a}^2\right)^{\frac{3}{2}}} \\
& \Rightarrow \frac{2 r}{\left(r^2-a^2\right)^2}=\frac{1}{\left(r^2+a^2\right)^{\frac{3}{2}}} \\
& \frac{4 r^2}{\left(r^2-a^2\right)^4}=\frac{1}{\left(r^2+a^2\right)^3} \\
& \Rightarrow 4 r^2\left(r^2+a^2\right)^3=\left(r^2-a^2\right)^4 \\
& 4 r^8\left(1+\frac{a^2}{r^2}\right)^3=r^8\left(1-\frac{a^2}{r^2}\right)^4 \\
& 4\left(1+\frac{a^2}{r^2}\right)^3=\left(1-\frac{a^2}{r^2}\right)^4
\end{aligned}
\)
\(
\text { But by solving from mathematical software we are getting } \mathrm{a} / \mathrm{r} \approx 3 \text {. }
\)
The electric flux is \(\phi=\alpha \sigma+\beta \lambda\) where \(\lambda\) and \(\sigma\) are linear and surface charge density, respectively. \(\left(\frac{\alpha}{\beta}\right)\) represents [JEE Main 2025]
(a) We are given that the electric flux is:
\(
\varphi=\alpha \sigma+\beta \lambda
\)
Here, \(\alpha\) and \(\beta\) are constants, \(\sigma\) is the surface charge density, and \(\lambda\) is the linear charge density. Now, let’s take the dimensions of both sides of the equation. For electric flux \(\varphi\), the dimension is:
\(
\begin{gathered}
{[\varphi]=[\alpha \sigma]=[\beta \lambda]} \\
{[\alpha]=\left[\frac{\varphi}{\sigma}\right]=\left[\frac{[Q / L]}{[Q / \text { Area }]}\right]=\left[\frac{\text { Area }}{\text { Length }}\right]}
\end{gathered}
\)
So, the dimensions of \(\alpha\) are \(\left[\frac{L^2}{L}\right]=L\). For \(\beta\), we get:
\(
[\beta]=\left[\frac{\varphi}{\lambda}\right]=\left[\frac{[Q / L]}{[Q / \text { Area }]}\right]=[L]
\)
Thus, the quantity \(\frac{\alpha}{\beta}\) represents a length, which corresponds to a displacement. Therefore, the correct answer is (a) displacement.
For a short dipole placed at origin O , the dipole moment P is along \(x\)-axis, as shown in the figure. If the electric potential and electric field at \(A\) are \(V_0\) and \(E_0\), respectively, then the correct combination of the electric potential and electric field, respectively, at point B on the \(y\)-axis is given by [JEE Main 2025]
(c) Electric Potential at B:
For a short dipole, the electric potential at points on the equatorial plane (like point B) is zero.
Electric Field at B:
The electric field due to a dipole at a point on the x -axis (like point A ) is given by \(E=(2 \mathrm{kp}) / \mathrm{r}^3\), where k is Coulomb’s constant, p is the dipole moment, and r is the distance.
Similarly, the electric field at a point on the \(y\)-axis (like point \(B\) ) is given by \(E=\) \((k p) / r^3\).
Since the distance from the dipole to point B is 4 times the distance from the dipole to point \(A(r B=4 r A)\), the electric field at \(B\) is \(1 / 16\) th of the electric field at \(A\) ( \(E_B=(1 / 16) E_0\) ).
Conclusion: Therefore, the electric potential at point B is 0 , and the electric field at point \(B\) is \(\mathrm{E}_0 / 16\).
A line charge of length \(\frac{\mathrm{a}^{\prime}}{2}\) is kept at the center of an edge \(B C\) of a cube ABCDEFGH having edge length ‘ \(a\) ‘ as shown in the figure. If the density of line charge is \(\lambda \mathbf{C}\) per unit length, then the total electric flux through all the faces of the cube will be ______. (Take, \(\epsilon_0\) as the free space permittivity) [JEE Main 2025]
(b) We can solve this using Gauss’s law, which states that the total electric flux \(\Phi\) through a closed surface is proportional to the total charge enclosed within the surface.
Mathematically:
\(
\Phi=\frac{Q_{\text {enclosed }}}{\epsilon_0}
\)
Step 1: Determine the enclosed charge \(Q_{\text {enclosed }}\)
Assume three imaginary cubes (total four cubes) surrounding the edge BC. The given line charge has a linear charge density \(\lambda\) (charge per unit length) and length \(\frac{a}{2}\). Therefore, the total charge \(Q_{\text {enclosed }}\) on the line is:
\(
Q_{\text {enclosed }}=\lambda \cdot \frac{a}{2}
\)
Step 2: Apply Gauss’s law
The total electric flux through all the four cubes is:
\(
\begin{gathered}
\Phi=\frac{Q_{\text {enclosed }}}{\epsilon_0} \\
\Phi=\frac{\lambda \cdot \frac{a}{2}}{\epsilon_0} \\
\Phi=\frac{\lambda a}{2 \epsilon_0}
\end{gathered}
\)
Final Answer: The total electric flux through one cube is:
\(
\Phi_{\text {single cube }}=\frac{\Phi}{4}=\frac{\frac{\lambda a}{2 \epsilon_0}}{4}=\frac{\lambda a}{8 \epsilon_0}
\)
An electric dipole of dipole moment \(6 \times 10^{-6} \mathrm{Cm}\) is placed in uniform electric field of magnitude \(10^6 \mathrm{~V} / \mathrm{m}\). Initially, the dipole moment is parallel to electric field. The work that needs to be done on the dipole to make its dipole moment opposite to the field, will be _________ J. [JEE Main 2025]
(a) Potential energy of a dipole in an electric field: \(U=-p E \cos \theta\)
Work done is equal to the change in potential energy: \(W=\Delta U=U_2-U_1\)
\(
\begin{aligned}
& U_1=-p E \cos \theta_1 \\
& U_1=-\left(6 \times 10^{-6} \mathrm{Cm}\right)\left(10^6 \mathrm{~V} / \mathrm{m}\right) \cos \left(0^{\circ}\right) \\
& U_1=-\left(6 \times 10^{-6}\right)\left(10^6\right)(1) \\
& U_1=-6 \mathrm{~J}
\end{aligned}
\)
\(
\begin{aligned}
& U_2=-p E \cos \theta_2 \\
& U_2=-\left(6 \times 10^{-6} \mathrm{Cm}\right)\left(10^6 \mathrm{~V} / \mathrm{m}\right) \cos \left(180^{\circ}\right) \\
& U_2=-\left(6 \times 10^{-6}\right)\left(10^6\right)(-1) \\
& U_2=6 \mathrm{~J}
\end{aligned}
\)
\(
\begin{aligned}
& W=\Delta U=U_2-U_1 \\
& W=6 \mathrm{~J}-(-6 \mathrm{~J}) \\
& W=12 \mathrm{~J}
\end{aligned}
\)
A square loop of sides \(a=1 \mathrm{~m}\) is held normally in front of a point charge \(\mathrm{q}=1 \mathrm{C}\) at a distance \(\frac{a}{2}\). The flux of the electric field through the shaded region is \(\frac{5}{p} \times \frac{1}{\varepsilon_0} \frac{\mathrm{Nm}^2}{\mathrm{C}}\), where the value of \(p\) is ________ . [JEE Main 2025]
(c)
Total flux through square \(=\frac{\mathrm{q}}{\epsilon_0}\left(\frac{1}{6}\right)\)
Lets divide square is 8 equal parts.
Flux is same for each part.
\(\therefore\) Flux through shaded portion is \(\frac{8}{5}\) (Total flux)
\(
=\frac{5}{8} \times \frac{q}{\epsilon_0} \frac{1}{6}=\frac{5}{48} \frac{1}{\epsilon_0}
\)
\(\therefore\) answer is 48
A positive ion \(A\) and a negative ion \(B\) has charges \(6.67 \times 10^{-19} \mathrm{C}\) and \(9.6 \times 10^{-10} \mathrm{C}\), and masses \(19.2 \times 10^{-27} \mathrm{~kg}\) and \(9 \times 10^{-27} \mathrm{~kg}\) respectively. At an instant, the ions are separated by a certain distance \(r\). At that instant the ratio of the magnitudes of electrostatic force to gravitational force is \(\mathrm{P} \times 10^{-13}\), where the value of P is ________ [JEE Main 2025]
(Take \(\frac{1}{4 \pi \varepsilon_0}=9 \times 10^9 \mathrm{Nm}^2 \mathrm{C}^{-1}\) and universal gravitational constant as \(6.67 \times 10^{-11} \mathrm{Nm}^2 \mathrm{~kg}^{-2}\) )
(b) To find the ratio of the magnitudes of electrostatic force to gravitational force between ions \(A\) and \(B\), we use the following formulas for electrostatic force \(\left(F_e\right)\) and gravitational force \(\left(F_g\right)\) :
\(
\begin{aligned}
& F_e=\frac{k \cdot q_1 \cdot q_2}{r^2} \\
& F_g=\frac{G \cdot m_1 \cdot m_2}{r^2}
\end{aligned}
\)
To find the ratio \(\frac{F_e}{F_g}\), simplify as follows:
\(
\frac{F_e}{F_g}=\frac{k \cdot q_1 \cdot q_2}{G \cdot m_1 \cdot m_2}
\)
\(
\frac{F_e}{F_g}=\frac{9 \times 10^9 \times 6.67 \times 10^{-19} \times 9.6 \times 10^{-10}}{6.67 \times 10^{-11} \times 19.2 \times 10^{-27} \times 9 \times 10^{-27}}
\)
\(
=\frac{10^{-20}}{2 \times 10^{-65}}=5 \times 10^{44}
\)
This calculation gives the ratio of the electrostatic force to the gravitational force without considering their separation distance \(r\), as it cancels out. The value of \(P[latex] mentioned in the prompt can be deduced from the simplified final expression. [latex]\text { Thus, } P=10 \text {. }\)
Five charges \(+q,+5 q,-2 q,+3 q\) and \(-4 q\) are situated as shown in the figure. The electric flux due to this configuration through the surface \(S\) is : [JEE Main 2024]
(d) According to Gauss’s law, the electric flux \(\Phi\) through a closed surface is given by:
\(
\Phi=\frac{q_{\text {in }}}{\epsilon_0}
\)
where \(q_{\text {in }}\) is the total charge enclosed by the surface.
In this problem, the charges enclosed by the surface are \(q_{i n}=q+(-2 q)+5 q=4 q\). Thus, the electric flux is:
\(
\Phi=\frac{4 q}{\epsilon_0}
\)
Two charged conducting spheres of radii \(a\) and \(b\) are connected to each other by a conducting wire. The ratio of charges of the two spheres respectively is: [JEE Main 2024]
(b) Let a be the radius of a sphere \(\mathrm{A}, Q_A\) be the charge on the sphere, and \(C_A\) be the capacitance of the sphere. Let b be the radius of a sphere \(\mathrm{B}, Q_B\) be the charge on the sphere, and \(C_B\) be the capacitance of the sphere. Since the two spheres are connected with a wire, their potential \((V)\) will become equal.
Let \(E_A\) be the electric field of sphere A and \(E_B\) be the electric field of sphere B. Therefore, their ratio,
\(
\begin{aligned}
& \frac{E_A}{E_B}=\frac{Q_A}{4 \pi \epsilon_0 \times a_2} \times \frac{b^2 \times 4 \pi \epsilon_0}{Q_B} \\
& \frac{E_A}{E_B}=\frac{Q_A}{Q_B} \times \frac{b^2}{a^2} \ldots \text { (1) }
\end{aligned}
\)
However, \(\frac{Q_A}{Q_B}=\frac{C_A V}{C_B V}\)
And, \(\frac{C_A}{C_B}=\frac{a}{b}\)
\(
\therefore \frac{Q_A}{Q_B}=\frac{a}{b} \ldots(2)
\)
Putting the value of (2) in (1), we obtain
\(
\therefore \frac{E_A}{E_B}-\frac{a}{B} \frac{b^2}{a^2}=\frac{b}{a}
\)
Therefore, the ratio of electric fields at the surface is \(\frac{b}{a}\).
Two identical conducting spheres P and S with charge Q on each, repel each other with a force 16 N. A third identical uncharged conducting sphere R is successively brought in contact with the two spheres. The new force of repulsion between P and S is : [JEE Main 2024]
(b) Step 1: Initially, the force of repulsion between P and S is 16 N .
Step 2: Sphere R is brought into contact with P , and the charge is shared equally. Charge on P and R after contact: \(\frac{Q}{2}\).
Step 3: Sphere R with charge \(\frac{Q}{2}\) is brought into contact with S . Charge on S and R after contact: \(\frac{3 Q}{4}\).
Step 4: After contact, the charges on P and S are \(\frac{Q}{2}\) and \(\frac{3 Q}{4}\) respectively.
Step 5: Calculate the new force of repulsion using Coulomb’s law: \(F^{\prime}=k \frac{\left(\frac{q}{2}\right)\left(\frac{3 q}{2}\right)}{r^2}=\frac{3}{8} F=6 \mathrm{~N}\).
\(\sigma\) is the uniform surface charge density of a thin spherical shell of radius R . The electric field at any point on the surface of the spherical shell is : [JEE Main 2024]
(b) Gauss’s law: \(\oint \vec{E} \cdot d \vec{A}=\frac{Q_{e n c}}{\epsilon_0}\)
Surface area of a sphere: \(A=4 \pi R^2\)
Consider a spherical Gaussian surface of radius \(r(r \approx R)\) just outside the charged shell.
The electric field \(\vec{E}\) is radial and constant in magnitude over the Gaussian surface.
The enclosed charge is \(Q_{\text {enc }}=\sigma A=\sigma\left(4 \pi R^2\right)\).
Applying Gauss’s law:
\(\oint \vec{E} \cdot d \vec{A}=E \oint d A=E\left(4 \pi R^2\right)=\frac{Q_{\text {enc }}}{\epsilon_0}\)
\(E\left(4 \pi R^2\right)=\frac{\sigma\left(4 \pi R^2\right)}{\epsilon_0}\)
Divide both sides by \(4 \pi R^2\) :
\(E=\frac{\sigma}{\epsilon_0}\)
The electric field at any point on the surface of the spherical shell is \(\frac{\sigma}{\epsilon_0}\).
The vehicles carrying inflammable fluids usually have metallic chains touching the ground: [JEE Main 2024]
(d) Option 1: Control the speed of the vehicle. This option is incorrect. Metallic ropes touching the ground during motion do not control the speed of the vehicle.
Option 2: Conduct the charge produced by friction. This is the correct answer. When vehicles carrying inflammable materials move, friction between the vehicle and the ground can generate static electricity. This static electricity can potentially ignite the inflammable materials, leading to a fire or explosion. By having metallic ropes touching the ground, the charge produced by friction is conducted away, preventing a buildup of static electricity and reducing the risk of ignition.
Option 3: Conduct the current produced by inflammable material. This option is incorrect. Inflammable materials do not typically produce current. The main concern is the generation of static electricity.
Option 4: Provide earthing for lightning. This option is incorrect. Metallic ropes touching the ground during motion do not provide earthing for lightning. Lightning protection systems use different mechanisms to safely direct lightning strikes to the ground.
In conclusion, option 2 is the correct answer as metallic ropes touching the ground during motion help conduct the charge produced by friction, reducing the risk of ignition for vehicles carrying inflammable materials.
In hydrogen-like system the ratio of coulombian force and gravitational force between an electron and a proton is in the order of : [JEE Main 2024]
(b)
\(
\begin{gathered}
\mathrm{F}_{\mathrm{e}}=\frac{\mathrm{KQ}_1 Q_2}{\mathrm{r}_2} \& \mathrm{~F}_{\mathrm{g}}=\frac{\mathrm{GM}_1 \mathrm{M}_2}{\mathrm{r}_2} \\
\frac{\mathrm{~F}_{\mathrm{e}}}{\mathrm{~F}_{\mathrm{g}}}=\frac{9 \times 10^9 \times 1.6 \times 10^{-19^2}}{6.67 \times 10^{-11} 9.1 \times 10^{-31} 1.67 \times 15^{-27}}=2.27 \times 10^{39}
\end{gathered}
\)
A charge \(q\) is placed at the center of one of the surface of a cube. The flux linked with the cube is: [JEE Main 2024]
(a) Gauss’s law states that the total electric flux through a closed surface is directly proportional to the enclosed electric charge: \(\Phi=\frac{q_{\text {enclosed }}}{\epsilon_0}\).
To apply Gauss’s law effectively, imagine a closed surface enclosing the charge.
Imagine another identical cube placed adjacent to the first cube, with the charge \(q\) at their common face.
This creates a closed Gaussian surface (a cube of double the volume) enclosing the charge \(q\).
The total flux through the entire doubled cube is given by Gauss’s law:
\(
\Phi_{\text {total }}=\frac{q}{e_0}
\)
Since the original cube is half of the doubled cube, the flux through it is half of the total flux:
\(
\begin{aligned}
\Phi_{\text {cube }} & =\frac{1}{2} \Phi_{\text {total }} \\
\Phi_{\text {cube }} & =\frac{1}{2} \frac{q}{\varepsilon_0} \\
\Phi_{\text {cube }} & =\frac{q}{2 \varepsilon_0}
\end{aligned}
\)
The electric flux linked with the cube is \(\frac{q}{2 \epsilon_0}\).
An infinitely long positively charged straight thread has a linear charge density \(\lambda \mathrm{Cm}^{-1}\). An electron revolves along a circular path having axis along the length of the wire. The graph that correctly represents the variation of the kinetic energy of electron as a function of radius of circular path from the wire is : [JEE Main 2024]
(c) Electric field E at a distance r due to infinite long wire is \(E=\frac{2 k \lambda}{r}\)
Force of electron \(\Rightarrow F=e E\)
\(
\begin{aligned}
& \mathrm{F}=\mathrm{e}\left(\frac{2 \mathrm{k} \lambda}{\mathrm{r}}\right) \\
& \mathrm{F}=\frac{2 \mathrm{k} \lambda \mathrm{e}}{\mathrm{r}}
\end{aligned}
\)
This force will provide required centripetal force
\(
\begin{aligned}
& \mathrm{F}=\frac{\mathrm{mv}^2}{\mathrm{r}}=\frac{2 \mathrm{k} \lambda \mathrm{e}}{\mathrm{r}} \\
& \mathrm{v}=\sqrt{\frac{2 \mathrm{k} \lambda \mathrm{e}}{\mathrm{~m}}} \\
& \mathrm{KE}=\frac{1}{2} \mathrm{mv}^2=\frac{1}{2} \mathrm{~m}\left(\frac{2 \mathrm{k} \lambda \mathrm{e}}{\mathrm{~m}}\right) \\
& =\mathrm{k} \lambda \mathrm{e}
\end{aligned}
\)
\(C_1[latex] and [latex]C_2\) are two hollow concentric cubes enclosing charges \(2 Q\) and \(3 Q\) respectively as shown in figure. The ratio of electric flux passing through \(C_1\) and \(C_2\) is : [JEE Main 2024]
(c) The electric flux \((\Phi)\) through a closed surface, according to Gauss’s law, is proportional to the enclosed charge \(Q\), and is given by \(\Phi=\frac{Q}{\epsilon_0}\), where \(\epsilon_0\) is the vacuum permittivity. This is regardless of the shape of the surface, as long as it is closed and it encloses the charge fully.
In this case, both cubes \(C_1\) and \(C_2\) are closed surfaces, and they are concentric, meaning they share the same center. Each cube encloses a different charge, \(2 Q\) for \(C_1\) and \(3 Q+\) \(2 Q=5 Q\) for \(C_2\). According to Gauss’s law, the electric flux through each cube is directly proportional to the enclosed charge.
For \(C_1\), enclosing charge \(2 Q: \Phi_{C_1}=\frac{2 Q}{\epsilon_0}\)
For \(C_2\), enclosing charge \(5 Q: \Phi_{C_2}=\frac{5 Q}{\epsilon_0}\)
Now, we want the ratio of electric flux through \(C_1\) to that through \(C_2\) :
\(
\frac{\Phi_{C_1}}{\Phi_{C_2}}=\frac{\frac{2 Q}{\epsilon_0}}{\frac{5 Q}{\epsilon_0}}=\frac{2 Q}{5 Q}=\frac{2}{5}
\)
Therefore, the ratio of electric flux passing through \(C_1\) to that passing through \(C_2\) is \(\frac{2}{5}\), which corresponds to option C.
Force between two point charges \(q_1\) and \(q_2\) placed in vacuum at ‘ \(r\) ‘ cm apart is \(F\). Force between them when placed in a medium having dielectric constant \(K=5\) at ‘ \(r / 5^{\prime} \mathrm{cm}\) apart will be: [JEE Main 2024]
(a) To find the force between two point charges in a medium with dielectric constant \(K\), we use Coulomb’s Law modified for the medium. The force in a medium is given by:
\(
F_m=\frac{F}{K}
\)
where \(F\) is the force in vacuum. Additionally, if the distance between the charges changes, the force is inversely proportional to the square of the distance. Therefore, the new force can be calculated as:
\(
F^{\prime}=\frac{F_m}{\left(\frac{r}{r^{\prime}}\right)^2}
\)
where \(r^{\prime}\) is the new distance.
Step 1: The initial force between the charges in vacuum is given by Coulomb’s Law:
\(
F=\frac{k q_1 q_2}{r^2}
\)
Step 2: When placed in a medium with dielectric constant \(K=5\), the force is reduced by a factor of \(K\) :
\(
F_m=\frac{F}{K}=\frac{F}{5}
\)
Step 3: The new distance between the charges is \(\frac{r}{5}\). The force is inversely proportional to the square of the distance:
\(
F^{\prime}=F_m\left(\frac{r}{r^{\prime}}\right)^2=\frac{F}{5}\left(\frac{r}{\frac{r}{5}}\right)^2=\frac{F}{5} \cdot 25=5 F
\)
Step 4: Thus, the force between the charges in the medium at the new distance is:
\(
F^{\prime}=5 F
\)
Two charges \(q\) and \(3 q\) are separated by a distance ‘ \(r\) ‘ in air. At a distance \(x\) from charge \(q\), the resultant electric field is zero. The value of \(x\) is : [JEE Main 2024]
(c)
The electric field due to charge \(q\) at distance \(x\) is \(E_1=k \frac{|q|}{x^2}\).
The electric field due to charge \(3 q\) at distance \(r-x\) is \(E_2=k \frac{|3 q|}{(r-x)^2}\).
For the resultant electric field to be zero, the magnitudes of \(E_1\) and \(E_2\) must be equal:
\(E_1=E_2\)
\(k \frac{|q|}{x^2}=k \frac{|3 q|}{(r-x)^2}\)
Cancel out \(k\) and \(|q|\) from both sides:
\(\frac{1}{x^2}=\frac{3}{(r-x)^2}\)
Take the square root of both sides:
\(\frac{1}{x}=\frac{\sqrt{3}}{r-x}\)
Solve for \(x\) :
\(r-x=\sqrt{3} x\)
\(r=x+\sqrt{3} x\)
\(r=x(1+\sqrt{3})\)
\(x=\frac{r}{1+\sqrt{3}}\)
The distance \(x\) from charge \(q\) where the resultant electric field is zero is \(\frac{r}{1+\sqrt{3}}\).
A particle of charge ‘ \(-q\) ‘ and mass ‘ \(m\) ‘ moves in a circle of radius ‘ \(r\) ‘ around an infinitely long line charge of linear charge density ‘ \(+\boldsymbol{\lambda}\) ‘. Then time period will be given as : [JEE Main 2024]
(Consider \(k\) as Coulomb’s constant)
(d) Electric field due to an infinitely long line charge: \(E=\frac{2 k \lambda}{r}\)
Centripetal force: \(F_c=\frac{m v^2}{r}\)
Relationship between velocity and time period: \(v=\frac{2 \pi r}{T}\)
The electric field due to the line charge is \(E=\frac{2 k \lambda}{r}\).
The electrostatic force on the particle is \(F_e=q E=\frac{2 k \lambda q}{r}\).
The centripetal force is \(F_c=\frac{m v^2}{r}\).
Equating the forces: \(\frac{2 k \lambda q}{r}=\frac{m v^2}{r}\).
\(
\begin{aligned}
& v^2=\frac{2 k \lambda q}{m} \\
& v=\sqrt{\frac{2 k \lambda q}{m}}
\end{aligned}
\)
The relationship between velocity and time period is \(v=\frac{2 \pi r}{T}\).
Substituting the value of \(v: \sqrt{\frac{2 k \lambda q}{m}}=\frac{2 \pi r}{T}\).
Solving for \(T: T=\frac{2 \pi r}{\sqrt{\frac{2 k \lambda q}{m}}}=2 \pi r \sqrt{\frac{m}{2 k \lambda q}}\).
The electrostatic potential due to an electric dipole at a distance ‘ \(r\) ‘ varies as : [JEE Main 2024]
(c) The electric potential \(\boldsymbol{v}\) due to a dipole at a distance \(r\) is given by:
\(V=\frac{1}{4 \pi \epsilon_0} \frac{p \cos \theta}{r^2}\)
where \(p\) is the dipole moment, \(\theta\) is the angle between the dipole moment and the position vector, and \(\epsilon_0\) is the permittivity of free space.
From the formula, it’s clear that the potential \(V\) is proportional to \(\frac{1}{r^2}\).
\(V \propto \frac{1}{r^2}\)
An electric field is given by \((6 \hat{i}+5 \hat{j}+3 \hat{k}) \mathrm{N} / \mathrm{C}\). The electric flux through a surface area \(30 \hat{i} \mathrm{~m}^2\) lying in YZ-plane (in SI unit) is : [JEE Main 2024]
(c)
\(
\begin{aligned}
& \overrightarrow{\mathrm{E}}=6 \hat{\mathrm{i}}+5 \hat{\mathrm{j}}+3 \hat{\mathrm{k}} \\
& \overrightarrow{\mathrm{~A}}=30 \hat{\mathrm{i}} \\
& \phi=\overrightarrow{\mathrm{E}} \cdot \overrightarrow{\mathrm{~A}} \\
& \phi=(6 \hat{\mathrm{i}}+5 \hat{\mathrm{j}}+3 \hat{\mathrm{k}}) \cdot(30 \hat{\mathrm{i}}) \\
& \phi=6 \times 30=180
\end{aligned}
\)
Two charges of \(5 Q\) and \(-2 Q\) are situated at the points \((3 a, 0)\) and \((-5 a, 0)\) respectively. The electric flux through a sphere of radius ‘ \(4 a\) ‘ having center at origin is : [JEE Main 2024]
(d) Determine which charges are inside the sphere.
The sphere radius is \(4 a\).
The charge \(5 Q\) is at \((3 a, 0)\), which is inside the sphere since \(3 a<4 a\).
The charge \(-2 Q\) is at \((-5 a, 0)\), which is outside the sphere since \(5 a>4 a\).
Calculate the total charge enclosed by the sphere.
\(Q_{\text {enclosed }}=5 Q\)
Use Gauss’s law to find the electric flux.
\(\phi=\frac{Q_{\text {enclosed }}}{\epsilon_0}\)
\(\phi=\frac{5 Q}{\epsilon_0}\)
The electric flux through the sphere is \(\frac{5 Q}{\epsilon_0}\).
Given below are two statements : one is labelled as Assertion (A) and the other is labelled as Reason (R).
Assertion (A) : Work done by electric field on moving a positive charge on an equipotential surface is always zero.
Reason (R) : Electric lines of forces are always perpendicular to equipotential surfaces.
In the light of the above statements, choose the most appropriate answer from the options given below : [JEE Main 2024]
(a) The work done by an electric field when moving a charge on an equipotential surface is zero because there is no change in electric potential energy. Electric lines of force are always perpendicular to equipotential surfaces, meaning that any movement along the surface does not alter the electric potential, confirming that no work is done.
\(
W=q \Delta V \cos \theta
\)
Because \(\Delta V=0\) on an equipotential surface, irrespective of the value of \(\cos \theta\), the work \(W\) will be zero. Hence, the Assertion \((\mathrm{A})\) is correct.
An electric charge \(10^{-6} \mu \mathrm{C}\) is placed at origin \((0,0) \mathrm{m}\) of \(\mathrm{X}-\mathrm{Y}\) co-ordinate system. Two points P and Q are situated at \((\sqrt{3}, \sqrt{3}) \mathrm{m}\) and \((\sqrt{6}, 0) \mathrm{m}\) respectively. The potential difference between the points \(\mathbf{P}\) and Q will be : [JEE Main 2024]
(a)
\(
\begin{aligned}
& \text { Potential difference }=\frac{K Q}{r_1}-\frac{K Q}{r_2} \\
& r_1=\sqrt{(\sqrt{3})^2+(\sqrt{3})^2} \\
& r_2=\sqrt{(\sqrt{6})^2+0}
\end{aligned}
\)
As \(r_1=r_2=\sqrt{6} \mathrm{~m}\)
So potential difference \(=0\)
An electric field \(\vec{E}=(2 x \hat{i}) N C^{-1}\) exists in space. A cube of side 2 m is placed in the space as per figure given below. The electric flux through the cube is ______ \(\mathrm{Nm}^2 / \mathrm{C}\). [JEE Main 2024]
(c) The electric flux is given by Gauss’s Law:
\(
\Phi=\oint \vec{E} \cdot d \vec{A}
\)
The field \(\vec{E}=2 x \hat{i}\) varies with \(x\).
For the cube, only the left ( \(x=0\) ) and right ( \(x=2\) ) faces contribute: \(\Phi=E_{\text {right }} A-E_{\text {left }} A\).
Substituting \(A=4 \mathrm{~m}^2, E_{\text {right }}=2(2)=4\), and \(E_{\text {left }}=2(0)=0\) :
\(
\Phi=4 \cdot 4-0 \cdot 4=16 \mathrm{Nm}^2 / \mathrm{C}
\)
At the centre of a half ring of radius \(R=10 \mathrm{~cm}\) and linear charge density \(4 \mathrm{nC} \mathrm{m}^{-1}\), the potential is \(x \pi \mathrm{~V}\). The value of \(x\) is _____. [JEE Main 2024]
(d) The length of the half-ring is half the circumference of a full circle: \(l=\pi R\).
The total charge \(Q\) is the product of the linear charge density \(\lambda\) and the length \(l\) :
\(Q=\lambda l\)
\(Q=\lambda \pi R\)
\(Q=\left(4 \times 10^{-9} \mathrm{C} / \mathrm{m}\right) \times \pi \times(0.1 \mathrm{~m})\)
\(Q=4 \pi \times 10^{-10} \mathrm{C}\)
The electric potential \(\boldsymbol{V}\) at the center of the half-ring is given by:
\(V=\frac{k Q}{R}\)
\(V=\frac{\left(9 \times 10^9 \mathrm{~N} \mathrm{~m}^2 / \mathrm{C}^2\right)\left(4 \pi \times 10^{-10} \mathrm{C}\right)}{0.1 \mathrm{~m}}\)
\(V=\frac{36 \pi \mathrm{~V} \mathrm{~m}}{0.1 \mathrm{~m}}\)
\(V=360 \pi \times 10^{-1} \mathrm{~V}\)
\(V=36 \pi \mathrm{~V}\)
We are given that \(V=x \pi \mathrm{~V}\).
Comparing this with our calculated value \(V=36 \pi \mathrm{~V}\), we get:
\(x \pi=36 \pi\)
\(x=36\)
The value of \(x\) is 36 .
If the net electric field at point \(P\) along \(Y\) axis is zero, then the ratio of \(\left|\frac{q_2}{q_3}\right|\) is \(\frac{8}{5 \sqrt{x}}\), where \(x=\) ____ [JEE Main 2024]
(a)
\(
\begin{aligned}
& E_2 \cos \theta=E_3 \cos \phi \\
& \frac{q_2}{\left(2^2+4^2\right)} \frac{4}{\sqrt{2^2+4^2}}=\frac{q_3}{4^2+3^2} \frac{4}{\sqrt{4^2+3^2}} \\
& \frac{q_2}{q_3}=\frac{20}{25} \frac{\sqrt{20}}{5}=\frac{4}{5} \times \frac{2 \sqrt{5}}{5} \\
& n=5
\end{aligned}
\)
An electric field, \(\overrightarrow{\mathrm{E}}=\frac{2 \hat{i}+6 \hat{j}+8 \hat{k}}{\sqrt{6}}\) passes through the surface of \(4 \mathrm{~m}^2\) area having unit vector \(\hat{n}=\left(\frac{2 \hat{i}+\hat{j}+\hat{k}}{\sqrt{6}}\right)\). The electric flux for that surface is _____ Vm .[JEE Main 2024]
(b) The electric flux through a surface is given by the formula:
\(
\Phi=\overrightarrow{\mathrm{E}} \cdot \overrightarrow{\mathrm{~A}}=|\overrightarrow{\mathrm{E}}||\overrightarrow{\mathrm{A}}| \cos \theta
\)
where \(\overrightarrow{\mathrm{E}}\) is the electric field, \(\overrightarrow{\mathrm{A}}\) is the area vector (with magnitude equal to the area of the surface and direction perpendicular to the surface, defined by the unit vector \(\hat{n}\) ), and \(\theta\) is the angle between \(\overrightarrow{\mathrm{E}}\) and \(\overrightarrow{\mathrm{A}}\). However, when using unit vectors to describe the directions of \(\overrightarrow{\mathrm{E}}\) and \(\hat{n}\), the dot product can be used to simplify the calculation as follows:
\(
\Phi=\overrightarrow{\mathrm{E}} \cdot(\overrightarrow{\mathrm{~A}})=(\overrightarrow{\mathrm{E}} \cdot \hat{n}) A
\)
Given that \(\overrightarrow{\mathrm{E}}=\frac{2 \hat{i}+6 \hat{j}+8 \hat{k}}{\sqrt{6}}\) and \(\hat{n}=\left(\frac{2 \hat{i}+\hat{j}+\hat{k}}{\sqrt{6}}\right)\), and the area \(A=4 \mathrm{~m}^2\), we can substitute them into our formula. Note that since \(\overrightarrow{\mathrm{A}}=A \hat{n}\), the magnitude of the area vector is the area of the surface itself. First, let’s find \(\overrightarrow{\mathrm{E}} \cdot \hat{n}\) :
\(
\overrightarrow{\mathrm{E}} \cdot \hat{n}=\left(\frac{2 \hat{i}+6 \hat{j}+8 \hat{k}}{\sqrt{6}}\right) \cdot\left(\frac{2 \hat{i}+\hat{j}+\hat{k}}{\sqrt{6}}\right)
\)
To compute the dot product, we multiply corresponding components and then add them up:
\(
\begin{aligned}
& \left(\frac{2 \hat{i}+6 \hat{j}+8 \hat{k}}{\sqrt{6}}\right) \cdot\left(\frac{2 \hat{i}+\hat{j}+\hat{k}}{\sqrt{6}}\right)=\frac{1}{6}(2 \cdot 2+6 \cdot 1+8 \cdot 1) \\
& =\frac{1}{6}(4+6+8)=\frac{18}{6}=3
\end{aligned}
\)
Then, the electric flux through the surface is:
\(
\begin{aligned}
& \Phi=(\overrightarrow{\mathrm{E}} \cdot \hat{n}) A=3 \times 4 \mathrm{~m}^2 \\
& \Phi=12 \mathrm{Vm}
\end{aligned}
\)
So, the electric flux for that surface is 12 Vm .
Three infinitely long charged thin sheets are placed as shown in the figure. The magnitude of electric field at the point \(P\) is \(\frac{x \sigma}{\epsilon_0}\). The value of \(x\) is ______ (all quantities are measured in SI units). [JEE Main 2024]
(b)
\(
\begin{aligned}
\overrightarrow{\mathrm{E}}_{\mathrm{p}} & =\left(\frac{\sigma}{2 \varepsilon_0}+\frac{2 \sigma}{2 \varepsilon_0}+\frac{\sigma}{2 \varepsilon_0}\right)(-\hat{\mathrm{i}}) \\
& =-\frac{2 \sigma}{\varepsilon_0} \hat{\mathrm{i}}
\end{aligned}
\)
The electric field at point \(\mathbf{p}\) due to an electric dipole is \(\mathbf{E}\). The electric field at point \(\mathbf{R}\) on equitorial line will be \(\frac{\mathrm{E}}{x}\). The value of \(x\) : [JEE Main 2024]
(a)
\(
\begin{aligned}
& E=\frac{2 k p}{r^3} \\
& E_R=\frac{k p}{(2 r)^3}=\frac{1}{8}\left(\frac{E}{2}\right) \\
& =\frac{E}{16} \\
& \therefore \quad x=16
\end{aligned}
\)
An infinite plane sheet of charge having uniform surface charge density \(+\sigma_{\mathrm{s}} \mathrm{C} / \mathrm{m}^2\) is placed on \(x-y\) plane. Another infinitely long line charge having uniform linear charge density \(+\lambda_e \mathrm{C} / \mathrm{m}\) is placed at \(z=4 \mathrm{~m}\) plane and parallel to \(y\)-axis. If the magnitude values \(\left|\sigma_{\mathrm{s}}\right|=2\left|\lambda_{\mathrm{e}}\right|\) then at point \((0,0,2)\), the ratio of magnitudes of electric field values due to sheet charge to that of line charge is \(\pi \sqrt{n}: 1\). The value of \(\)n\(\) is ________ . [JEE Main 2024]
(d) Electric Field Due to the Infinite Plane Sheet of Charge:
The electric field \(E_s\) due to an infinite plane sheet of charge with surface charge density \(\sigma\) is given by:
\(
E_s=\frac{\sigma}{2 \epsilon_0}
\)
Electric Field Due to the Line Charge:
The electric field \(E_\lambda\) at a perpendicular distance \(r\) from an infinitely long line charge with linear charge density \(\lambda_e\) is:
\(
E_\lambda=\frac{\lambda_e}{2 \pi \epsilon_0 r}
\)
where \(r=4-2=2 \mathrm{~m}\) (the distance from the line charge at \(z=4 \mathrm{~m}\) to the point \((0,0,2)\) ).
Substitute Values and Simplify:
Given \(|\sigma|=2\left|\lambda_e\right|\), we substitute this into the expressions for \(E_s\) and \(E_\lambda\) :
\(
\begin{aligned}
& E_s=\frac{\sigma}{2 \epsilon_0}=\frac{2 \lambda_e}{2 \epsilon_0}=\frac{\lambda_e}{\epsilon_0} \\
& E_\lambda=\frac{\lambda_e}{2 \pi \epsilon_0 \times 2}=\frac{\lambda_e}{4 \pi \epsilon_0}
\end{aligned}
\)
Calculate the Ratio of the Electric Fields:
The ratio of the magnitudes of electric fields \(\frac{E_s}{E_\lambda}\) is:
\(
\frac{E_s}{E_\lambda}=\frac{\frac{\lambda_c}{\epsilon_0}}{\frac{\lambda_c}{4 \pi \varepsilon_0}}=4 \pi
\)
Therefore,
\(
\frac{E_s}{E_\lambda}=\pi \sqrt{16}: 1
\)
Comparing with \(\pi \sqrt{n}: 1\), we find \(n=16\).
Suppose a uniformly charged wall provides a uniform electric field of \(2 \times 10^4 \mathrm{~N} / \mathrm{C}\) normally. A charged particle of mass 2 g being suspended through a silk thread of length 20 cm and remain stayed at a distance of 10 cm from the wall.
Then the charge on the particle will be \(\frac{1}{\sqrt{x}} \mu \mathrm{C}\) where \(x=\) ______ . [use \(\mathrm{g}=10 \mathrm{~m} / \mathrm{s}^2\) ] [JEE Main 2024]
(c)
\(
\begin{aligned}
&\sin \theta=\frac{10}{20}=\frac{1}{2}\\
&\theta=30^{\circ}\\
&\tan \theta=\frac{\mathrm{qE}}{\mathrm{mg}}\\
&\tan 30^{\circ}=\frac{\mathrm{q} \times 2 \times 10^4}{1 \times 10^{-3} \times 10}\\
&\frac{1}{\sqrt{3}}=q \times 10^6\\
&q=\frac{1}{\sqrt{3}} \times 10^{-6} C\\
&x=3
\end{aligned}
\)
Two identical charged spheres are suspended by strings of equal lengths. The strings make an angle \(\theta\) with each other. When suspended in water the angle remains the same. If density of the material of the sphere is \(1.5 \mathrm{~g} / \mathbf{c c}\), the dielectric constant of water will be ______. (Take density of water \(=1 \mathrm{~g} / \mathrm{cc}\) )
(a)
In air \(\tan \frac{\theta}{2}=\frac{F}{m g}=\frac{q^2}{4 \pi \varepsilon_0 r^2 m g}\)
In water \(\tan \frac{\theta}{2}=\frac{\mathrm{F}^{\prime}}{\mathrm{mg}^{\prime}}=\frac{\mathrm{q}^2}{4 \pi \varepsilon_0 \varepsilon_{\mathrm{r}} \mathrm{r}^2 \mathrm{mg}_{\text {elf }}}\)
Equate both equations
\(
\varepsilon_0 g=\varepsilon_0 \varepsilon_{\mathrm{r}} \mathrm{~g}\left[1-\frac{1}{1.5}\right]
\)
\(
\varepsilon_{\mathrm{r}}=3
\)
The distance between charges \(+q\) and \(-q\) is \(2 l\) and between \(+2 q\) and \(-2 q\) is \(4 l\). The electrostatic potential at point \(P\) at a distance \(r\) from center \(O\) is \(-\alpha\left[\frac{q l}{r^2}\right] \times 10^9 \mathrm{~V}\), where the value of \(\alpha\) is _________ (Use \(\frac{1}{4 \pi \varepsilon_0}=9 \times 10^9 \mathrm{Nm}^2 \mathrm{C}^{-2}\) )
(d)
\(
\begin{aligned}
& \mathrm{V}=\frac{\mathrm{Kp} \cdot \overrightarrow{\mathrm{r}}}{\mathrm{r}^3}=\frac{9 \times 10^9(6 \mathrm{q} \ell)}{\mathrm{r}^2} \cos \left(120^{\circ}\right) \\
& =-(27)\left(\frac{\mathrm{q} \ell}{\mathrm{r}^2}\right) \times 10^9 \mathrm{Nm}^2 \mathrm{c}^{-2} \\
& \Rightarrow \alpha=27
\end{aligned}
\)
Two identical charged spheres are suspended by strings of equal lengths. The strings make an angle of \(37^{\circ}\) with each other. When suspended in a liquid of density \(0.7 \mathrm{~g} / \mathrm{cm}^3\), the angle remains same. If density of material of the sphere is \(1.4 \mathrm{~g} / \mathrm{cm}^3\), the dielectric constant of the liquid is ______ \(\left(\tan 37^{\circ}=\frac{3}{4}\right)\) [JEE Main 2024]
The angle between the strings is \(37^{\circ}\) in both air and liquid.
Density of the liquid \(\rho_l=0.7 \frac{\mathrm{~g}}{\mathrm{~cm}^3}\).
Density of the sphere \(\rho_s=1.4 \frac{\mathrm{~g}}{\mathrm{~cm}^3}\).
\(
\tan 37^{\circ}=\frac{3}{4}
\)
The electrostatic force is reduced by a factor of the dielectric constant \(K\) in a medium.
Buoyant force \(F_b=V \rho_{l} g\), where \(V\) is the volume of the sphere.
How to solve
Equate the ratio of electrostatic force to the effective weight of the sphere in air and liquid to find the dielectric constant.
Step 1: Forces in air
The electrostatic force is \(F_e\).
The weight of the sphere is \(W=m g=V \rho_s g\).
\(
\tan \frac{\theta}{2}=\frac{F_e}{W}
\)
Step 2: The electrostatic force is \(F_e^{\prime}=\frac{F_e}{K}\).
The effective weight is \(W^{\prime}=W-F_b=V \rho_s g-V \rho_l g=V g\left(\rho_s-\rho_l\right)\).
\(
\tan \frac{\theta}{2}=\frac{F_e^{\prime}}{W^{\prime}}=\frac{F_e}{K V g\left(\rho_s-\rho_l\right)}
\)
Step 3:
\(
\begin{aligned}
& \frac{F_e}{V \rho_s g}=\frac{F_e}{K V g\left(\rho_s-\rho_l\right)} . \\
& \rho_s=K\left(\rho_s-\rho_l\right) .
\end{aligned}
\)
Step 4:
\(
\begin{aligned}
K & =\frac{\rho_s}{\rho_s-\rho_l} . \\
K & =\frac{1.4}{1.4-0.7} . \\
K & =\frac{1.4}{0.7} . \\
K & =2 .
\end{aligned}
\)
The dielectric constant of the liquid is 2.
An electron is moving under the influence of the electric field of a uniformly charged infinite plane sheet S having surface charge density \(+\sigma\). The electron at \(t=0\) is at a distance of 1 m from \(S[latex] and has a speed of [latex]1 \mathrm{~m} / \mathrm{s}\). The maximum value of \(\sigma\) if the electron strikes \(S\) at \(t=1 \mathrm{~s}\) is \(\alpha\left[\frac{m \epsilon_0}{e}\right] \frac{C}{m^2}\), the value of \(\alpha\) is _______. [JEE Main 2024]
(a) The electric field \(E\) due to an infinite plane sheet with surface charge density \(\sigma\) is:
\(E=\frac{\sigma}{2 e_0}\)
The force \(F\) on the electron due to the electric field \(E\) is:
\(F=e E\)
\(F=e \frac{\sigma}{2 \epsilon_0}\)
Using Newton’s second law \(F=m a\), the acceleration \(a\) of the electron is:
\(a=\frac{F}{m}\)
\(\quad a=-\frac{e \sigma}{2 m \epsilon_0}\) (The acceleration is negative because it’s acting in the opposite direction to the initial velocity, causing the electron to decelerate and stop at the sheet)
The kinematic equation for displacement \(S\) is:
\(
S=u t+\frac{1}{2} a t^2
\)
Substitute values:
\(
-1=1 \times 1+\frac{1}{2} \times-\frac{\sigma e}{2 \varepsilon_0 m} \times(1)^2
\)
Solve for \(\sigma\) :
\(
\begin{aligned}
& -1=1-\frac{\sigma e}{4 \varepsilon_0 m} \\
& \frac{\sigma e}{4 \varepsilon_0 m}=2
\end{aligned}
\)
Therefore, \(\sigma=8 \frac{\varepsilon_0 m}{e}\)
Determine \(\alpha\) :
Given \(\sigma=\alpha\left[\frac{m \varepsilon_0}{e}\right]\), we find \(\alpha=8\).
Two charges of \(-4 \mu \mathrm{C}\) and \(+4 \mu \mathrm{C}\) are placed at the points \(\mathrm{A}(1,0,4) \mathrm{m}\) and \(\mathrm{B}(2,-1,5) \mathrm{m}\) located in an electric field \(\overrightarrow{\mathrm{E}}=0.20 \hat{i} \mathrm{~V} / \mathrm{cm}\). The magnitude of the torque acting on the dipole is \(8 \sqrt{\alpha} \times 10^{-5} \mathrm{Nm}\), where \(\alpha=\) _____. [JEE Main 2024]
(b)
\(
\begin{aligned}
& \vec{\tau}=\vec{p} \times \vec{E} \\
& \vec{p}=q \vec{\ell} \\
& \overrightarrow{\mathrm{E}}=0.2 \frac{\mathrm{~V}}{\mathrm{~cm}}=20 \frac{\mathrm{~V}}{\mathrm{~m}} \\
& \overrightarrow{\mathrm{p}}=4 \times(\hat{\mathrm{i}}-\hat{\mathrm{j}}+\hat{\mathrm{k}}) \\
& =(4 \hat{\mathrm{i}}-4 \hat{\mathrm{j}}+4 \hat{\mathrm{k}}) \mu \mathrm{C}-\mathrm{m} \\
& \vec{\tau}=(4 \hat{\mathrm{i}}-4 \hat{\mathrm{j}}+4 \hat{\mathrm{k}}) \times(20 \hat{\mathrm{i}}) \times 10^{-6} \mathrm{Nm} \\
& =(8 \hat{\mathrm{k}}+8 \hat{\mathrm{j}}) \times 10^{-5}=8 \sqrt{2} \times 10^{-5} \\
& \alpha=2
\end{aligned}
\)
The electric potential at the surface of an atomic nucleus \((z=50)\) of radius \(9 \times 10^{-13} \mathrm{~cm}\) is _____ \(\times 10^6 \mathrm{~V}\). [JEE Main 2024]
(c) Concept:
The total charge on a nucleus is given by:
\(
q=Z \times e
\)
where \(\mathrm{q}=\) charge
\(Z=\) atomic number of the nucleus
\(e=\) charge of electron
Electrical potential is given by:
\(
\mathrm{V}=\frac{1}{4 \pi \epsilon_0} \frac{q}{r}
\)
Calculation:
Given \(\mathrm{z}=50, \mathrm{r}=9 \times 10^{-15} \mathrm{~m}\)
\(
\begin{aligned}
& q=Z \times e \\
& q=50 \times 1.6 \times 10^{-19} \\
& q=8 \times 10^{-18} C
\end{aligned}
\)
Potential at the surface of a nucleus is given as:
\(
\begin{aligned}
& \mathrm{V}=\frac{1}{4 \pi \epsilon_0} \frac{q}{r} \\
& \text { Since, } \frac{1}{4 \pi \epsilon_o}=9 \times 10^9 \\
& \mathrm{~V}=\frac{9 \times 10^9 \times 8 \times 10^{-18}}{9 \times 10^{-15}} \\
& =8 \times 10^6 \mathrm{volt}
\end{aligned}
\)
A thin metallic wire having cross sectional area of \(10^{-4} \mathrm{~m}^2\) is used to make a ring of radius 30 cm . A positive charge of \(2 \pi \mathrm{C}\) is uniformly distributed over the ring, while another positive charge of 30 pC is kept at the centre of the ring. The tension in the ring is ________ N ; provided that the ring does not get deformed (neglect the influence of gravity). (given, \(\frac{1}{4 \pi \epsilon_0}=9 \times 10^9 \mathrm{SI}\) units) [JEE Main 2024]
(c)
\(
\begin{aligned}
&\operatorname{Sin}\left(\frac{d \theta}{2}\right) \simeq \frac{d \theta}{2} \text { for very small value of } \theta\\
&2 \mathrm{~T}\left(\frac{d \theta}{2}\right)=\frac{k \lambda R d \theta}{R^2}\\
&\begin{aligned}
\lambda & =\frac{Q}{2 \pi R A} \\
T & =\frac{k Q q}{2 \pi R^2}=3 N
\end{aligned}
\end{aligned}
\)
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