A charged particle (-q) is moving in a circular orbit around a fixed charge (+Q). The electrostatic force between the charges provides the necessary centripetal force for the circular motion.
2. Electrostatic ForceThe electrostatic force (\( F_e \)) between the charges is given by Coulomb's law:
\[ F_e = \frac{kQq}{r^2} \]where:
The centripetal force (\( F_c \)) required for the circular motion is:
\[ F_c = \frac{mv^2}{r} \]where:
Since the electrostatic force provides the centripetal force:
\[ F_e = F_c \] \[ \frac{kQq}{r^2} = \frac{mv^2}{r} \] 5. Relate Velocity to Time PeriodThe velocity (\( v \)) of the particle is related to the time period (\( T \)) and the radius (\( r \)) by:
\[ v = \frac{2\pi r}{T} \] 6. Substitute Velocity into the EquationSubstitute the expression for \( v \) into the equation from step 4:
\[ \frac{kQq}{r^2} = \frac{m\left( \frac{2\pi r}{T} \right)^2}{r} \]Simplify:
\[ \frac{kQq}{r^2} = \frac{4\pi^2mr}{T^2} \] 7. Solve for the Relation between T and rSubstitute \( k = \frac{1}{4\pi\epsilon_0} \):
\[ \frac{Qq}{4\pi\epsilon_0 r^2} = \frac{4\pi^2mr}{T^2} \]Rearrange to solve for \( r \):
\[ QqT^2 = 16\pi^3\epsilon_0mr^3 \] \[ r^3 = \frac{QqT^2}{16\pi^3\epsilon_0m} \] \[ r^3 = \frac{Qq}{16\pi^3\epsilon_0mT^2} \] Therefore, the relation between the time period \( T \) and the radius of the orbit \( r \) is: \[ r^3 = \frac{Qq}{16\pi^3\epsilon_0mT^2} \] The correct answer is (2) \( r^3 = \frac{Qq}{16\pi^3\epsilon_0mT^2} \).To solve the problem, we need to determine the relationship between the time period (T) and the radius (r) of the orbit of a particle with mass \( m \) and charge \( -q \), moving in a circular orbit around a fixed charge \( +Q \).
1. Understanding the Motion:
This situation describes the motion of a charged particle around a central charge, which is a classical example of the Bohr model of the atom. The force acting on the particle is the electrostatic force, given by Coulomb's law:
2. Relating the Time Period and Radius:
The speed \( v \) of the particle can be related to the time period \( T \) by the relation:
\[
v = \frac{2\pi r}{T}
\]
Substituting \( v \) into the force equation, we can derive the relationship between the time period \( T \) and the radius \( r \) of the orbit. After simplifying the expression, we obtain:
\[
r^3 = \frac{Qq}{16\pi^2 \epsilon_0 m} T^2
\]
3. Conclusion:
The correct relationship between the time period and the radius is:
Final Answer:
The correct option is (B) \( r^3 = \frac{Qq}{16\pi^2 \epsilon_0 m} T^2 \).