A uniform rod of length \(l\) is suspended by an end and is made to undergo small oscillations. The time period of small oscillation is \(T\). Then, the acceleration due to gravity at this place is:
1. | \(4\pi^2\dfrac{l}{T^2}\) | 2. | \(\dfrac{4\pi^2}{3}\dfrac{l}{T^2}\) |
3. | \(\dfrac{8\pi^2}{3}\dfrac{l}{T^2}\) | 4. | \(\dfrac{12\pi^2l}{T^2}\) |
1. | \({\Large\sqrt\frac23}T_0\) | 2. | \({\Large\sqrt\frac{1}{12}}T_0\) |
3. | \({\Large\sqrt\frac32}T_0\) | 4. | \(T_0\) |
1. | \(T\) | 2. | \(\pi T\) |
3. | \(\pi\sqrt2T\) | 4. | \(\dfrac{\pi}{\sqrt 2}T\) |
1. | \(2\pi\sqrt{\dfrac{L}{g}}\) | 2. | \(2\pi\sqrt{\dfrac{2L}{g}}\) |
3. | \(2\pi\sqrt{\dfrac{L}{2g}}\) | 4. | \(2\pi\sqrt{\dfrac{2L}{\sqrt3g}}\) |
A simple pendulum of time period \(T_0\) is taken in a rocket which is accelerating upwards initially and then, after some time, it moves with uniform velocity upward. The time period of the pendulum is observed within the rocket and is found to be \(2T_0\). The rocket, at that time, must be at a distance (above the earth's surface) of (radius of earth = \(R\))
1. | \(\dfrac{R}{2}\) | 2. | \(\dfrac{R}{4}\) |
3. | \(R\) | 4. | \(4R\) |
Assertion (A): | The time period of small oscillations of a simple pendulum is independent of the amplitude. |
Reason (R): | The oscillatory motion of a simple pendulum is affected by the mass of the bob and the acceleration due to gravity, and so the time period depends only on these quantities. |
1. | Both (A) and (R) are True and (R) is the correct explanation of (A). |
2. | Both (A) and (R) are True but (R) is not the correct explanation of (A). |
3. | (A) is True but (R) is False. |
4. | (A) is False but (R) is True. |
1. | remain unchanged |
2. | \(4~\text{s}\) | increase to
3. | \(1~\text{s}\) | decrease to
4. | decrease to \(0.5~\text{s}\) |
1. | \(\sqrt{\Large\frac{k}{M}}\) | 2. | \(\sqrt{\Large\frac{12k}{M}}\) |
3. | \(\sqrt{\Large\frac{3k}{M}}\) | 4. | \(\sqrt{\Large\frac{3k}{2M}}\) |