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There are two bodies A and B of same mas...

There are two bodies A and B of same mass. A is placed near equator of earth and B is placed at a height `h` above the pole of earth. if both the bodies weighs equally. Find `h` in terms of radius `R` of earth, angular speed `omega` of earth and `g` acceleration due to gravity close to earth.

A

`R omega^2/(2g)`

B

`R^2 omega^2/(2g)`

C

`gR/omega^2`

D

`g/omega^2`

Text Solution

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The correct Answer is:
To solve the problem, we need to find the height \( h \) above the pole where body B weighs the same as body A located at the equator. We will use the concepts of gravitational acceleration and the effects of Earth's rotation. ### Step-by-Step Solution: 1. **Understanding the Weights**: - The weight of body A at the equator can be expressed as: \[ W_A = m \cdot g_A \] - The weight of body B at height \( h \) above the pole can be expressed as: \[ W_B = m \cdot g_B \] - Since both bodies weigh equally, we have: \[ W_A = W_B \implies m \cdot g_A = m \cdot g_B \] - We can cancel the mass \( m \) from both sides: \[ g_A = g_B \] 2. **Calculating Gravitational Acceleration**: - The gravitational acceleration at the equator (body A) is affected by the centrifugal force due to Earth's rotation: \[ g_A = g - \omega^2 R \] - The gravitational acceleration at height \( h \) above the pole (body B) is: \[ g_B = g \left(1 - \frac{2h}{R}\right) \] 3. **Setting the Accelerations Equal**: - From the previous step, we equate \( g_A \) and \( g_B \): \[ g - \omega^2 R = g \left(1 - \frac{2h}{R}\right) \] 4. **Simplifying the Equation**: - Distributing \( g \) on the right side: \[ g - \omega^2 R = g - \frac{2gh}{R} \] - Now, we can cancel \( g \) from both sides: \[ -\omega^2 R = -\frac{2gh}{R} \] 5. **Rearranging to Solve for \( h \)**: - Multiplying both sides by \( -1 \): \[ \omega^2 R = \frac{2gh}{R} \] - Now, multiply both sides by \( R \): \[ \omega^2 R^2 = 2gh \] - Finally, solving for \( h \): \[ h = \frac{\omega^2 R^2}{2g} \] ### Final Result: The height \( h \) above the pole where body B weighs the same as body A at the equator is given by: \[ h = \frac{\omega^2 R^2}{2g} \]
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