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The speed of earth's rotation about its ...

The speed of earth's rotation about its axis is `omega`. Its speed is increased to `x` times to make the effective acceleration due to gravity equal to zero at the equator, then `x` is around `(g= 10 ms^(-2) R = 6400 km)`

A

`1`

B

`8.5`

C

`17`

D

`34`

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The correct Answer is:
To solve the problem, we need to determine the factor \( x \) by which the speed of the Earth's rotation must be increased to make the effective acceleration due to gravity at the equator equal to zero. ### Step-by-Step Solution: 1. **Understanding Effective Gravity**: The effective acceleration due to gravity \( g_{\text{effective}} \) at the equator is given by: \[ g_{\text{effective}} = g - \omega^2 R \] where \( g \) is the gravitational acceleration (approximately \( 10 \, \text{m/s}^2 \)), \( \omega \) is the angular speed of the Earth, and \( R \) is the radius of the Earth (approximately \( 6400 \, \text{km} = 6.4 \times 10^6 \, \text{m} \)). 2. **Setting Effective Gravity to Zero**: We want to find \( x \) such that: \[ g - \omega_2^2 R = 0 \] where \( \omega_2 = x \omega \). Rearranging gives: \[ g = \omega_2^2 R \] 3. **Substituting \( \omega_2 \)**: Substitute \( \omega_2 \) into the equation: \[ g = (x \omega)^2 R \] This simplifies to: \[ g = x^2 \omega^2 R \] 4. **Finding the Original Angular Speed \( \omega \)**: The original angular speed \( \omega \) can be calculated using the period of rotation of the Earth (24 hours): \[ \omega = \frac{2\pi}{T_1} = \frac{2\pi}{24 \times 3600} \, \text{s}^{-1} \] 5. **Substituting \( \omega \)**: Now, substituting \( \omega \) back into the equation: \[ g = x^2 \left(\frac{2\pi}{24 \times 3600}\right)^2 R \] 6. **Solving for \( x^2 \)**: Rearranging gives: \[ x^2 = \frac{g}{R \left(\frac{2\pi}{24 \times 3600}\right)^2} \] 7. **Calculating \( x \)**: Plugging in the values: - \( g = 10 \, \text{m/s}^2 \) - \( R = 6.4 \times 10^6 \, \text{m} \) - \( T_1 = 24 \times 3600 \, \text{s} \) Calculate \( \omega \): \[ \omega = \frac{2\pi}{86400} \approx 7.272 \times 10^{-5} \, \text{rad/s} \] Now calculate \( \omega^2 R \): \[ \omega^2 R = (7.272 \times 10^{-5})^2 \times 6.4 \times 10^6 \approx 0.0032 \, \text{m/s}^2 \] Therefore: \[ x^2 = \frac{10}{0.0032} \approx 3125 \] Thus: \[ x \approx \sqrt{3125} \approx 56 \] ### Final Answer: The value of \( x \) is approximately \( 56 \).

To solve the problem, we need to determine the factor \( x \) by which the speed of the Earth's rotation must be increased to make the effective acceleration due to gravity at the equator equal to zero. ### Step-by-Step Solution: 1. **Understanding Effective Gravity**: The effective acceleration due to gravity \( g_{\text{effective}} \) at the equator is given by: \[ g_{\text{effective}} = g - \omega^2 R ...
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