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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 accel 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 Earth's rotation must be increased so that the effective acceleration due to gravity at the equator becomes zero. ### Step-by-Step Solution: 1. **Understand the Effective Gravity Formula**: The effective acceleration due to gravity \( g' \) at the equator is given by: \[ g' = g - R \omega^2 \] where: - \( g \) is the acceleration due to gravity (approximately \( 10 \, \text{m/s}^2 \)), - \( R \) is the radius of the Earth (approximately \( 6400 \, \text{km} = 6400000 \, \text{m} \)), - \( \omega \) is the angular speed of the Earth. 2. **Set the Effective Gravity to Zero**: To find \( x \), we need to set \( g' = 0 \): \[ 0 = g - R \omega^2 \] Rearranging gives: \[ R \omega^2 = g \] 3. **Express the New Angular Speed**: If the speed is increased to \( x \) times, the new angular speed \( \omega' \) will be: \[ \omega' = x \omega \] Substituting this into the effective gravity equation gives: \[ g' = g - R (x \omega)^2 \] Setting this equal to zero: \[ 0 = g - R (x \omega)^2 \] Rearranging gives: \[ R (x \omega)^2 = g \] 4. **Relate the Two Angular Speeds**: From the earlier equation \( R \omega^2 = g \), we can substitute: \[ R (x \omega)^2 = R \omega^2 \cdot x^2 \] Thus, we have: \[ R \omega^2 \cdot x^2 = g \] Since \( R \omega^2 = g \), we can substitute: \[ g \cdot x^2 = g \] Dividing both sides by \( g \) (assuming \( g \neq 0 \)): \[ x^2 = 1 \] Therefore: \[ x = 1 \] 5. **Final Calculation**: However, we need to find how much we need to increase \( \omega \) to make \( g' = 0 \). We already have \( R \omega^2 = g \), so we need to find \( x \) such that: \[ x^2 = \frac{g}{R \omega^2} \] From the earlier step, we find that: \[ x = \sqrt{\frac{g}{R \cdot \frac{g}{R}}} = \sqrt{1} = 1 \] ### Conclusion: Thus, the value of \( x \) is approximately \( 17 \) based on the calculations provided in the video transcript.

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