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Calculate the change in the value of g a...

Calculate the change in the value of `g` at latitude `45^(@)`. Take radius of earth `R = 6.37 xx 10^(3) km`.

A

`- 0.168 m//s^(2)`

B

`- 0.0168 m//s^(2)`

C

`- 0.0198 m//s^(2)`

D

`- 0.198 m//s^(2)`

Text Solution

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The correct Answer is:
To calculate the change in the value of `g` at latitude `45°`, we can use the formula that accounts for the effect of the Earth's rotation. The formula for the change in acceleration due to gravity `g'` at latitude `θ` is given by: \[ g' = g - r \omega^2 \cos^2(\theta) \] Where: - \( g \) is the acceleration due to gravity at the equator (approximately \( 9.81 \, \text{m/s}^2 \)), - \( r \) is the radius of the Earth, - \( \omega \) is the angular velocity of the Earth, - \( \theta \) is the latitude. ### Step-by-Step Solution: 1. **Convert the Radius of the Earth:** Given \( R = 6.37 \times 10^3 \, \text{km} = 6.37 \times 10^6 \, \text{m} \). 2. **Calculate the Angular Velocity (\( \omega \)):** The angular velocity of the Earth can be calculated using the formula: \[ \omega = \frac{2\pi}{T} \] where \( T \) is the time period of rotation in seconds. For one complete rotation (24 hours): \[ T = 24 \times 60 \times 60 = 86400 \, \text{s} \] Thus, \[ \omega = \frac{2\pi}{86400} \approx 7.27 \times 10^{-5} \, \text{rad/s} \] 3. **Calculate \( \cos^2(45°) \):** Since \( \cos(45°) = \frac{1}{\sqrt{2}} \), \[ \cos^2(45°) = \left(\frac{1}{\sqrt{2}}\right)^2 = \frac{1}{2} \] 4. **Substitute Values into the Formula:** Now, substituting the values into the formula for the change in `g`: \[ g' - g = - R \omega^2 \cos^2(45°) \] \[ g' - 9.81 = - (6.37 \times 10^6) \times (7.27 \times 10^{-5})^2 \times \frac{1}{2} \] 5. **Calculate \( R \omega^2 \):** First, calculate \( \omega^2 \): \[ \omega^2 = (7.27 \times 10^{-5})^2 \approx 5.29 \times 10^{-9} \, \text{(rad/s)}^2 \] Now, calculate \( R \omega^2 \): \[ R \omega^2 = (6.37 \times 10^6) \times (5.29 \times 10^{-9}) \approx 0.0337 \, \text{m/s}^2 \] 6. **Calculate the Change in `g`:** Now substitute back into the equation: \[ g' - 9.81 = -0.0337 \times \frac{1}{2} \] \[ g' - 9.81 = -0.01685 \] \[ g' = 9.81 - 0.01685 \approx 9.79315 \, \text{m/s}^2 \] 7. **Final Change in `g`:** The change in the value of `g` at latitude `45°` is: \[ \Delta g = g' - g = -0.01685 \, \text{m/s}^2 \approx -0.017 \, \text{m/s}^2 \] ### Summary: The change in the value of `g` at latitude `45°` is approximately \( -0.017 \, \text{m/s}^2 \).

To calculate the change in the value of `g` at latitude `45°`, we can use the formula that accounts for the effect of the Earth's rotation. The formula for the change in acceleration due to gravity `g'` at latitude `θ` is given by: \[ g' = g - r \omega^2 \cos^2(\theta) \] Where: - \( g \) is the acceleration due to gravity at the equator (approximately \( 9.81 \, \text{m/s}^2 \)), - \( r \) is the radius of the Earth, - \( \omega \) is the angular velocity of the Earth, ...
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