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The acceleration due to gravity at the p...

The acceleration due to gravity at the poles is `10ms^(-2)` and equitorial radius is 6400km for the earth. Then the angular velocity of rotation of the earth about its axis so that the weight of a body at the equator reduces to 75% is

A

`1/1600 "rads"^(-1)`

B

`1/800 "rads"^(-1)`

C

`1/400 "rads"^(-1)`

D

`1/200 "rads"^(-1)`

Text Solution

AI Generated Solution

The correct Answer is:
To solve the problem, we need to find the angular velocity of the Earth such that the weight of a body at the equator is reduced to 75% of its weight at the poles. Here’s how we can approach this step-by-step: ### Step 1: Understand the relationship between gravity at the poles and at the equator. The acceleration due to gravity at the poles (GP) is given as \(10 \, \text{m/s}^2\). The acceleration due to gravity at the equator (GE) can be expressed as: \[ GE = \frac{3}{4} GP \] This means: \[ GE = \frac{3}{4} \times 10 \, \text{m/s}^2 = 7.5 \, \text{m/s}^2 \] ### Step 2: Use the formula for gravitational acceleration at the equator. The gravitational acceleration at the equator can also be expressed as: \[ GE = GP - R \omega^2 \] where \(R\) is the radius of the Earth and \(\omega\) is the angular velocity. ### Step 3: Substitute the known values into the equation. We know: - \(GP = 10 \, \text{m/s}^2\) - \(GE = 7.5 \, \text{m/s}^2\) - \(R = 6400 \, \text{km} = 6400 \times 10^3 \, \text{m} = 6.4 \times 10^6 \, \text{m}\) Now substituting these values into the equation: \[ 7.5 = 10 - (6.4 \times 10^6) \omega^2 \] ### Step 4: Rearrange the equation to solve for \(\omega^2\). Rearranging gives: \[ (6.4 \times 10^6) \omega^2 = 10 - 7.5 \] \[ (6.4 \times 10^6) \omega^2 = 2.5 \] ### Step 5: Solve for \(\omega^2\). Now, divide both sides by \(6.4 \times 10^6\): \[ \omega^2 = \frac{2.5}{6.4 \times 10^6} \] ### Step 6: Calculate \(\omega\). Now we can calculate \(\omega\): \[ \omega = \sqrt{\frac{2.5}{6.4 \times 10^6}} \] Calculating this gives: \[ \omega = \sqrt{\frac{2.5}{6400000}} = \sqrt{3.90625 \times 10^{-7}} \approx 1.975 \times 10^{-4} \, \text{rad/s} \] ### Final Answer: Thus, the angular velocity of rotation of the Earth about its axis so that the weight of a body at the equator reduces to 75% is approximately: \[ \omega \approx 1.975 \times 10^{-4} \, \text{rad/s} \]
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