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Question: If ‘R’ is the radius of the earth and \(\omega \) is the angular velocity with which it rotates abou...

If ‘R’ is the radius of the earth and ω\omega is the angular velocity with which it rotates about its axis, the variation in the value of ‘g’ at 45{45^ \circ } latitude of the earth stops its rotation will be
A) Increases by Rω22\dfrac{{R{\omega ^2}}}{2}
B) Decreases by Rω22\dfrac{{R{\omega ^2}}}{2}
C) Increases by Rω24\dfrac{{R{\omega ^2}}}{4}
D) Decreases by Rω24\dfrac{{R{\omega ^2}}}{4}

Explanation

Solution

The earth latitude of a point is the angle ϕ\phi between the equatorial plane and line joining that point to the center of the earth. Due to the rotational motion of the earth about its axis, the body experiences a centrifugal force.

Formula Used: We will be using the formula of the variation of acceleration due to gravity with a Latitudinal position on earth is g=gω2Rcos2ϕg' = g - {\omega ^2}R{\cos ^2}\phi .

Complete step by step solution:
At equator, the Latitude ϕ=0\phi = 0, the acceleration due to gravity is minimum. At poles ϕ=90\phi = {90^ \circ } and so the acceleration due to gravity is maximum.

A body of mass m at a point P with latitude ϕ\phi and g’ be the acceleration due to gravity at point P. The expression for acceleration due to gravity at a point P on the surface of the earth having latitude ϕ\phi is defined as the difference between the two forces is equal to the weight of that body at that point.
mg=mgmrω2cosϕmg' = mg - mr{\omega ^2}\cos \phi
Therefore, r=Rcosϕr = R\cos \phi
g=gω2Rcos2ϕg' = g - {\omega ^2}R{\cos ^2}\phi
Given: The variation in the value of ‘g’ at 45{45^ \circ } latitude of the earth stops. To find whether the rotation is increasing or decreases.
We already know the relation of the acceleration due to gravity due to earth’s rotation
g=gω2Rcos2ϕg' = g - {\omega ^2}R{\cos ^2}\phi
According the given latitude 45{45^ \circ },
ϕ=45\phi = {45^ \circ } Acceleration due to gravity at 45{45^ \circ } latitude
g=gω2Rcos245g' = g - {\omega ^2}R{\cos ^2}{45^ \circ }
g=gω2R2g' = g - \dfrac{{{\omega ^2}R}}{2}
When earth stops rotating, that is ω=0\omega = 0, then the acceleration due to gravity at 45{45^ \circ } latitude will increases by Rω22\dfrac{{R{\omega ^2}}}{2}

Option (A), Increases by Rω22\dfrac{{R{\omega ^2}}}{2} is the answer.

Note: The acceleration due to gravity is defined as the acceleration gained by an object due to gravitational force. The standard value of g on the surface of the earth is 9.8ms29.8m{s^{ - 2}}. The acceleration due to gravity is constant but it varies from place to place.