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MHT CET · Physics · Gravitation

Consider earth to be a sphere of radius \(R_e\) rotating about its own axis with angular speed \(\omega\). If \(g_{\mathrm{E}}\) and \(g_{\mathrm{P}}\) are the accelerations due to gravity at the equator and the poles respectively, then \(\left(g_{\mathrm{P}}-g_{\mathrm{E}}\right)\) is given by
\(\left[\cos \left(0^{\circ}\right)=\sin \left(\frac{\pi}{2}\right)=1, \sin \left(0^{\circ}\right)=\cos \left(\frac{\pi}{2}\right)=0\right]\)

  1. A \(\frac{R_{\mathrm{E}}}{\omega^2}\)
  2. B \(R_{\mathrm{E}} \omega^2\)
  3. C \(R_{\mathrm{E}} \omega\)
  4. D \(R_{\mathrm{E}}^2 \omega^2\)
Verified Solution

Answer & Solution

Correct Answer

(B) \(R_{\mathrm{E}} \omega^2\)

Step-by-step Solution

Detailed explanation

Acceleration due to gravity at a place of latitude \(\lambda\) due to the rotation of earth is
\(g^{\prime}=g-\mathrm{R}_{\mathrm{E}} \omega^2\left(\cos ^2 \lambda\right)\)
At equator, \(\lambda=0^{\circ}, \cos 0^{\circ}=1\)
\(\Rightarrow g_E=g-\mathrm{R}_{\mathrm{E}} \omega^2\)
At poles, \(\lambda=90^{\circ}, \cos (\lambda)=0\)
\(\begin{aligned} & \therefore g^{\prime}=g_{\mathrm{P}}=g \\ & \therefore g_{\mathrm{P}}-g_{\mathrm{E}}=g-\left(g-R_E \omega^2\right)=R_E \omega^2\end{aligned}\)