Calculate the difference in the value of $g$ at the equator and at the poles due to the rotation of the Earth.

  • A
    $R_{e} \omega^{2}$
  • B
    $0$
  • C
    $2 R_{e} \omega^{2}$
  • D
    $\frac{1}{2} R_{e} \omega^{2}$

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