MCQ
The difference in the acceleration due togravity at the pole and equator is $(g=$ acceleration due to gravity, $R=$ radius of earth, $\theta=$ latitude, $\omega=$ angular velocity, $\cos 0^{\circ}=1, \cos 90^{\circ}=0 )$
- A$\frac{R \omega^2}{g^2}$
- B$\omega \cos ^2 \theta$
- ✓$R \omega^2$
- D$R \omega^2 \cos ^2 \theta$