Alec Aivazis edited Spacetime Geometery.tex  almost 10 years ago

Commit id: 3fbac9e071fe9282f117b25c8f124d0ca42b435b

deletions | additions      

       

\begin{equation}  \frac{\omega_1}{\omega_2} = \frac{1-2M/r_2}{1-2M/r_1}  \end{equaton}o_1 / o_2 = (1-2M/r_2)/(1-2M/r_1)