\begin{table}%t3
%\centering
\par
\caption{Analytical approximation and numerical results for the rotational-CAK model with $\delta=0$.
Note: the mass loss rate is given in units of  $10^{-9}~ M_{\odot} / \rm year$ and the terminal velocity is in km~s$^{-1}$. \label{tabla3} }
$$
\begin{array}{cccccccc}   %{p{0.5\linewidth}l}
\hline \hline
\noalign{\smallskip}
\Omega\; & r_{\rm min}/R_{\ast} \;& r_{\rm max}/R_{\ast} \;&r_{\rm crit}/R_{\ast} \;& \bar{C}_{\rm max} \;&  \bar{C} \;& \dot{M} \;&v_{\infty}\\%
\noalign{\smallskip}
\hline
\noalign{\smallskip}
0 \;& 1 \;& 706.50 \;& 1.559 \;& 48.248 \;& 48.223 \;& 1.814 \;& 1008.2\\
\hline
0.2\; &  5.316\; & 706.46 \;& 5.370  \;& 47.972 \;& 47.961\;& 1.831 \;& 920.1\\
0.4\; & 10.632\; & 706.34 \;& 10.669 \;& 47.648 \;& 47.634\;& 1.854 \;& 800.3\\
0.6\; & 15.948\; & 706.14 \;& 15.992 \;& 47.322 \;& 47.303\;& 1.877 \;& 683.3\\
0.8\; & 21.264\; & 705.86 \;& 21.334 \;& 46.992 \;& 46.964\;& 1.902 \;& 574.5\\
\noalign{\smallskip}
\hline
\end{array}
$$
\end{table}