**Table 4:** Numerical results for the rotation-CAK model with $\delta =0.02$ . 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.
$\begin{table} \par \begin{displaymath} \begin{array}{ccccc} % \hline \hline \noa... ...& 564.6 \\ \noalign{\smallskip } \hline \end{array}\end{displaymath}\end{table}$

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