All Figures

$\begin{figure} \par\includegraphics[width=8cm]{8236fig1.ps}\par\end{figure}$ Figure 1: Search for velocity gradient at P₁ for model S-30 when $\Phi = \Phi _{\rm RL}$ . The asterisks indicate the two roots of the equation Q₁ = 0. The open circle is the prediction of the moving-RL from Paper I.
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In the text

$\begin{figure} \par\includegraphics[width=8cm]{8236fig2.ps}\end{figure}$ Figure 2: Velocity gradients satisfying the equation Q₁ = 0 at P₁as functions of $\Phi$ . The R- and S-branches are indicated. The asterisks and the open circle are for $\Phi = \Phi _{\rm RL}$ , as in Fig. 1. The star on the S-branch is the CAK solution. Points on the R-branch below the filled circle give singularity-free winds extending to $r = \infty$ .
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In the text

$\begin{figure} \par\includegraphics[width=8cm]{8236fig3.ps}\end{figure}$ Figure 3: Functions Q_i(z) for points (v_i, x_i) throughout the supersonic wind of model S-30. The asterisk is the initial gradient $z_{\rm R}$ and the corresponding Q₁(z) is labelled - see also Fig. 1. The arrows indicate the direction of increasing v along the line Q = 0 and the filled circles locate the stationary points z^s_i of the Q_i(z).
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In the text

$\begin{figure} \par\includegraphics[width=8cm]{8236fig4.ps}\end{figure}$ Figure 4: Shooting integrations to determine $(\Phi _{\rm CAK})_{1}$ , all starting at P₁. The curves are labelled with $\Phi$ in units of $10^{-6}~M_{\hbox{$\odot$ }}/{\rm yr}$ .
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In the text

$\begin{figure} \par\includegraphics[width=8cm]{8236fig1.ps}\par\end{figure}$	Figure 1: Search for velocity gradient at P₁ for model S-30 when $\Phi = \Phi _{\rm RL}$ . The asterisks indicate the two roots of the equation Q₁ = 0. The open circle is the prediction of the moving-RL from Paper I.
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$\begin{figure} \par\includegraphics[width=8cm]{8236fig2.ps}\end{figure}$	Figure 2: Velocity gradients satisfying the equation Q₁ = 0 at P₁as functions of $\Phi$ . The R- and S-branches are indicated. The asterisks and the open circle are for $\Phi = \Phi _{\rm RL}$ , as in Fig. 1. The star on the S-branch is the CAK solution. Points on the R-branch below the filled circle give singularity-free winds extending to $r = \infty$ .
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$\begin{figure} \par\includegraphics[width=8cm]{8236fig3.ps}\end{figure}$	Figure 3: Functions Q_i(z) for points (v_i, x_i) throughout the supersonic wind of model S-30. The asterisk is the initial gradient $z_{\rm R}$ and the corresponding Q₁(z) is labelled - see also Fig. 1. The arrows indicate the direction of increasing v along the line Q = 0 and the filled circles locate the stationary points z^s_i of the Q_i(z).
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$\begin{figure} \par\includegraphics[width=8cm]{8236fig4.ps}\end{figure}$	Figure 4: Shooting integrations to determine $(\Phi _{\rm CAK})_{1}$ , all starting at P₁. The curves are labelled with $\Phi$ in units of $10^{-6}~M_{\hbox{$\odot$ }}/{\rm yr}$ .
Open with DEXTER