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Next: Stability of torsional flow Up: Parallel-Plate Flow Previous: Parallel-Plate Flow

Problem formulation

In what follows we use cylindrical coordinates with the dimensionless velocity given by

\begin{displaymath}
{\bf v}=(u,v,w)\end{displaymath}

(i.e. u is the radial, v the azimuthal and w the axial velocity) and the extra stress tensor

\begin{displaymath}
\mbox{\boldmath$\tau$}=\left ( \begin{array}
{ccc}
\Sigma &...
 ...
\zeta&\Delta&\Pi \\ 
\gamma&\Pi&\Gamma \end{array} \right ).
\end{displaymath}

One solution of this problem is the torsional flow given by
\begin{displaymath}
{\bf v}=(0,rz,0)
\end{displaymath} (152)
and
\begin{displaymath}
\tau =\left ( \begin{array}
{ccc}
0&0&0\\ 0&2r^{2}\beta{\rm De}&r\beta \\ 0&r\beta &0 \end{array} \right ).
\end{displaymath} (153)
Our goal is to determine the stability of this solution and to find the solutions which bifurcate from it when stability is lost. For ease of analysis we shall consider a class of similarity solutions which include the viscometric torsional solution. Introduce the following similarity variables

\begin{displaymath}
u=r\frac{d f}{d z}, \hspace{.2in} 
w=-2f(z), \hspace{.2in} v=rg(z), \end{displaymath}

\begin{displaymath}
\Sigma=r^{2}\hat{\Sigma}(z),\hspace{.2in} \zeta=r^{2}\hat{\zeta}(z),
\hspace{.2in} \gamma=r\hat{\gamma}(z), \end{displaymath}

\begin{displaymath}
\Delta=r^{2}\hat{\Delta}(z), \hspace{.2in}
\Pi=r\hat{\Pi}(z), \hspace{.2in}
\Gamma=\hat{\Gamma}(z),\end{displaymath}

Substituting in the governing equations (Appendix 1) and dropping the hats we obtain the following.  
 \begin{displaymath}
(1-\beta)\frac{\partial^{4} f}{\partial z^{4}}+
\frac{\part...
 ...l\Sigma}
{\partial z}-\frac{\partial \Delta }{\partial z}=0

\end{displaymath} (154)
\begin{displaymath}
(1-\beta)\frac{\partial^2 g}{\partial z^{2}}+\frac{\partial \Pi}
{\partial z}+4\zeta =0
\end{displaymath} (155)
\begin{displaymath}
{\rm De}
\frac{\partial \Sigma}{\partial t}+\Sigma=2{\rm De}...
 ...a}
{\partial z}+\gamma \frac{\partial^{2} f}{\partial z^{2}})
\end{displaymath} (156)
\begin{displaymath}
{\rm De}
\frac{\partial \zeta}{\partial t}+\zeta={\rm De}(2f...
 ...al g}{\partial z}+\Pi \frac{\partial^{2} f}
{\partial z^{2}})
\end{displaymath} (157)
\begin{displaymath}
{\rm De}
\frac{\partial \gamma}{\partial t}+\gamma-\beta \fr...
 ...f}{\partial z}+\Gamma \frac{\partial^{2} f}
{\partial z^{2}})
\end{displaymath} (158)
\begin{displaymath}
{\rm De}
\frac{\partial \Delta}{\partial t}+\Delta=2{\rm De}...
 ...rtial \Delta}
{\partial z}+\Pi \frac{\partial g}{\partial z})
\end{displaymath} (159)
\begin{displaymath}
{\rm De}
\frac{\partial \Pi}{\partial t}+\Pi-\beta \frac{\pa...
 ...artial f}
{\partial z}+\Gamma \frac{\partial g}{\partial z}).
\end{displaymath} (160)
 
 \begin{displaymath}
{\rm De}\frac{\partial \Gamma}{\partial t}+\Gamma+4\beta \fr...
 ...\Gamma}{\partial z}
-2\Gamma \frac{\partial f}{\partial z})

\end{displaymath} (161)
The boundary conditions become
\begin{displaymath}
f=f^{'}=g=0, \: \mbox{for} \: z=0
\end{displaymath} (162)
and
\begin{displaymath}
f=f^{'}=0, \: g=1 \: \mbox{for}\: z=1.
\end{displaymath} (163)

next up previous contents
Next: Stability of torsional flow Up: Parallel-Plate Flow Previous: Parallel-Plate Flow
Michael Renardy
1998-07-13