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Next: Appendix 2: Linearized equations Up: Cone-and-Plate Flow Previous: Hopf bifurcation

Appendix 1: Governing equations

For axisymmetric, creeping flow the leading order equations (for $\alpha<<1$), after dropping the subscripts, are [3]:  
 \begin{displaymath}
\rho\frac{\partial u}{\partial \rho}-
\frac{\partial v}{\partial \psi}=0,

\end{displaymath} (209)
 
 \begin{displaymath}
\rho\frac{\partial p}{\partial \rho} =\rho\frac{\partial \Si...
 ...al \zeta}{\partial \psi}
 -\Delta
 +(1-\beta) \nabla^{2}u,

\end{displaymath} (210)
 
 \begin{displaymath}
-\frac{\partial p}{\partial \psi}= \rho \frac{\partial \zeta...
 ...-\frac{\partial \Gamma}{\partial \psi}+(1-\beta)\nabla^{2}v,

\end{displaymath} (211)
 
 \begin{displaymath}
0=\rho\frac{\partial \gamma}{\partial \rho} 
-\frac{\partial \Pi}{\partial \psi}+(1-\beta)\nabla^{2}w,

\end{displaymath} (212)

   \begin{eqnarray}
\Sigma+De\frac{\partial \Sigma}{\partial t}&=& -\mbox{We} 
 (u...
 ...\ 
 & & +2\beta\rho\frac{\partial u}{\partial \rho}, \nonumber

\end{eqnarray}

   \begin{eqnarray}
\zeta+De\frac{\partial \zeta}{\partial t}&=&
 -\mbox{We}(u\rho...
 ...partial \rho}-
 \frac{\partial u}{\partial \psi}), \nonumber

 \end{eqnarray}

   \begin{eqnarray}
\gamma + {\rm De}\frac{\partial \gamma}{\partial t}&=&
-\mbox{...
 ...si} )
 +\beta \rho \frac{\partial w}{\partial \rho}, \nonumber

\end{eqnarray}

 
 \begin{displaymath}
\Gamma+{\rm De}\frac{\partial \Gamma}{\partial t} =
 - \mbo...
 ...{\partial \psi})
 -2\beta\frac{\partial v}{\partial \psi}, 

\end{displaymath} (213)

   \begin{eqnarray}
\Pi+{\rm De}\frac{\partial \Pi}{\partial t}&=&
 -\mbox{We} (u\...
 ...tial \psi})
 -\beta \frac{\partial w}{\partial \psi},\nonumber

\end{eqnarray}

and  
 \begin{displaymath}
\Delta+{\rm De} \frac{\partial \Delta}{\partial t}=
 -\mbox...
 ...
 -\gamma \rho \frac{\partial w}{\partial \rho}). \nonumber 

\end{displaymath}   

In these equation the Deborah number is defined based on the rotation rate ${\rm De}=\lambda\Omega$, while the Weissenberg number is based on the shear rate ${\rm We}=\lambda\dot\gamma=\lambda\Omega/\alpha$.The no-slip boundary conditions in this case are  
 \begin{displaymath}
u=v=w=0, \; \mbox{on} \; \psi=0,

\end{displaymath} (214)
and  
 \begin{displaymath}
u=v=0, \; w=1, \; \mbox{on} \;\psi=1.

\end{displaymath} (215)
In addition, we require u, v, and w to be bounded at $\rho =0$ and as $\rho \rightarrow \infty$. The Laplacian is defined as

\begin{displaymath}
\nabla^{2} \equiv \rho^{2}\frac{\partial^{2}}{\partial \rho^...
 ...artial}{\partial \rho}+\frac{\partial^{2}}{\partial \psi^{2}}.
\end{displaymath}


next up previous contents
Next: Appendix 2: Linearized equations Up: Cone-and-Plate Flow Previous: Hopf bifurcation
Michael Renardy
1998-07-13