/[MITgcm]/manual/s_algorithm/text/spatial-discrete.tex
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revision 1.10 by cnh, Thu Oct 25 18:36:53 2001 UTC revision 1.11 by adcroft, Tue Nov 13 18:15:26 2001 UTC
# Line 57  recovers the same ODE's resulting from f Line 57  recovers the same ODE's resulting from f
57  interior of a fluid. Differences arise at boundaries where a boundary  interior of a fluid. Differences arise at boundaries where a boundary
58  is not positioned on a regular or smoothly varying grid. This method  is not positioned on a regular or smoothly varying grid. This method
59  is used to represent the topography using lopped cell, see  is used to represent the topography using lopped cell, see
60  \cite{Adcroft98}. Subtle difference also appear in more than one  \cite{adcroft:97}. Subtle difference also appear in more than one
61  dimension away from boundaries. This happens because the each  dimension away from boundaries. This happens because the each
62  direction is discretized independently in the finite difference method  direction is discretized independently in the finite difference method
63  while the integrating over finite volume implicitly treats all  while the integrating over finite volume implicitly treats all
64  directions simultaneously. Illustration of this is given in  directions simultaneously. Illustration of this is given in
65  \cite{Adcroft02}.  \cite{ac:02}.
66    
67  \subsection{C grid staggering of variables}  \subsection{C grid staggering of variables}
68    
# Line 79  equations. } Line 79  equations. }
79  The basic algorithm employed for stepping forward the momentum  The basic algorithm employed for stepping forward the momentum
80  equations is based on retaining non-divergence of the flow at all  equations is based on retaining non-divergence of the flow at all
81  times. This is most naturally done if the components of flow are  times. This is most naturally done if the components of flow are
82  staggered in space in the form of an Arakawa C grid \cite{Arakawa70}.  staggered in space in the form of an Arakawa C grid \cite{arakawa:77}.
83    
84  Fig. \ref{fig:cgrid3d} shows the components of flow ($u$,$v$,$w$)  Fig. \ref{fig:cgrid3d} shows the components of flow ($u$,$v$,$w$)
85  staggered in space such that the zonal component falls on the  staggered in space such that the zonal component falls on the
# Line 400  thickness of the open side is given by $ Line 400  thickness of the open side is given by $
400  \label{fig:hfacs}  \label{fig:hfacs}
401  \end{figure}  \end{figure}
402    
403  \cite{Adcroft97} presented two alternatives to the step-wise finite  \cite{adcroft:97} presented two alternatives to the step-wise finite
404  difference representation of topography. The method is known to the  difference representation of topography. The method is known to the
405  engineering community as {\em intersecting boundary method}. It  engineering community as {\em intersecting boundary method}. It
406  involves allowing the boundary to intersect a grid of cells thereby  involves allowing the boundary to intersect a grid of cells thereby
# Line 524  the atmosphere. Line 524  the atmosphere.
524  The difference in approach between ocean and atmosphere occurs because  The difference in approach between ocean and atmosphere occurs because
525  of the direct use of the ideal gas equation in forming the potential  of the direct use of the ideal gas equation in forming the potential
526  energy conversion term $\alpha \omega$. The form of these conversion  energy conversion term $\alpha \omega$. The form of these conversion
527  terms is discussed at length in \cite{Adcroft01}.  terms is discussed at length in \cite{adcroft:02}.
528    
529  Because of the different representation of hydrostatic balance between  Because of the different representation of hydrostatic balance between
530  ocean and atmosphere there is no elegant way to represent both systems  ocean and atmosphere there is no elegant way to represent both systems

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