Index: mttroot/mtt/lib/examples/Thermal/GasTurbines/SimpleGasTurbine/SimpleGasTurbine_desc.tex
==================================================================
--- mttroot/mtt/lib/examples/Thermal/GasTurbines/SimpleGasTurbine/SimpleGasTurbine_desc.tex
+++ mttroot/mtt/lib/examples/Thermal/GasTurbines/SimpleGasTurbine/SimpleGasTurbine_desc.tex
@@ -5,10 +5,13 @@
 % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 % %% Version control history
 % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 % %% $Id$
 % %% $Log$
+% %% Revision 1.1  1998/05/18 15:45:50  peterg
+% %% Initial revision
+% %%
 % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
 
    The acausal bond graph of system \textbf{SimpleGasTurbine} is
    displayed in Figure \Ref{SimpleGasTurbine_abg} and its label
    file is listed in Section \Ref{sec:SimpleGasTurbine_lbl}.
@@ -18,17 +21,16 @@
    turbine (producing shaft power) with an ideal-gas working fluid. It
    corresponds to the simple Joule Cycle as described in Chapter 12 of
    Rogers and Mayhew and in Chapter 2 of Cohen, Rogers and
    Saravanamutto. However, unlike those examples, the system is
    written with dynamics in mind.
-
-The system is described using an energy Bond Graph- this ensures
-that the first law is observed. In particular (for I believe the first
-time) transformers are used to explicitly convert between energy
-covariables. Although this is a simple model, I believe that it
-provides the basis for building complex thermodynamic systems
-involving gas power cycles.
+   
+   The system is described using an energy Bond Graph- this ensures
+   that the first law is observed. In particular transformers are used
+   to explicitly convert between energy covariables. Although this is
+   a simple model, I believe that it provides the basis for building
+   complex thermodynamic systems involving gas power cycles.
 
 
 There are five main components:
 \begin{enumerate}
 \item p1 -- a \textbf{Pump} component representing the compressor
@@ -63,11 +65,11 @@
 (power sensor) component, that for work output is embedded in the
 \textbf{Load} component. These can be monitored to give the efficiency
 of the \textbf{SimpleGasTurbine}.
 
 A symbolic steady-state for the model was computed -- see Section
-\ref{sec:SimpleGasTurbine_sspar.tex}. In particular, the load
+\ref{sec:SimpleGasTurbine_ss.tex}. In particular, the load
 resistance was chosen to absorb all the generated work at the steady
 state and the shaft inertia was chosen to give a unit time constant
 for the linearised system. The mass flow and shaft speeds were taken
 as unity.
 
@@ -79,24 +81,24 @@
 Simulations were performed starting at the steady state and increasing
 the combustion chamber temperature by 10\% at $t=1$ and reducing by
 10\% at $t=5$. Graphs of the various outputs are plotted:
 \begin{itemize}
 \item Figure
-  \Ref{fig:SimpleGasTurbine_odeso.ps-SimpleGasTurbine-p1-T,SimpleGasTurbine-c1-T,SimpleGasTurbine-t1-T}
+  \Ref{fig:SimpleGasTurbine_odeso-SimpleGasTurbine-comp-1-T,SimpleGasTurbine-c1-1-T,SimpleGasTurbine-turb-1-T.ps}
   -- the temperatures at the output of the
   \begin{itemize}
   \item compressor,
   \item combustion chamber and
   \item turbine
   \end{itemize}
 \item Figure
-  \Ref{fig:SimpleGasTurbine_odeso.ps-SimpleGasTurbine-Heat,SimpleGasTurbine-Work}
+  \Ref{fig:SimpleGasTurbine_odeso-SimpleGasTurbine-fuel-1-Heat-1-y,SimpleGasTurbine-load-1-Work-1-y.ps}
   -- the heat input and work output
 \item Figure
-  \Ref{fig:SimpleGasTurbine_odeso.ps-SimpleGasTurbine-Speed} -- the shaft speed and
+  \Ref{fig:SimpleGasTurbine_odeso-SimpleGasTurbine-shaft-1-speed-1-y.ps} -- the shaft speed and
 \item Figure
-  \Ref{fig:SimpleGasTurbine_odeso.ps-SimpleGasTurbine-p1-P,SimpleGasTurbine-c1-P,SimpleGasTurbine-t1-P}
+  \Ref{fig:SimpleGasTurbine_odeso-SimpleGasTurbine-c1-1-P.ps}
   -- the pressure at the output of the
   \begin{itemize}
   \item compressor,
   \item combustion chamber and
   \item turbine