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latex/Kapitel/simulation.tex

@@ -1,5 +1,4 @@
-\chapter{Static Axisymmetric Rod}
-\label{cha:simulation}
+\chapter{Static Axisymmetric Rod}\label{cha:simulation}
 
 see appendix~\ref{apx:pub4}
 
@@ -93,8 +92,8 @@ lists a table of references to individual models and in which order to execute t
     \begin{tabular}{llll}
         \textbf{\#number} & \textbf{electromagnetic} & \textbf{thermal} & \textbf{mechanical} \\
         100 &  crank\_induction & crank\_heating \\
-        1 & -- & crank\_quench \\
-        -- & -- & -- & crank\_stress
+        1 & --- & crank\_quench \\
+        --- & --- & --- & crank\_stress
     \end{tabular}
 \end{center}
 
@@ -215,7 +214,14 @@ A {\ttfamily*VISCO} calculation then takes that thermal result as a volumetric t
 
 \section{Results}
 
-The results obtained by the thermal approximation were 
+Two of methods shall be presented to vizualize the simulated induction heating process:
+Areal stress distribution along the \ang{0} plane of the crankshaft as defined in section~\ref{sec:residual_stresses}.
+
+Stress distributions after heating (and thus, austenitization) are compared with those after quenching and subsequent air-cooling in figure~\ref{fig:plate-stress-distro}.
+After the heating time decribed in figure~\ref{fig:thermal-approx-curve} the zones of full austenitization and transition can be seen in all the left hand figures, but figure~\ref{fig:plate-stress-distro-ht} shows the austenitized zone as a compressive area.
+Quenching introduces higher compressive and tensile stresses, especially in the axial direction (fig.~\ref{fig:plate-stress-distro-qa}).
+
+The mechanisms of the stress evoltion can are examined in figures~\ref{fig:time_data_ax_h}--\ref{fig:time_data_tan_q} 
 
 
 \begin{figure}[p]
@@ -223,12 +229,12 @@ The results obtained by the thermal approximation were
     \begin{tabular}{cc}
         \subfloat[Radial Stresses after heating]{\includegraphics[width = 0.45\linewidth]{Abbildungen/kw-th-heating-S-Rad.png}} &  
         \subfloat[Radial Stresses after quenching]{\includegraphics[width = 0.45\linewidth]{Abbildungen/kw-th-aircool-S-Rad.png}} \\
-        \subfloat[Tangential Stresses after heating]{\includegraphics[width = 0.45\linewidth]{Abbildungen/kw-th-heating-S-Tan.png}} &  
+        \subfloat[Tangential Stresses after heating\label{fig:plate-stress-distro-ht}]{\includegraphics[width = 0.45\linewidth]{Abbildungen/kw-th-heating-S-Tan.png}} &  
         \subfloat[Tangential Stresses after quenching]{\includegraphics[width = 0.45\linewidth]{Abbildungen/kw-th-aircool-S-Tan.png}} \\
         \subfloat[Axial Stresses after heating]{\includegraphics[width = 0.45\linewidth]{Abbildungen/kw-th-heating-S-Axi.png}} &  
-        \subfloat[Axial Stresses after quenching]{\includegraphics[width = 0.45\linewidth]{Abbildungen/kw-th-aircool-S-Axi.png}}
+        \subfloat[Axial Stresses after quenching\label{fig:plate-stress-distro-qa}]{\includegraphics[width = 0.45\linewidth]{Abbildungen/kw-th-aircool-S-Axi.png}}
     \end{tabular}
-    \caption[Stress component distribuiton of crankshaft.]{Sectional views of stress component distributions before and after quenching. It must be noted that the image scales of \textbf{(a)}, \textbf{(c)},and \textbf{(e)} are equalized but reduced by a factor 3 to those of \textbf{(b)}, \textbf{(d)}, and \textbf{(f)}.}\label{fig:plate-stress-distro}
+    \caption[Stress component distribuiton of crankshaft.]{Sectional views of stress component distributions before and after quenching. It must be noted that the image scales of \textbf{(a)}, \textbf{(c)},and \textbf{(e)} are equalized but their minimum and maximum values differ to those of \textbf{(b)}, \textbf{(d)}, and \textbf{(f)}.}\label{fig:plate-stress-distro}
 \end{figure}
 
 \begin{figure}[htbp]

latex/Kapitel/validation_data.tex

@@ -89,7 +89,7 @@ Some microscope analysis was also done on sample plates cut from rod samples, bu
 \subsection*{Sample Preparation}
 \subsection*{Results}
 
-\section{Residual Stresses and Austenite}
+\section{Residual Stresses and Austenite}\label{sec:residual_stresses}
 
 As explained in section~\ref{sec:sota_residual_stress}, measuring internal residual stresses of three-dimensional parts is always full of compromise. 
 For this thesis, a high spatial resolution of data points was accomplished by machining sample plates from the heat treated parts that could be examined through \acrshort{hexrd} at the particle accelerator at DESY, Hamburg.

latex/todo.md

@@ -28,7 +28,10 @@
 - [] Figures
 	- [X] Short captions for Index
 	- [] Unify Captions
+	- [] Check that all Images are labeled in english!
+
+- [] Spellchack!!
 
 - [] Style
-	- [] Cpatialize references or no?
+	- [] Capitalize references or no?
 	- [] chack all dashes ?