diff --git a/tex/header/preamble.tex b/tex/header/preamble.tex
index 83e7cafd8d5e465d9c2dbbe5fd3d9eb075d4314e..08f4b5853a90a5ead99191e4f771bec67cc60b98 100644
--- a/tex/header/preamble.tex
+++ b/tex/header/preamble.tex
@@ -1,6 +1,6 @@
 %! TEX program = lualatex
 
-\documentclass{scrartcl}
+\documentclass[landscape]{scrartcl}
 \usepackage[margin=1cm, bottom=2.5cm]{geometry}
 %   \RedeclareSectionCommand % das kommt vom KOMA-Skript
 %     [beforeskip=-1.5ex plus -.1ex minus -.1ex,
diff --git a/tex/main.tex b/tex/main.tex
index 0901c4ef0588e8885edb9923a9d8005120a81644..842dc81c6fee45a6551959fedb16e028fc82df51 100644
--- a/tex/main.tex
+++ b/tex/main.tex
@@ -5,6 +5,7 @@
 \author{Felix Hilsky}
 \maketitle
 % use \textinput as described in /header and _TEMPLATE
+{\scriptsize This document is set in landscape to show the tables without special formattling.}
 \textinput{setup}
 \textinput{reynold.tex}
 \textinput{results}
diff --git a/tex/results.tex b/tex/results.tex
index 37e08c0b45632c3f0909401f046aeec73ad93764..878035236fa45e495d266a66bda93ff781991e7f 100644
--- a/tex/results.tex
+++ b/tex/results.tex
@@ -28,6 +28,9 @@ For the Nusselt number Churchill and Berstein found the following formula in ter
 The results of this equation are listed in table \ref{tab:values}.
 
 For reference values for the drag coefficiant we can refer to the paper \textcite{same} which solved the same problem for $\Rey = 100, 1000$ and $3900$.
+The values for $100$ and $1000$ are inserted into table \ref{tab:values} for comparison.
+
+\textcite[4.1.1 The laminar flow][5]{same} reports that at $\Rey = 100$ a steady state is reached after \SI{15}{\second}. This was not confirmed by my experiments: the visual inspection indicated a stabilisation around \SIrange{60}{80}{\second}. The development of the drag coefficiant over time indicates stabilisation at around \SI{}{\second}.?? % check at end
 
 \section{Measurements}
 The drag coefficiant was calculated with the OpenFOAM intrinsic function
@@ -42,9 +45,13 @@ The results are summerized in table \ref{tab:values}.
   \centering
   \caption{Scalar results of the numerical experiments. ref-$\Nus$ is the Nusselt number according to the Churchill-Bernstein equation.}
   \label{tab:values}
-  \begin{tabular}{ccccccc}
-    $\Rey$ & $u_{in}$ & \# cells & $C_D$ & $\vec n · ∇T\vert_{\text{cyl}}$ & $\Nus$ & ref-$\Nus$\\
-    \num{e2} & \num{0.05} & & & & & 5.1%56
+  \begin{tabular}{cccccccccc}
+    $\Rey$ & $u_{in}$ & \# cells & $Δt$ & $t_{\max}$ $C_D$ & $\vec n · ∇T\vert_{\text{cyl}}$ & ref-$C_D$ & $\Nus$ & ref-$\Nus$\\
+    \num{e2} & \num{0.05} & 1664 & &  & & 5.1%56
+    \\
+    \num{e2} & \num{0.05} & 6656 & & & & 5.1%56
+    \\
+    \num{e2} & \num{0.05} & 26624 & & & & 5.1%56
     \\
     \num{e3} & \num{0.5} & & & & & 15%.930
     \\
diff --git a/tex/setup.tex b/tex/setup.tex
index 94382e2fce86aa7b1cdf16d736ef595c0e9e042f..0d506ee05a1e5e6d813415a8a8fa260cb84ee5b4 100644
--- a/tex/setup.tex
+++ b/tex/setup.tex
@@ -31,8 +31,8 @@ The mesh at $N=1$ is displayed in figure \ref{fig:mesh}.
 
 \begin{figure}[htpb]
   \centering
-  \includegraphics[width=0.95\linewidth]{.maindir/zeichnungen/mesh}  % check at end
-  \includegraphics[width=0.95\linewidth]{.maindir/zeichnungen/meshcloseup}  % check at end
+  \includegraphics[width=0.95\linewidth,height=0.4\textheight,keepaspectratio]{.maindir/zeichnungen/mesh}  % check at end
+  \includegraphics[width=0.95\linewidth,height=0.4\textheight,keepaspectratio]{.maindir/zeichnungen/meshcloseup}  % check at end
   \caption{The mesh at $N=1$. As mentioned in the description the resolution at the cylinder wall is very high and therefore a second close-up view of the cylinder is displayed here (which is still too big). For orientation the corners of the arked square are marked red.}%
   \label{fig:mesh}
 \end{figure}