thanks,
gsal
Code: Select all
\begin{minipage}[b]{0.58\textwidth}
\begin{itemize}
\item Note that the CFD mass flow had to be multiplied by 18 (since only 20 degree sector was modeled) and then divided by 1.1275428 (the density when TCOOL=40\,$^\circ C$). The temperature had to be converted to $^\circ C$ and also corrected due to the CFD rotor duct length (of 3 inches) and converted from total to static temperature. Also the vent scoop flow was evenly divided and added to the last four rotor ducts.
\item Blower pressure=4599$Pa$, exhaust pressure=1049.94$Pa$, and intake pressure=3741.92$Pa$ -- same as the CFD boundary conditions.
\item The loss coefficient from the blower to the airgap, CEN, was set to 0.72 and the corresponding reference area, AEN, was set to 273431 mm. Note that the value for CEN was arbitrarily set to match the CFD airgap pressures at the beginning of the airgap.
\item The loss coefficients for the stator vents were calculated from CFD results using the same Fluent UDF that was previously created for setting the loss coefficients for TG3503. See the attached .pdf files below for details.
\end{itemize}
\begin{quote}
\attachfile[icon=Paperclip]{air-gap.pdf} air-gap.pdf \\ \\
\attachfile[icon=Paperclip]{method.pdf} method.pdf
\end{quote}
\end{minipage}
\hspace{0.5cm}
\begin{minipage}[b]{0.15\textwidth}
\begin{tabular}{|p{1.5cm}|p{2cm}|p{1.cm}|}
\hline
Rotor Vent No. & Volume flow ($m^3/s$) & Ts ($^\circ C$) \\
\hline
1 & 0.236519478 & 49.50 \\
2 & 0.230733088 & 49.37 \\
3 & 0.220691624 & 49.25 \\
4 & 0.212382880 & 49.17 \\
5 & 0.204646381 & 49.11 \\
6 & 0.198191839 & 49.08 \\
7 & 0.192881787 & 49.07 \\
8 & 0.186177887 & 49.07 \\
9 & 0.180839064 & 49.05 \\
10 & 0.176753425 & 48.99 \\
11 & 0.173361514 & 48.93 \\
12 & 0.168978563 & 48.88 \\
13 & 0.166117338 & 48.85 \\
14 & 0.164573235 & 48.85 \\
15 & 0.164713898 & 48.88 \\
16 & 0.164173622 & 48.94 \\
17 & 0.162926831 & 48.98 \\
18 & 0.162997163 & 48.98 \\
19 & 0.163703678 & 48.94 \\
20 & 0.165068754 & 48.88 \\
21 & 0.167060423 & 48.81 \\
22 & 0.169576384 & 48.74 \\
23 & 0.172533517 & 48.66 \\
24 & 0.753677541 & 48.57 \\
25 & 0.756091201 & 48.47 \\
26 & 0.758626343 & 48.35 \\
27 & 0.761151894 & 48.21 \\
\hline
\end{tabular}
\end{minipage}