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\large{\textbf{IAES-2024-Paper ID (YYY)}}\\ \vspace{0.15cm}
\small{\textbf{Proceedings of the International Conference on Advances in Aerospace and Energy Systems\\ April 04-06, 2024, Liquid Propulsion Systems Centre (ISRO), Thiruvananthapuram-695547, Kerala, India}} \\
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\begin{document}
\title{\LARGE{\vspace{5mm} \bf This Sample of a Full Paper for the IAES 2024 Proceedings was Prepared using LaTeX}\vspace{-9mm}}
\author{\textbf{Author A\textsuperscript{1}, Author B\textsuperscript{2}, Author C\textsuperscript{3*}, and Author D\textsuperscript{1}}\\
\textsuperscript{1}\small{Department of Aerospace Engineering, IIST, Thiruvananthapuram-695547, India }\\
\textsuperscript{2} \small{Centre for High Energy Physics, IISc, Bengaluru-560012, India }\\
\textsuperscript{3} \small{Planetary Sciences Division, PRL, Ahmedabad-380009, India \vspace{2mm}}\\
\textsuperscript{*} \small{\hspace{-1mm}Corresponding author: author.c@prl.res.in \vspace{-2.5mm}}}
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\vspace{1mm}
\begin{abstract}
\noindent {Write your abstract here. Limit the abstract to 200 words. This will contain a brief introduction to the paper, and a summary of the salient results and conclusions.}
\end{abstract}
\vspace{1.5mm}
\noindent
\raggedright{\textbf{Keywords:} Insert 3-4 keywords, separated by comma, that categorize your work}
\vspace{2.5mm}
\end{@twocolumnfalse}
]
\noindent
\section*{\textbf{NOMENCLATURE \vspace{2mm}}}
\begin{tabular}{ccc}
$A$ & Frontal area of rotor & [m$^2$]\\
$Re$ & Reynolds number & -- \\
$\epsilon$ & Dissipation & --
\end{tabular}
\section{{\textbf{INTRODUCTION}}}
Write your introduction section here in 10 point Times New Roman. The introduction part should give the necessary background / motivation behind the work. The citations of others’ work may be bracketed \cite{Gsell2017,Panton2009} appropriately \cite{Pascal2000}.
\section{\textbf{LITERATURE REVIEW AND OBJECTIVE}}\label{sec2}
This subsection should contain the literature review and the objective of the work undertaken Write text matter here in. Necessary citations may be bracketed \cite{Panton2009,raj2013wettability,prasanna2020analysis,suman2015performance,Pascal2000} appropriately.
\section{\textbf{MATERIALS AND METHODOLOGY}}
Write your texts here. This part should contain the necessary matters related to computational, experimental and analytical investigations. All Figures / Tables are to be cited within the texts. The Figure/Table captions must be written as indicated here. The Figure caption should appear at the bottom of the Figure, while the Table caption should appear on top of the Table. This is the standard practice.
\begin{eqnarray}
\frac{\partial u_i}{\partial x_i}&=&0 \label{eq1} \\
\frac{\partial u_i}{\partial t} + \frac{\partial (u_i u_j)}{\partial x_j} &=& -\frac{\partial p}{\partial x_i} + \sqrt{\frac{Pr}{Ra}}\frac{\partial^2 u_i}{\partial x_j \partial x_j} + \delta_{iy}\theta \label{eq2} \\
\frac{\partial \theta}{\partial t} + \frac{\partial (u_j \theta)}{\partial x_j} &=&
\sqrt{\frac{1}{RaPr}}\frac{\partial^2 \theta}{\partial x_j \partial x_j}
\label{eq3}
\end{eqnarray}
where, $x_i (i=1,2, 3)$ represent the spatial coordinates ($x,y,z$) with $y$ being the vertical direction, $u_i(u, v,w)$ are the velocity components, $p$ the pressure and $\theta$ the normalized temperature ($\theta=(T-T_C)/(T_H-T_C)$) with $T$ is the instantaneous temperature and $T_H$, $T_C$ are, respectively, the temperature of the hot and cold plates. We have used $H,~\sqrt{g \alpha \Delta T H}$ and $~(T_H-T_C)$ as the scales for normalization of length, velocity and temperature, respectively. Equations \ref{eq1}-\ref{eq3} are discretized using finite volume framework. The same could be written as finite volume framework is used to discretize Eqs. \ref{eq1}-\ref{eq3}. No-slip condition is implemented for all the velocity components on the walls, while for temperature, isothermal condition is applied on the horizontal walls and no-flux (adiabatic) conditions is applied on the vertical walls. Hence, at the top and bottom solid walls, the temperature takes specified values (0 and 1).
\subsection{\textbf{Validation}}\label{sec2p1}
The simulation details are given in the Table~\ref{table2}. To validate our code we computed the Nusselt numbers through three different ways \cite{Panton2009}: (a) using the mean heat flux at the horizontal surfaces near the hot and bottom plates ($Nu_S$), (b) using the heat dissipation ($Nu_{\epsilon_T}={(RaPr)}^{1/2}<\epsilon_T>_{global}$), and (c) using the viscous dissipation ($Nu_{\epsilon_u}={(RaPr)}^{1/2}<\epsilon_u>_{global}+1$).
\begin{figure}
\centering
\includegraphics[width=0.8\textwidth]{figure1.eps}
\caption{Variations of the percentage volume occupied by the plume and the background in the cubic cell with $Ra$ for different threshold value $\delta$.}
\label{figure1}
\end{figure}
\section{\textbf{RESULTS AND DISCUSSION}}\label{sec3}
All the figures and Tables should be referred in order of their appearances. Figure \ref{figure1} should be written if it appears at the start of a sentence, while Fig. \ref{figure1} is the correct way otherwise. However, Table \ref{table2} should appear in full irrespective of its position. The validation were presented in Sec.~\ref{sec2p1}.
Discussion of the results is to be written here. All Figures are to be cited within the text. Results obtained may be compared with the published data wherever applicable/possible through necessary citations in bracketed form \cite{krishna2012integrative,prasanna2020analysis}.
\begin{table}
\centering
\caption{The values of the fitting parameters}%\vspace{-10pt}
\begin{tabular}{|c|c|c|c|c|}
\hline
$\delta(\%)$ & $A_{pl}$ & $\beta_{pl}$& $A_{bg}$ &$\beta_{bg}$ \\
\hline
$0$&$0.138$ &$-0.197$ &$0.553$ & $-0.269$\\
$0.1$&$0.115$ &$-0.198$ &$0.838$ &$-0.279$ \\
$1$&$0.072$ &$-0.182$ &$0.919$ &$-0.287$ \\
$5$&$0.033$ &$-0.144$ &$0.531$ &$-0.265$\\
$10$&$0.02$ &$-0.118$ &$0.377$ &$-0.248$\\
\hline
\end{tabular}
\label{table2}
\end{table}
In RBC one of the central theme of the turbulent research is to get the scalings for the dissipation rates and further establish its connection with the nature of heat transport in the turbulent state \cite{Pascal2000}. A plume can be defined in the region where there is strong correlation between the vertical velocity ($w$) and the temperature fluctuations defined as $\theta(\textbf{x},t)=T(\textbf{x},t)-\langle T(z)\rangle_{A,t}$ where, $<.>_{A,t}$ is the averaged over horizontal plane and the time, exists.
\begin{figure}
\centering
\includegraphics[width=0.8\textwidth]{figure2.eps}
\caption{Variations of the contribution of the plumes and the background to the heat dissipation rates with the Rayleigh number.}
\label{fig:3}
\end{figure}
All the references that appear in the section ``REFERENCES" should be cited appropriately in the text.
\section{\textbf{CONCLUSIONS}}\label{sec4}
The key findings of the work are to be placed here. The conclusion part should be qualitative and quantitative.
\vspace{0.1cm}
\noindent
\section*{\textbf{ACKNOWLEDGEMENTS}}
\noindent If the authors want to acknowledge any person, institute, or facilities, it may be done here.
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\noindent
\textbf{Notes to Author(s)}
\begin{itemize}
\item{The full paper is restricted to a maximum of 6 pages.}
\item{In each section, sub-sectioning if required, can be done appropriately.}
\item{The full paper manuscript filename should be ``IAES-2024-Paper ID''}
\item{Once the paper is compiled, remove all the instructions, if any, in this template.}
\item{Please remove this ``Notes to Author(s)'' in the submission.}
\end{itemize}
\end{document}
