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5 changes: 5 additions & 0 deletions Chapters/00Abstract.tex
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\renewcommand{\abstractname}{\vspace{-\baselineskip}} % https://tex.stackexchange.com/questions/42482/remove-abstract-title-from-abstract
\begin{abstract} \bfseries

These instructions give you guidelines for preparing papers for AIAA Technical Papers using \LaTeX{}. Define all symbols used in the abstract. Do not cite references in the abstract. The footnote on the first page should list the Job Title and AIAA Member Grade for each author, if known Authors do not have to be AIAA members.
\end{abstract}
137 changes: 137 additions & 0 deletions Chapters/01Nomenclature.tex
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%%% Nomenclature Code
% incorporate https://tex.stackexchange.com/questions/112884/how-to-achieve-nomenclature-entries-like-symbol-description-dimension-and-uni

\newcommand{\DimensUnits}[2]{\hfill\makebox[8em]{#1\hfill}%
\makebox[5em]{#2\hfill}\ignorespaces} % first number related to 'dimensions' box size, second number related to 'units' box size
\newcommand{\DefinitionCol}[1]{\hfill\parbox[t]{13em}{#1}\ignorespaces} % number related to 'definition' box size


\newcommand{\nomsubtitle}[1]{\item[\Large\bfseries #1]}
\renewcommand\nomgroup[1]{%
\itemsep0pt % just disable this line if you do not want spacing
\vspace{10pt}
\def\nomtemp{\csname nomstart#1\endcsname}\nomtemp
}

\newcommand{\nomstartA}{\nomsubtitle{Acronyms}%
\item[\bfseries Symbol]\textbf{Description}}
\newcommand{\nomstartD}{\nomsubtitle{Dimensionless numbers}%
\item[\bfseries Symbol]\textbf{Description}\DefinitionCol{\textbf{Definition}}}

\newcommand{\nomstartR}{\nomsubtitle{Latin symbols}% % R for Roman
\item[\bfseries Symbol]%
\textbf{Description}\DimensUnits{\textbf{Dimensions}}{\textbf{Units}}}
\newcommand{\nomstartG}{\nomsubtitle{Greek symbols}%
\item[\bfseries Symbol]%
\textbf{Description}\DimensUnits{\textbf{Dimensions}}{\textbf{Units}}}

\newcommand{\nomstartS}{\nomsubtitle{Superscripts}%
\item[\bfseries Symbol]\textbf{Description}}
\newcommand{\nomstartU}{\nomsubtitle{Subscripts}%
\item[\bfseries Symbol]\textbf{Description}}

\renewcommand*{\nompreamble}{
\markboth{\nomname}{\nomname}
%\begin{multicols*}{2}
}
\renewcommand{\nompostamble}{}%\end{multicols*}}

\newcommand{\nomdescr}[1]{\parbox[t]{8cm}{\RaggedRight #1}} % the cm box changes the size of the description box
\newcommand{\nomwithdim}[5]{\nomenclature[#1]{#2}%
{\nomdescr{#3}\DimensUnits{#4}{#5}}}

\newcommand{\nomtypeA}[3][]{\nomenclature[A#1]{#2}{#3}}
\newcommand{\nomtypeD}[4][]{\nomenclature[D#1]{#2}{\nomdescr{#3}\DefinitionCol{#4}}}
\newcommand{\nomtypeR}[5][]{\nomwithdim{R#1}{#2}{#3}{#4}{#5}}
\newcommand{\nomtypeG}[5][]{\nomwithdim{G#1}{#2}{#3}{#4}{#5}}
\newcommand{\nomtypeS}[3][]{\nomenclature[S#1]{#2}{#3}}
\newcommand{\nomtypeU}[3][]{\nomenclature[U#1]{#2}{#3}}
\makenomenclature

\mbox{}

%%% NOMENCLATURE GOES BELOW
% Dimensions based on https://www.ldeo.columbia.edu/~martins/hydro/case_studies/units_dimensions.html
\newcommand{\Lunit}{\textrm{L}} % length unit for MLT system
\newcommand{\Munit}{\textrm{M}} % mass unit for MLT system
\newcommand{\Tunit}{\textrm{T}} % time unit for MLT system
\newcommand{\Qunit}{\textrm{Q}} % temperature unit for MLT system

% ADD ACRONYMS HERE
\nomtypeA{ROI}{Reality of interest}
\nomtypeA{BEM}{Blade element momentum theory}
\nomtypeA{RPM}{Revolutions per minute}
\nomtypeA{tol}{Tolerance}
\nomtypeA{TUI}{Text user interface}
\nomtypeA[ZZZ]{}{} % make sure to finish off with this, fixes small issue with spacing on the last line

% ADD DIMENSIONLESS NUMBERS HERE
\nomtypeD{\( \Re \)}{Reynolds number}{\(\displaystyle \frac{U L}{\nu} \)}
\nomtypeD[ZZZ]{}{}{} % make sure to finish off with this, fixes small issue with spacing on the last line

% ADD GREEK SYMBOLS HERE
\nomtypeG{\( \gamma \)} {Yaw angle}{--}{\si{\degree}}
\nomtypeG{\( \chi \)} {Wake skew angle}{--}{\si{\degree}}
\nomtypeG{\( \psi \)} {Azimuthal angle}{--}{\si{\degree}}
\nomtypeG{\( \phi \)} {Inflow angle}{--}{\si{\degree}}
\nomtypeG{\( \alpha \)} {Angle of attack}{--}{\si{\degree}}
\nomtypeG{\( \beta \)} {Blade twist angle}{--}{\si{\degree}}
\nomtypeG{\( \theta \)} {Collective pitch angle}{--}{\si{\degree}}
\nomtypeG{\( \epsilon \)}{Error}{--}{--}
\nomtypeG{\( \mu \)} {Normalized radial position}{--}{--}
\nomtypeG{\( \rho \)} {Air density}{\( \Munit\Lunit^{-3} \)}{\si{\kilogram\per\meter\cubed}}
\nomtypeG{\( \Omega \)} {Radial velocity}{\( \Tunit^{-1} \)}{\si{\radian\per\second}}
\nomtypeG{\( \omega \)} {Vorticity}{\( \Tunit^{-1} \)}{\si{\per\second}}
\nomtypeG{\( \sigma_r \)} {Blade solidity}{--}{--}
\nomtypeG{\( \Gamma \)} {Circulation}{\( \Lunit^{2} \Tunit^{-1} \)}{\si{ \meter \squared \per \second}}
\nomtypeG{\( \lambda \)} {Tip speed ratio}{--}{--}
\nomtypeG[ZZZ]{}{}{}{} % make sure to finish off with this, fixes small issue with spacing on the last line

% ADD ROMAN SYMBOLS HERE
\nomtypeR{\( U_{\infty} \)}{Free-stream velocity}{\( \Lunit\Tunit^{-1} \)}{\si{\meter\per\second}}
\nomtypeR{\( V_{a} \)} {Axial velocity}{\( \Lunit\Tunit^{-1} \)}{\si{\meter\per\second}}
\nomtypeR{\( V_{t} \)} {Tangential velocity}{\( \Lunit\Tunit^{-1} \)}{\si{\meter\per\second}}
\nomtypeR{\( W \)} {Total effective velocity}{\( \Lunit\Tunit^{-1} \)}{\si{\meter\per\second}}
\nomtypeR{\( L \)} {Lift}{\( \Munit\Lunit\Tunit^{-2} \)}{\si{\newton}}
\nomtypeR{\( F \)} {Force}{\( \Munit\Lunit\Tunit^{-2} \)}{\si{\newton}}
\nomtypeR{\( D \)} {Drag}{\( \Munit\Lunit\Tunit^{-2} \)}{\si{\newton}}
\nomtypeR{\( C_p \)} {Power coefficient}{--}{--}
\nomtypeR{\( C_T \)} {Thrust coefficient}{--}{--}
\nomtypeR{\( C_l \)} {Sectional lift coefficient}{--}{--}
\nomtypeR{\( C_d \)} {Sectional drag coefficient}{--}{--}
\nomtypeR{\( a \)} {Axial induction factor}{--}{--}
\nomtypeR{\( a' \)} {Azimuthal induction factor}{--}{--}
\nomtypeR{\( h \)} {ISA altitude}{\( \Lunit \)}{\si{\meter}}
\nomtypeR{\( p \)} {Static pressure}{\( \Munit\Lunit^{-1}\Tunit^{-2} \)}{\si{\pascal}}
\nomtypeR{\( T \)} {Static temperature}{\( \Qunit \)}{\si{\kelvin}}
\nomtypeR{\( N_b \)} {Number of blades}{--}{--}
\nomtypeR{\( C_v \)} {Specific volumetric heat capacity}{\( \Lunit^2\Qunit^{-1}\Tunit^{-2} \)}{\si{\joule\per\kilogram\per \kelvin}}
\nomtypeR{\( N_r \)} {Number of annuli elements}{--}{--}
\nomtypeR{\( N_{\psi} \)}{Number of azimuthal elements}{--}{--}
\nomtypeR{\( c \)} {Chord length}{\( \Lunit \)}{\si{\meter}}
\nomtypeR{\( A \)} {Surface area}{\( \Lunit^2 \)}{\si{\meter\squared}}
\nomtypeR{\( t \)} {Time}{\( \Tunit \)}{\si{\second}}
\nomtypeR{\( n \)} {Rotational velocity}{\( \Tunit^{-1} \)}{\si{\per\second}}
\nomtypeR{\( P \)} {Power}{\( \Munit\Lunit^2\Tunit^{-3} \)}{\si{\watt}}
\nomtypeR{\( Q \)} {Torque}{\( \Munit\Lunit^2\Tunit^{-2} \)}{\si{\newton\meter}}
\nomtypeR{\( D \)} {Rotor diameter}{\( \Lunit \)}{\si{\meter}}
\nomtypeR{\( f \)} {Prandtl root/tip correction factor}{--}{--}
\nomtypeR{\( h \)} {Specific stagnation enthalpy}{\( \Lunit^{2}\Tunit^{-2} \)}{\si{\joule\per\kilogram}}
\nomtypeR{\( r \)} {Radial position}{\( \Lunit \)}{\si{\meter}}
\nomtypeR[ZZZ]{}{}{}{} % make sure to finish off with this, fixes small issue with spacing on the last line

% ADD SUPERSCRIPTS HERE
\nomtypeS{\( n \)}{time step}
\nomtypeS[ZZZ]{}{} % make sure to finish off with this, fixes small issue with spacing on the last line

% ADD SUBSCRIPTS HERE
\nomtypeU{\( \infty \)}{free stream}
\nomtypeU{\( \textrm{disk} \)}{Rotor disk}
\nomtypeU{\( \textrm{0} \)}{Disk averaged}
\nomtypeU{\( \bar{\psi} \)}{Azimuthal averaged}
\nomtypeU{\( x \)}{$x$-direction}
\nomtypeU{\( y \)}{$y$-direction}
\nomtypeU[ZZZ]{}{} % make sure to finish off with this, fixes small issue with spacing on the last line

\printnomenclature[6em] % change spacing between symbol and description
\newpage
181 changes: 181 additions & 0 deletions Chapters/02Introduction.tex
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\chapter{Introduction}

WORK IN PROGRESS

This template

when there exists an author with last name prefix of 'van', use the \textbackslash VAN command , and follow it up with a \textasciitilde (see reference for example)


\citet*{Allen2002}

\citet*{Bettini2021}

\citet*{Eitelberg2020}

\citet*{Sinnige2020}

\citet*{Herrez2016}


\chapter{Examples}

\section{Tables}

\subsection{tabularx}

\begingroup
\renewcommand\tabularxcolumn[1]{m{#1}} % https://latex.org/forum/viewtopic.php?t=32433

\begin{minipage}[t]{0.48\textwidth}
\begin{table}[H]
\centering
\caption{Fuselage geometry \cite[Tab.~4]{Bettini2021}}
\label{tab:fuselage_geom}
{\footnotesize
\begin{tabularx}{\textwidth}[t]{X|rl} \toprule
\multicolumn{1}{c|}{\textbf{Parameter}} &
\multicolumn{2}{c}{\textbf{Value}} \\ \midrule
Length & 1.342 & \si{\meter} \\
Diameter & 0.140 & \si{\meter} \\
Volume & 0.0160632 & \si{\meter\cubed} \\
Volume of aft support strut (estimate) & 0.0004491 & \si{\meter\cubed} \\
Volume of wing support struts (estimate for both struts together) & 0.0035296 & \si{\meter\cubed} \\ \bottomrule
\end{tabularx}
}
\end{table}
\end{minipage}
\hfill
\begin{minipage}[t]{0.48\textwidth}
\begin{table}[H]
\centering
\caption{Propeller geometry \cite[Tab.~8]{Bettini2021}}
\label{tab:prop_geom}
{\footnotesize
\begin{tabularx}{\textwidth}[t]{X|rl} \toprule
\multicolumn{1}{c|}{\textbf{Parameter}} &
\multicolumn{2}{c}{\textbf{Value}} \\ \midrule
Number of blades & 6 & \\
Diameter & 0.2032 & \si{\meter} \\
Pitch angle at $r/R = 0.7$ & 45 & deg \\
Rotation direction (from rear) & CW & 2x \\
& CCW & 1x \\ \bottomrule
\end{tabularx}
}
\end{table}
\end{minipage}

\begin{table}[H]
\caption{Wing geometry \cite[Tab.~5]{Bettini2021}}
\label{tab:wing_geom}
\begin{subtable}[t]{0.48\textwidth}
\centering
{\footnotesize
\begin{tabularx}{\textwidth}[t]{X|rl} \toprule
\multicolumn{1}{c|}{\textbf{Parameter}} &
\multicolumn{2}{c}{\textbf{Value}} \\ \midrule
Span & 1.397 & \si{\meter} \\
Area & 0.2172 & \si{\meter\squared} \\
Mean aerodynamic chord & 0.165 & \si{\meter} \\
Aspect ratio & 8.98 & \\
Taper ratio & 0.40 & \\
Sweep angle at $0.25c$ & 0 & deg \\
Incidence angle & 0 & deg \\
Dihedral angle & 4 & deg \\
Twist & 2 & deg \\ \bottomrule
\end{tabularx}
}
\end{subtable}
\hfill
\begin{subtable}[t]{0.48\textwidth}
\centering
{\footnotesize
\begin{tabularx}{\textwidth}[t]{X|rl} \toprule
\multicolumn{1}{c|}{\textbf{Parameter}} &
\multicolumn{2}{c}{\textbf{Value}} \\ \midrule
Airfoil (constant over span) & DU 96-150 & \\
Aileron span & 0.197 & \si{\meter} \\
Aileron spanwise position & 0.71 < y/(b/2) < 0.99 & \\
Aileron chord & 0.029 & \si{\meter} \\
Flap span (per side) & 0.369 & \si{\meter} \\
Flap chord & 0.060 & \si{\meter} \\
Wing $0.25c$ from fuselage nose & 0.680 & \si{\meter} \\
Volume & 0.0030229 & \si{\meter\cubed} \\ \bottomrule
\end{tabularx}
}
\end{subtable}
\end{table}

\endgroup


\section{Graphs}

\subsection{subfigures}
\begin{figure}[H]
\centering
\begin{subfigure}[t]{0.48\textwidth}
\centering
\includegraphics[width=1.0\textwidth]{Images/graph.jpg}
\caption{graph 1}
\label{subfig:graph1}
\end{subfigure}
\hfill
\begin{subfigure}[t]{0.48\textwidth}
\centering
\includegraphics[width=1.0\textwidth]{Images/graph.jpg}
\caption{graph 2}
\label{subfig:graph2}
\end{subfigure}
\bigskip
\begin{subfigure}[t]{0.48\textwidth}
\centering
\includegraphics[width=1.0\textwidth]{Images/graph.jpg}
\caption{graph 3 help help help help help help help help help help help help help}
\label{subfig:graph3}
\end{subfigure}
\hfill
\begin{subfigure}[t]{0.48\textwidth}
\centering
\includegraphics[width=1.0\textwidth]{Images/graph.jpg}
\caption{graph 4}
\label{subfig:graph4}
\end{subfigure}
\caption{graphs (subfigures)}
\label{fig:graph_subfigures}
\end{figure}

\subsection{Continued float}
\begin{figure}[H]
\centering
\begin{subfigure}[t]{0.48\textwidth}
\centering
\includegraphics[width=1.0\textwidth]{Images/graph.jpg}
\caption{graph 5}
\label{subfig:graph5}
\end{subfigure}
\hfill
\begin{subfigure}[t]{0.48\textwidth}
\centering
\includegraphics[width=1.0\textwidth]{Images/graph.jpg}
\caption{graph 6}
\label{subfig:graph6}
\end{subfigure}
\end{figure}%
\begin{figure}[H]\ContinuedFloat
\begin{subfigure}[t]{0.48\textwidth}
\centering
\includegraphics[width=1.0\textwidth]{Images/graph.jpg}
\caption{graph 7}
\label{subfig:graph7}
\end{subfigure}
\hfill
\begin{subfigure}[t]{0.48\textwidth}
\centering
\includegraphics[width=1.0\textwidth]{Images/graph.jpg}
\caption{graph 8}
\label{subfig:graph8}
\end{subfigure}
\caption{graphs (continued float)}
\label{fig:graph_contfloat}
\end{figure}
61 changes: 61 additions & 0 deletions Chapters/A_Appendix.tex
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%% If your highest level are chapters, then use this line!
\newcommand\invisibleappendix[1]{ % makes an invisible appendix header!
\addcontentsline{toc}{chapter}{\protect{\thechapter}#1}%
\chaptermark{#1}}

%% If your highest level are parts, then use this line below instead!
% \newcommand\invisibleappendix[1]{ % makes an invisible appendix header!
% \addcontentsline{toc}{part}{\protect{\thechapter}#1}%
% \chaptermark{#1}}

\renewcommand{\thesection}{\Alph{section}}
\renewcommand{\thesubsection}{\Alph{section}.\arabic{subsection}}
\renewcommand{\sectionmark}[1]{\markboth{#1}{}}
\renewcommand{\subsectionmark}[1]{\markright{#1}} % If this was not enabled in the main file.

\titleformat{\section}
{\Large\bfseries}
{Appendix \Huge{\thesection}\space}{5pt}{#1}[]
\titlespacing{\section}{0pt}{0.5\baselineskip}{0pt}

\titleformat{\subsection}
{\bfseries}
{\thesubsection\space}{5pt}{#1}[]
\titlespacing{\section}{0pt}{0.5\baselineskip}{0pt}

\newpage
\pagestyle{appendix}
\appendix
% \markboth{APPENDICES}{APPENDICES} % Solution to wrong header name provided in https://latex.org/forum/viewtopic.php?t=19574
\invisibleappendix{Appendices}

%%% GENERAL FORMAT OF APPENDICES:

% \section{TEST}
% \startcontents[sections]
% \printcontents[sections]{l}{1}[2]
% DESCRIPTOR

% \subsection{A}
% \subsection{B}

% \stopcontents[sections]

\section{Appendix First}
\label{app:AppendixFirst}

\startcontents[sections]
\printcontents[sections]{l}{1}[2]

blablablabla

\newpage

\invisiblesubsection{Appendix Second}
blabla





\stopcontents[sections]
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