我浏览了论坛，发现了一些关于此问题的问题，但大多数问题都建议更改为不同的环境。我需要 longtable，因为它将分为 2 页。用户 @Zarko 要求我给出 MWE：
它的编译如下：
这是 MWE（所有额外的内容都是因为它是从较长的文档中提取出来的）：
\documentclass[12pt, a4paper]{report}
\usepackage[utf8]{inputenc}
\usepackage{graphicx}
\usepackage{amsmath}
\usepackage{float}
\setlength{\parskip}{1em}
\usepackage[a4paper, total={6in, 8in}]{geometry}
\graphicspath{ {images/} }
\newcommand{\degree}{\ensuremath{^\circ}}
\newcommand{\quotes}[1]{``#1''}
\setlength\parindent{0pt}
\usepackage[utf8]{inputenc}
\usepackage[T1]{fontenc}
\usepackage{imakeidx}
\makeindex[columns=3, title=Alphabetical Index, intoc]
\usepackage[spanish,es-nodecimaldot]{babel}
\usepackage[sorting=none]{biblatex}
\addbibresource{Bibfile.bib}
\DeclareMathOperator\grad{grad}
\DeclareMathOperator\prima{'}
\DeclareMathOperator\sen{sen}
\usepackage{array}
\usepackage{tabularx}
\usepackage{lscape}
\usepackage{caption}
\captionsetup[table]{position=bottom}
\usepackage{booktabs}
\usepackage{mathptmx}
\usepackage[per-mode=symbol]{siunitx}
\usepackage{bm}
\usepackage{amsmath}
\newcolumntype{L}[1]{>{\raggedright\arraybackslash}p{#1}}
\newcolumntype{C}[1]{>{\centering\arraybackslash}p{#1}}
\usepackage{longtable}
\interfootnotelinepenalty=10000
\usepackage[spanish]{minitoc}
\usepackage{hyperref}
\usepackage{siunitx}
\sisetup{group-digits=false}
\usepackage{mathtools, nccmath}
\begin{document}
\begin{longtable}{ |L{4cm}|c|c|c|c| }
\caption[Datos de los alerones y spoilers de aviones semejantes.]{\label{aler_spoil}}
\endlastfoot
\hline
\multicolumn{5}{|c|}{\textbf{Alerones y Spoilers\footnote{Las definiciones son análogas a las dadas para dispositivos hipersustentadores.}}} \\
\hline
& Proyecto & \vtop{\hbox{\strut \makebox[2.5cm][c]{A319-100}\par }\hbox{\strut \makebox[2.5cm][c]{\cite{A319APM,JanesA319,A319TC,EurocontrolA319}}\par}} & \vtop{\hbox{\strut \makebox[2.5cm][c]{B737-700}\par }\hbox{\strut \makebox[2.5cm][c]{\cite{B737APM,JanesB737,B737TC,EurocontrolB737}}\par}} & \vtop{\hbox{\strut \makebox[2.5cm][c]{A220-300}\par }\hbox{\strut \makebox[2.5cm][c]{\cite{A220APM,JanesA220,A220TC,EurocontrolA220}}\par}} \\
\hline
Número de alerones por semiala & I/B: 0 O/B: 1 & I/B: 0 O/B: 1 & I/B: 0 O/B: 1 & I/B: 0 O/B: 1 \\
\hline
Número de spoilers por semiala\footnote{Al igual que con los slats, consideramos que los spoilers externos conforman un único dispositivo. De esta manera, empleamos los subíndices $sp\;I/B$ y $sp\;O/B$ para referirnos a los spoilers interno y externos, respectivamente.} & I/B: 1 O/B: 4 & I/B: 1 O/B: 4 & I/B:1 O/B: 5 & I/B:1 O/B: 4 \\
\hline
Envergadura (m) & \vtop{\hbox{\strut \makebox[3cm][c]{$b_a = 5.9214$}\par }\hbox{\strut \makebox[3cm][c]{$b_{sp\;I/B} = 3.1275$}\par}\hbox{\strut \makebox[3cm][c]{$b_{sp\;O/B} = 11.2382$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$b_a \approx 5.2692$}\par }\hbox{\strut \makebox[3cm][c]{$b_{sp\;I/B} \approx 2.7943$}\par}\hbox{\strut \makebox[3cm][c]{$b_{sp\;O/B} \approx 10.8577$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$b_a \approx 5.9551$}\par }\hbox{\strut \makebox[3cm][c]{$b_{sp\;I/B} \approx 4.7014$}\par}\hbox{\strut \makebox[3cm][c]{$b_{sp\;O/B} \approx 10.3430$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$b_a \approx 5.8881$}\par }\hbox{\strut \makebox[3cm][c]{$b_{sp\;I/B} \approx 4.0107$}\par}\hbox{\strut \makebox[3cm][c]{$b_{sp\;O/B} \approx 11.2641$}\par}} \\
\hline
Relación $b_{a,sp}/b$ & \vtop{\hbox{\strut \makebox[3cm][c]{$b_a/b = 0.1704$}\par }\hbox{\strut \makebox[3cm][c]{$b_{sp\;I/B}/b = 0.0900$}\par}\hbox{\strut \makebox[3cm][c]{$b_{sp\;O/B}/b = 0.3234$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$b_a/b \approx 0.1545$}\par }\hbox{\strut \makebox[3cm][c]{$b_{sp\;I/B}/b \approx 0.0082$}\par}\hbox{\strut \makebox[3cm][c]{$b_{sp\;O/B}/b \approx 0.3184$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$b_a/b \approx 0.1735$}\par }\hbox{\strut \makebox[3cm][c]{$b_{sp\;I/B}/b \approx 0.1370$}\par}\hbox{\strut \makebox[3cm][c]{$b_{sp\;O/B}/b \approx 0.3014$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$b_a/b \approx 0.1831$}\par }\hbox{\strut \makebox[3cm][c]{$b_{sp\;I/B}/b \approx 0.1247$}\par}\hbox{\strut \makebox[3cm][c]{$b_{sp\;O/B}/b \approx 0.3503$}\par}} \\
\hline
Distancia al plano de simetría del avión $y_{a,sp}$ (m) & \vtop{\hbox{\strut \makebox[3cm][c]{$y_a = 14.0599$}\par }\hbox{\strut \makebox[3cm][c]{$y_{sp\;I/B} = 4.8754$}\par}\hbox{\strut \makebox[3cm][c]{$y_{sp\;O/B} = 9.2122$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$y_a \approx 14.75$}\par }\hbox{\strut \makebox[3cm][c]{$y_{sp\;I/B} \approx 5.5$}\par}\hbox{\strut \makebox[3cm][c]{$y_{sp\;O/B} \approx 9.8997$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$y_a \approx 12.1452$}\par }\hbox{\strut \makebox[3cm][c]{$y_{sp\;I/B} \approx 3.4477$}\par}\hbox{\strut \makebox[3cm][c]{$y_{sp\;O/B} \approx 7.6789$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$y_a \approx 13.7388$}\par }\hbox{\strut \makebox[3cm][c]{$y_{sp\;I/B} \approx 5.1201$}\par}\hbox{\strut \makebox[3cm][c]{$y_{sp\;O/B} \approx 9.0454$}\par}} \\
\hline
Relación $y_{a,sp}/b$ & \vtop{\hbox{\strut \makebox[3cm][c]{$y_a/b = 0.4046$}\par }\hbox{\strut \makebox[3cm][c]{$y_{sp\;I/B}/b = 0.1403$}\par}\hbox{\strut \makebox[3cm][c]{$y_{sp\;O/B}/b = 0.2651$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$y_a/b \approx 0.4326$}\par }\hbox{\strut \makebox[3cm][c]{$y_{sp\;I/B}/b \approx 0.1613$}\par}\hbox{\strut \makebox[3cm][c]{$y_{sp\;O/B}/b \approx 0.2903$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$y_a/b \approx 0.3539$}\par }\hbox{\strut \makebox[3cm][c]{$y_{sp\;I/B}/b \approx 0.1005$}\par}\hbox{\strut \makebox[3cm][c]{$y_{sp\;O/B}/b \approx 0.2237$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$y_a/b \approx 0.4273$}\par }\hbox{\strut \makebox[3cm][c]{$y_{sp\;I/B}/b \approx 0.1592$}\par}\hbox{\strut \makebox[3cm][c]{$y_{sp\;O/B}/b \approx 0.2813$}\par}} \\
\hline
Fracción de cuerda $c_{a,sp}/c$ & \vtop{\hbox{\strut \makebox[3cm][c]{$c_a/c = 0.2372$}\par }\hbox{\strut \makebox[3cm][c]{$c_{sp\;I/B}/c = 0.1478$}\par}\hbox{\strut \makebox[3cm][c]{$c_{sp\;O/B}/c = 0.1902$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$c_a/c \approx 0.3333$}\par }\hbox{\strut \makebox[3cm][c]{$c_{sp\;I/B}/c \approx 0.1579$}\par}\hbox{\strut \makebox[3cm][c]{$c_{sp\;O/B}/c \approx 0.25$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$c_a/c \approx 0.1892$}\par }\hbox{\strut \makebox[3cm][c]{$c_{sp\;I/B}/c \approx 0.1029$}\par}\hbox{\strut \makebox[3cm][c]{$c_{sp\;O/B}/c \approx 0.1739$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$c_a/c \approx 0.25$}\par }\hbox{\strut \makebox[3cm][c]{$c_{sp\;I/B}/c \approx 0.12$}\par}\hbox{\strut \makebox[3cm][c]{$c_{sp\;O/B}/c \approx 0.1714$}\par}} \\
\hline
Coeficiente de volumen\footnote{Para calcular el coeficiente de volumen, hemos tomado $c_{a,sp}$ como la cuerda del elemento en el punto medio de su semienvergadura.} $y_ab_ac_a/(S_wb)$ & \vtop{\hbox{\strut \makebox[3cm][c]{$\eta_a =$}\par}\hbox{\strut \makebox[3cm][c]{$ \num{9.7611e-3}$}\par}\hbox{\strut \makebox[3cm][c]{$\eta_{sp\;I/B} =$}\par}\hbox{\strut \makebox[3cm][c]{$\num{2.3028e-3}$}\par}\hbox{\strut \makebox[3cm][c]{$\eta_{sp\;O/B} =$}\par}\hbox{\strut \makebox[3cm][c]{$\num{1.3864e-2}$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$\eta_a \approx$}\par}\hbox{\strut \makebox[3cm][c]{$ \num{1.0407e-2}$}\par}\hbox{\strut \makebox[3cm][c]{$\eta_{sp\;I/B} \approx$}\par}\hbox{\strut \makebox[3cm][c]{$\num{2.3518e-3}$}\par}\hbox{\strut \makebox[3cm][c]{$\eta_{sp\;O/B} \approx$}\par}\hbox{\strut \makebox[3cm][c]{$\num{1.8504e-2}$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$\eta_a \approx$}\par }\hbox{\strut \makebox[3cm][c]{$\num{7.9043e-3}$}\par}\hbox{\strut \makebox[3cm][c]{$\eta_{sp\;I/B} \approx$}\par}\hbox{\strut \makebox[3cm][c]{$\num{1.7714e-3}$}\par}\hbox{\strut \makebox[3cm][c]{$\eta_{sp\;O/B} \approx$}\par}\hbox{\strut \makebox[3cm][c]{$\num{1.1573e-2}$}\par}} & \vtop{\hbox{\strut \makebox[3cm][c]{$\eta_a \approx$}\par }\hbox{\strut \makebox[3cm][c]{$\num{1.0972e-2}$}\par}\hbox{\strut \makebox[3cm][c]{$\eta_{sp\;I/B} \approx$}\par}\hbox{\strut \makebox[3cm][c]{$\num{ 2.7852e-3}$}\par}\hbox{\strut \makebox[3cm][c]{$\eta_{sp\;O/B} \approx$}\par}\hbox{\strut \makebox[3cm][c]{$\num{1.1516e-2}$}\par}} \\
\hline
\end{longtable}
\printbibliography
\end{document}
MWE 的 Bibfile.bib：
@book{JanesA220,
title = {Jane's All the World's Aircraft: Development \& Production},
author = {Paul Jackson},
year = {2016-2017},
publisher = {IHS Markit},
}
@book{JanesA319,
title = {Jane's All the World's Aircraft: Development \& Production},
author = {Paul Jackson},
year = {2007-2008},
publisher = {IHS Markit},
}
@book{JanesB737,
title = {Jane's All the World's Aircraft: Development \& Production},
author = {Paul Jackson},
year = {2012-2013},
publisher = {IHS Markit},
}
@Manual{A319APM,
title = {A319 Aircraft Characteristics: Airport and Maintenance Planning},
organization = {Airbus S.A.S. Customer Services, Technical Data Support and Services},
address = {31707, Blagnac Cedex, Francia},
year = {Revisión Diciembre 2020},
url = {https://www.airbus.com/aircraft/support-services/airport-operations-and-technical-data/aircraft-characteristics.html},
}
@Manual{B737APM,
title = {737 Airplane Characteristics for Airport Planning},
organization = {Boeing Commercial Airplanes},
address = {North Riverside, Chicago, IL 60606, USA},
year = {Revisión Septiembre 2020},
url = {https://www.boeing.com/commercial/airports/plan_manuals.page},
}
@Manual{A220APM,
title = {A220 Airport Planning Publication},
organization = {Airbus Canada Limited Partnership Customer Services},
address = {13100 Henri-Fabre Blvd., Mirabel, Quebec,
Canada},
year = {Revisión Junio 2020},
url = {A220World.airbus.com
},
}
@book{JanesCFM,
title = {Jane's Aero-Engines},
author = {Mark Daly \& Bill Gunston},
year = {2012-2013},
publisher = {IHS Markit},
}
@book{JanesP&W,
title = {Jane's Aero-Engines},
author = {Mark Daly},
year = {2016-2017},
publisher = {IHS Markit},
}
@techreport{A319TC,
type={\unskip\space},
title = {{Type Certificate Data Sheet No. EASA.A.064 for AIRBUS A318 – A319 – A320 – A321}},
year = {2021},
institution = {Agencia de la Unión Europea para la Seguridad Aérea},
}
@techreport{B737TC,
type={\unskip\space},
title = {Type Certificate Data Sheet No. EASA.IM.A.120
for BOEING 737},
year = {2021},
institution = {Agencia de la Unión Europea para la Seguridad Aérea},
}
@techreport{A220TC,
type={\unskip\space},
title = {Type Certificate Data Sheet No. EASA.IM.A.570 for BD-500 (A220 SERIES)},
year = {2021},
institution = {Agencia de la Unión Europea para la Seguridad Aérea},
}
@techreport{CFMTC,
type={\unskip\space},
title = {Type Certificate Data Sheet No. E.004
for CFM56-7B series engines},
year = {2019},
institution = {Agencia de la Unión Europea para la Seguridad Aérea},
}
@techreport{P&WTC,
type={\unskip\space},
title = {Type Certificate Data Sheet No. IM.E.090
for PW1500G Series Engines},
year = {2018},
institution = {Agencia de la Unión Europea para la Seguridad Aérea},
}
@book{Torenbeek,
title = {Synthesis of Subsonic Airplane Design},
author = {Egbert Torenbeek},
year = {1982},
publisher = {Delft University Press},
}
@misc{EurocontrolA319,
author = {Eurocontrol},
title = {{Aircraft Performance Database - A319-100}},
howpublished = "\url{https://contentzone.eurocontrol.int/aircraftperformance/details.aspx?ICAO=A319}",
}
@misc{EurocontrolB737,
author = {Eurocontrol},
title = {{Aircraft Performance Database - B737-700}},
howpublished = "\url{https://contentzone.eurocontrol.int/aircraftperformance/details.aspx?ICAO=B737}",
}
@misc{EurocontrolA220,
author = {Eurocontrol},
title = {{Aircraft Performance Database - A220-300}},
howpublished = "\url{https://contentzone.eurocontrol.int/aircraftperformance/details.aspx?ICAO=BCS3}",
}
@book{Roskam,
title = {Airplane Design. Part I: Preliminary Sizing of Airplanes},
author = {Jan Roskam},
year = {1985},
publisher = {Design, Analysis and Research Corporation (DARcorporation)},
}
@book{Roskam2,
title = {Airplane Design. Part II: Preliminary Sizing of Airplanes},
author = {Jan Roskam},
year = {1985},
publisher = {Design, Analysis and Research Corporation (DARcorporation)},
}
答案1
接下来的重新设计怎么样？
\documentclass[12pt, a4paper]{article}
\usepackage[a4paper, total={6in, 8in}]{geometry}
\usepackage{longtable}
\usepackage[per-mode=symbol]{siunitx}
\usepackage{booktabs}
\usepackage{threeparttablex}
\usepackage{geometry}
\begin{document}
\begin{ThreePartTable}
\begin{TableNotes}
\footnotesize
\item[1] Las definiciones son análogas a las dadas para dispositivos hipersustentadores.
\item[2] Al igual que con los slats, consideramos que los spoilers externos conforman un único dispositivo. De esta manera, empleamos los subíndices $sp\;I/B$ y $sp\;O/B$ para referirnos a los spoilers interno y externos, respectivamente.
\item[3] Para calcular el coeficiente de volumen, hemos tomado $c_{a,sp}$ como la cuerda del elemento en el punto medio de su semienvergadura.
\end{TableNotes}
\begin{longtable}{wr{3cm}*{4}{S[table-format=2.4]}}
\caption{Datos de los alerones y spoilers de aviones semejantes.}
\label{aler_spoil}\\
\toprule
\multicolumn{5}{c}{Alerones y Spoilers\tnote{1}} \\
\midrule
& {Proyecto} & {A319-100} & {B737-700} & {A220-300} \\
& & {\cite{A319APM,JanesA319,A319TC,EurocontrolA319}}
& {\cite{B737APM,JanesB737,B737TC,EurocontrolB737}}
& {\cite{A220APM,JanesA220,A220TC,EurocontrolA220}} \\
\midrule
\endfirsthead
\caption[]{Datos de los alerones y spoilers de aviones semejantes. -- continued from previous page}\\
\toprule
& {Proyecto} & {A319-100} & {B737-700} & {A220-300} \\
& & {\cite{A319APM,JanesA319,A319TC,EurocontrolA319}}
& {\cite{B737APM,JanesB737,B737TC,EurocontrolB737}}
& {\cite{A220APM,JanesA220,A220TC,EurocontrolA220}} \\
\midrule
\endhead
\insertTableNotes
\endlastfoot
\multicolumn{4}{@{}l}{Número de alerones por semiala} \\*
\addlinespace
I/B & {0} & {0} & {0} & {0} \\*
O/B & {1} & {1} & {1} & {1} \\
\midrule
\multicolumn{4}{@{}l}{Número de spoilers por semiala\tnote{2}}\\*
\addlinespace
I/B & {1} & {1} & {1} & {1} \\*
O/B & {4} & {4} & {5} & {4} \\
\midrule
\multicolumn{4}{@{}l}{Envergadura (m)} \\*
\addlinespace
$b_a$ & 5.9214 & 5.2692 & 5.9551 & 5.8881 \\*
$b_{sp\;I/B}$ & 3.1275 & 2.7943 & 4.7014 & 4.0107 \\*
$b_{sp\;O/B}$ & 11.2382 & 10.8577 & 10.3430 & 11.2641\\
\midrule
\multicolumn{4}{@{}l}{Relación $b_{a,sp}/b$} \\*
\addlinespace
$b_a/b$ & 0.1704 & 0.1545 & 0.1735 & 0.1831 \\*
$b_{sp\;I/B}/b$ & 0.0900 & 0.0082 & 0.1370 & 0.1247 \\*
$b_{sp\;O/B}/b$ & 0.3234 & 0.3184 & 0.3014 & 0.3503 \\
\midrule
\multicolumn{4}{@{}l}{Distancia al plano de simetría del avión $y_{a,sp}$ (m)}\\*
\addlinespace
$y_a$ & 14.0599 & 14.75 & 12.1452 & 13.7388 \\*
$y_{sp\;I/B}$ & 4.8754 & 5.5 & 3.4477 & 5.1201 \\*
$y_{sp\;O/B}$ & 9.2122 & 9.8997 & 7.6789 & 9.0454 \\
\midrule
\multicolumn{4}{@{}l}{Relación $y_{a,sp}/b$}\\*
\addlinespace
$y_a/b$ & 0.4046 & 0.4326 & 0.3539 & 0.4273 \\*
$y_{sp\;I/B}/b$ & 0.1403 & 0.1613 & 0.1005 & 0.1592 \\*
$y_{sp\;O/B}/b$ & 0.2651 & 0.2903 & 0.2237 & 0.2813 \\
\midrule
\multicolumn{4}{@{}l}{Fracción de cuerda $c_{a,sp}/c$ }\\*
\addlinespace
$c_a/c$ & 0.2372 & 0.3333 & 0.1892 & 0.25 \\*
$c_{sp\;I/B}/c$ & 0.1478 & 0.1579 & 0.1029 & 0.12 \\*
$c_{sp\;O/B}/c$ & 0.1902 & 0.25 & 0.1739 & 0.1714 \\
\midrule
\multicolumn{4}{@{}l}{Coeficiente de volumen\tnote{3}~ $y_ab_ac_a/(S_wb)$ }\\*
\addlinespace
$\eta_a$ & {\num{9.7611e-3}} & {\num{1.0407e-2}} & {\num{7.9043e-3}} & {\num{1.0972e-2}} \\*
$\eta_{sp\;I/B}$ & {\num{2.3028e-3}} & {\num{2.3518e-3}} & {\num{1.7714e-3}} & {\num{2.7852e-3}} \\*
$\eta_{sp\;O/B}$ & {\num{1.3864e-2}} & {\num{1.8504e-2}} & {\num{1.1573e-2}} & {\num{1.1516e-2}} \\
\bottomrule
\end{longtable}
\end{ThreePartTable}
\end{document}
答案2
- 你的表格太宽了，即使你使用字体大小，也无法适合纵向或横向的页面
\footnotesize - 一个可能的解决方案是局部增加文本区域大小，然后使用
landscape定向页面 - 作为起点，您可以考虑以下解决方案，即清理表格代码并使用以下方法更改文本区域大小
\newgeometry{hmargin=0.8in}：
\documentclass[12pt]{report}
\usepackage[total={6in, 8in}]{geometry}
\usepackage{amsmath}
\usepackage{tabularray}
\UseTblrLibrary{siunitx}
\usepackage{pdflscape}
\begin{document}
\newgeometry{hmargin=0.8in}
\begin{landscape}
\sisetup{tight-spacing,
exponent-product = \cdot
}
\begin{talltblr}[
caption = {Datos de los alerones y spoilers de aviones semejantes.},
label={aler_spoil},
note{1} = {Las definiciones son análogas a las dadas para dispositivos hipersustentadores.},
note{2} = {Al igual que con los slats, consideramos que los spoilers externos conforman un único dispositivo. De esta manera, empleamos los subíndices $sp\;I/B$ y $sp\;O/B$ para referirnos a los spoilers interno y externos, respectivamente.},
note{3} = {Para calcular el coeficiente de volumen, hemos tomado $c_{a,sp}$ como la cuerda del elemento en el punto medio de su semienvergadura.}
]{hlines, vlines,
colspec={X[1.1,l,h] *{4}{X[c,m]}},
columns = {font=\footnotesize\linespread{0.84}\selectfont},
row{1} ={font=\bfseries},
rowsep=3pt,
hspan =minimal
}
\SetCell[c=5]{c}
Alerones y Spoilers\TblrNote{1}
& & & \\
& Proyecto
& {A319-100\\ \cite{A319APM,JanesA319,A319TC,EurocontrolA319}}
& {B737-700\\ \cite{B737APM,JanesB737,B737TC,EurocontrolB737}}
& {A220-300\\ \cite{A220APM,JanesA220,A220TC,EurocontrolA220}} \\
Número de alerones por semiala
& I/B: 0 O/B: 1 & I/B: 0 O/B: 1 & I/B: 0 O/B: 1 & I/B: 0 O/B: 1 \\
Número de spoilers por semiala\TblrNote{2}
& I/B: 1 O/B: 4 & I/B: 1 O/B: 4 & I/B:1 O/B: 5 & I/B:1 O/B: 4 \\
Envergadura (m)
& $\begin{aligned}
b_a & = 5.9214\\
b_{sp\;I/B} & = 3.1275\\
sp\;O/B & = 11.2382
\end{aligned}$
& $\begin{aligned}
b_a & \approx 5.2692\\
b_{sp\;I/B} & \approx 2.7943\\
~ sp\;O/B & \approx 10.8577
\end{aligned}$
& $\begin{aligned}
b_a & \approx 5.8881\\
b_{sp\;I/B} & \approx 4.0107\\
sp\;O/B & \approx 11.2641
\end{aligned}$
& $\begin{aligned}
b_a & \approx 5.8881\\
b_{sp\;I/B} & \approx 4.0107\\
sp\;O/B & \approx 11.2641
\end{aligned}$ \\
Relación $b_{a,sp}/b$
& $\begin{aligned}
b_a/b & = 0.1704\\
b_{sp\;I/B}/b & = 0.0900\\
b_{sp\;O/B}/b & = 0.3234
\end{aligned}$
& $\begin{aligned}
b_a/b & \approx 0.1545\\
b_{sp\;I/B}/b & \approx 0.0082\\
b_{sp\;O/B}/b & \approx 0.3184
\end{aligned}$
& $\begin{aligned}
b_a/b & \approx 0.1735\\
b_{sp\;I/B}/b & \approx 0.1370\\
b_{sp\;O/B}/b & \approx 0.3014
\end{aligned}$
& $\begin{aligned}
b_a/b & \approx 0.1831\\
b_{sp\;I/B}/b & \approx 0.1247\\
b_{sp\;O/B}/b & \approx 0.3503
\end{aligned}$ \\
Distancia al plano de simetría del avión $y_{a,sp}$ (m)
& $\begin{aligned}
y_a & = 14.0599\\
y_{sp\;I/B} & = 4.8754\\
y_{sp\;O/B} & = 9.2122
\end{aligned}$
& $\begin{aligned}
y_a & \approx 14.75\\
y_{sp\;I/B} & \approx 5.5\\
y_{sp\;O/B} & \approx 9.8997
\end{aligned}$
& $\begin{aligned}
y_a & \approx 12.1452\\
y_{sp\;I/B} & \approx 3.4477\\
y_{sp\;O/B} & \approx 7.6789
\end{aligned}$
& $\begin{aligned}
y_a & \approx 13.7388\\
y_{sp\;I/B} & \approx 5.1201\\
y_{sp\;O/B} & \approx 9.0454
\end{aligned}$ \\
Relación $y_{a,sp}/b$
& $\begin{aligned}
y_a/b & = 0.4046\\
y_{sp\;I/B}/b & = 0.1403\\
y_{sp\;O/B}/b & = 0.2651
\end{aligned}$
& $\begin{aligned}
y_a/b & \approx 0.4326\\
y_{sp\;I/B}/b & \approx 0.1613\\
y_{sp\;O/B}/b & \approx 0.2903
\end{aligned}$
& $\begin{aligned}
y_a/b & \approx 0.3539\\
y_{sp\;I/B}/b & \approx 0.1005\\
y_{sp\;O/B}/b & \approx 0.2237
\end{aligned}$
& $\begin{aligned}
y_a/b & \approx 0.4273\\
y_{sp\;I/B}/b & \approx 0.1592\\
y_{sp\;O/B}/b & \approx 0.2813
\end{aligned}$ \\
Fracción de cuerda $c_{a,sp}/c$
& $\begin{aligned}
c_a/c & = 0.2372\\
c_{sp\;I/B}/c & = 0.1478\\
c_{sp\;O/B}/c & = 0.1902
\end{aligned}$
& $\begin{aligned}
c_a/c & \approx 0.3333\\
c_{sp\;I/B}/c & \approx 0.1579\\
c_{sp\;O/B}/c & \approx 0.25
\end{aligned}$
& $\begin{aligned}
c_a/c & \approx 0.1892\\
c_{sp\;I/B}/c & \approx 0.1029\\
c_{sp\;O/B}/c & \approx 0.173
\end{aligned}$
& $\begin{aligned}
c_a/c & \approx 0.25\\
c_{sp\;I/B}/c & \approx 0.12\\
c_{sp\;O/B}/c & \approx 0.1714
\end{aligned}$ \\
Coeficiente de volumen\TblrNote{3} $y_ab_ac_a/(S_wb)$
& $\begin{aligned}
\eta_a & = \num{9.7611e-3}\\
\eta_{sp\;I/B} & = \num{2.3028e-3}\\
\eta_{sp\;O/B} & = \num{1.3864e-2}
\end{aligned}$
& $\begin{aligned}
\eta_a & \approx \num{1.0407e-2}\\
\eta_{sp\;I/B} & \approx \num{2.3518e-3}\\
\eta_{sp\;O/B} & \approx \num{1.8504e-2}
\end{aligned}$
& $\begin{aligned}
\eta_a & \approx \num{7.9043e-3}\\
\eta_{sp\;I/B} & \approx \num{1.7714e-3}\\
\eta_{sp\;O/B} & \approx \num{1.1573e-2}
\end{aligned}$
& $\begin{aligned}
\eta_a & \approx \num{1.0972e-2}\\
\eta_{sp\;I/B} & \approx \num{ 2.7852e-3}\\
\eta_{sp\;O/B} & \approx \num{1.1516e-2}
\end{aligned}$ \\
\end{talltblr}
\end{landscape}
\restoregeometry
\end{document}
