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Longtable을 만드는 중에 문제가 발생했습니다. ! 잘못 배치된 \noalign 오류

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Longtable을 만드는 중에 문제가 발생했습니다. ! 잘못 배치된 \noalign 오류

Longtable 패키지를 사용할 때 문제가 발생합니다. 이미 여러 게시물에서 3시간 정도 검색했지만 아무 효과가 없었습니다. 나는 테이블을 업로드합니다.

\usepackage{longtable,lscape}
\usepackage{multirow,multicol}
\begin{center}
\fontsize{9}{10}\selectfont
\begin{longtable}{|c|c|X|X|X|}%[H]

\caption{3D printing materials}\label{tabla:Materials}

\hline

\textbf{Printing Technology} & \textbf{Material} & \multicolumn{2}{c|}
{\textbf{Material properties}} & \textbf{3D printing problems} \\ \hline
\multirow{21}{*}{FDM\footnote{All data is against XZ axis.}} 

& \multirow{7}{*}{PC-ABS\footnote{All data obtained from 
\cite{materials:pcabs_stratasys}}} & Tensile Modulus & 1810MPa & \multirow{21}
{*}{blablabla} \\ \cline{3-4}
& & Tensile Strength & 34MPa &  \\ \cline{3-4}
& & Elongation to Break & 5\% &  \\ \cline{3-4}
& & Flexural Modulus & 1740MPa & \\ \cline{3-4}
& & Flexural Strength & 59MPa & \\ \cline{3-4}
& & Melting Point & N/A\footnote{Due to amorphous nature, material does not 
display a melting point.} & \\ \cline{3-4}
& & Dielectric Constant\footnote{Also known as Relative Permittivity.} & 2.78 
- 2.83 &  \\ 
\cline{2-4}
&\multirow{7}{*}{ABS\footnote{All data obtained from \cite{materials:abs_stratasys}}} & Tensile Modulus & 2230MPa & \\ \cline{3-4}
& & Tensile Strength & 32MPa &  \\ \cline{3-4}
& & Elongation to Break & 7\% &  \\ \cline{3-4}
& & Flexural Modulus & 2060MPa & \\ \cline{3-4}
& & Flexural Strength & 60MPa & \\ \cline{3-4}
& & Melting Point & N/A & \\ \cline{3-4}
& & Dielectric Constant & 2.6 - 2.86 & \\ \cline{2-4}

& \multirow{7}{*}{Nylon 12\footnote{All data obtained from \cite{materials:nylon_stratasys}}} & Tensile Modulus & 1282MPa &  \\ \cline{3-4}
& & Tensile Strength & 46MPa &  \\ \cline{3-4}
& & Elongation to Break & 30\% &  \\ \cline{3-4}
& & Flexural Modulus & 1276 &  \\ \cline{3-4}
& & Flexural Strength & 67MPa &  \\ \cline{3-4}
& & Melting Point & 178$^{\circ}$C &  \\ \cline{3-4}
& & Dielectric Constant & N/A &  \\ \cline{2-4}
\hline 

\multirow{14}{*}{SLA\footnote{All data obtained from 
\cite{materials:3dsystems_materials}}} & 

\multirow{7}{*}{VisiJet\textregistered\ Black} & Tensile Modulus & 2150MPa & 
\multirow{14}{*}{blablabla} \\ \cline{3-4}
& & Tensile Strength & 45MPa &  \\ \cline{3-4}
& & Elongation to Break & 5\% & \\ \cline{3-4}
& & Flexural Modulus & 2350 & \\ \cline{3-4}
& & Flexural Strength & 76Pa & \\ \cline{3-4}
& & Melting Point & N/A & \\ \cline{3-4}
& & Dielectric Constant & N/A & \\ \cline{2-4}

\multirow{7}{*}{VisiJet\textregistered\ Tough} & Tensile Modulus & 1890MPa & \\ \cline{3-4}
& & Tensile Strength & 41MPa & \\ \cline{3-4}
& & Elongation to Break & 18\% & \\ \cline{3-4}
& & Flexural Modulus & 1850 & \\ \cline{3-4}
& & Flexural Strength & 62MPa & \\ \cline{3-4}
& & Melting Point & NA & \\ \cline{3-4}
& & Dielectric Constant & N/A & \\ \cline{2-4}
\hline  

\multirow{14}{*}{SLS} & 
\multirow{7}{*}{Alumide\textregistered \footnote{All data obtained from \cite{materials:shapeways_alumide}}} & Tensile Modulus & 3800MPa & \multirow{14}{*}{blablabla} \\ \cline{3-4}
& & Tensile Strength & 48MPa &  \\ \cline{3-4}
& & Elongation to Break & 4\% &  \\ \cline{3-4}
& & Flexural Modulus & 3600 & \\ \cline{3-4}
& & Flexural Strength & 72MPa & \\ \cline{3-4}
& & Melting Point & 172-180$^{\circ}$C & \\ \cline{3-4}
& & Dielectric Constant & 13 ${\pm}$ 1.5 &  \\ \cline{2-4}


& \multirow{7}{*}{Nylon (PA2200) \footnote{All data obtained from \cite{materials:shapeways_pa2200}}} & Tensile Modulus & 1700MPa &  \\ \cline{3-4}
& & Tensile Strength & 48MPa &  \\ \cline{3-4} 
& & Elongation to Break & 24\% &  \\ \cline{3-4}
& & Flexural Modulus & 1500 &  \\ \cline{3-4}
& & Flexural Strength & 58MPa &  \\ \cline{3-4}
& & Melting Point & 172-180$^{\circ}$C &  \\ \cline{3-4}
& & Dielectric Constant & NA &  \\ \cline{2-4}
\hline 

%\end{tabularx}

\end{longtable}
\normalsize
\end{center}

도움을 주시면 정말 감사하겠습니다

답변1

유감스럽게도 귀하의 코드에는 여러 가지 심각한 오류가 있으며 이로 인해 컴파일이 중단될 수 있습니다. 다음에서는 실제로 충돌을 일으키는 원인을 내가 인식한 부분을 수정하려고 노력했습니다. 당연히 내용을 판단할 수 있는 입장은 아닙니다.

이전 코드와 새 코드를 비교하여 내가 변경한 모든 내용을 확인하세요. 가장 중요한 것 중에는 다음과 같은 것이 있습니다.

  • 수정된 코드 에서는 table및 tabular환경 대신 longtable및 tabularx환경을 사용합니다. (여담: 환경 tabularx안에 환경을 넣을 수는 없습니다 longtable.)

  • 명령문 안에 명령 \footnote이 있으면 제대로 작동하지 않습니다 \multirow. 따라서 패키지를 로드 threeparttable하고 지침을 및 지침 \footnote쌍으로 분할했습니다. 별도로, 수직 공간이 중요하기 때문에 여러 개의 짧은 각주를 한 줄에 조판할 수 있도록 옵션을 패키지에 로드했습니다.\tnote\itemthreeparttablepara

  • \cline{2.4}오버레이 및 지침을 사용하지 마십시오 \hline.

여기에 이미지 설명을 입력하세요

\documentclass[10pt]{article}
\usepackage{multirow,array}
\setlength\extrarowheight{1pt}
% set page parameters:
\usepackage[letterpaper,margin=1in]{geometry} 
\usepackage[skip=0.333\baselineskip]{caption}
\usepackage[para,flushleft]{threeparttable}
\begin{document}

\begin{table}
\centering
\begin{threeparttable}
\fontsize{9}{10}\selectfont
\caption{3D printing materials}\label{tabla:Materials}
\begin{tabular}{|>{\centering}p{2.25cm}| c| *{2}{l|}
                 >{\centering\arraybackslash}p{2.25cm}| }
\hline
\textbf{Printing Technology} &
\textbf{Material} &
\multicolumn{2}{c|}{\textbf{Material properties}} & 
\textbf{3D printing problems} \\
\hline

\multirow{21}{*}{FDM\tnote{1}}
& \multirow{7}{*}{PC-ABS\tnote{2}}
  & Tensile Modulus & 1810MPa & 
  \multirow{21}{*}{blablabla} \\ \cline{3-4}
& & Tensile Strength & 34MPa &  \\ \cline{3-4}
& & Elongation to Break & 5\% &  \\ \cline{3-4}
& & Flexural Modulus & 1740MPa & \\ \cline{3-4}
& & Flexural Strength & 59MPa & \\ \cline{3-4}
& & Melting Point & N/A\tnote{3} & \\ \cline{3-4}
& & Dielectric Constant\tnote{4} & 2.78--2.83 &  \\
\cline{2-4}

&\multirow{7}{*}{ABS\tnote{5}} 
  & Tensile Modulus & 2230MPa & \\ \cline{3-4}
& & Tensile Strength & 32MPa &  \\ \cline{3-4}
& & Elongation to Break & 7\% &  \\ \cline{3-4}
& & Flexural Modulus & 2060MPa & \\ \cline{3-4}
& & Flexural Strength & 60MPa & \\ \cline{3-4}
& & Melting Point & N/A & \\ \cline{3-4}
& & Dielectric Constant & 2.6--2.86 & \\ 
\cline{2-4}

& \multirow{7}{*}{Nylon 12\tnote{6}} 
  & Tensile Modulus & 1282MPa &  \\ \cline{3-4}
& & Tensile Strength & 46MPa &  \\ \cline{3-4}
& & Elongation to Break & 30\% &  \\ \cline{3-4}
& & Flexural Modulus & 1276 &  \\ \cline{3-4}
& & Flexural Strength & 67MPa &  \\ \cline{3-4}
& & Melting Point & 178$^{\circ}$C &  \\ \cline{3-4}
& & Dielectric Constant & N/A &  \\ 
%%%\cline{2-4}
\hline

\multirow{14}{*}{SLA\tnote{7}} 
& \multirow{7}{*}{VisiJet\textsuperscript{\textregistered} Black} 
  & Tensile Modulus & 2150MPa &
  \multirow{14}{*}{blablabla} \\ \cline{3-4}
& & Tensile Strength & 45MPa &  \\ \cline{3-4}
& & Elongation to Break & 5\% & \\ \cline{3-4}
& & Flexural Modulus & 2350 & \\ \cline{3-4}
& & Flexural Strength & 76Pa & \\ \cline{3-4}
& & Melting Point & N/A & \\ \cline{3-4}
& & Dielectric Constant & N/A & \\ 
\cline{2-4}

& \multirow{7}{*}{VisiJet\textsuperscript{\textregistered} Tough}
  & Tensile Modulus & 1890MPa & \\ \cline{3-4}
& & Tensile Strength & 41MPa & \\ \cline{3-4}
& & Elongation to Break & 18\% & \\ \cline{3-4}
& & Flexural Modulus & 1850 & \\ \cline{3-4}
& & Flexural Strength & 62MPa & \\ \cline{3-4}
& & Melting Point & NA & \\ \cline{3-4}
& & Dielectric Constant & N/A & \\ 
%%%\cline{2-4}
\hline

\multirow{14}{*}{SLS} 
& \multirow{7}{*}{Alumide\textsuperscript{\textregistered} \tnote{8}} 
  & Tensile Modulus & 3800MPa & 
  \multirow{14}{*}{blablabla} \\ \cline{3-4}
& & Tensile Strength & 48MPa &  \\ \cline{3-4}
& & Elongation to Break & 4\% &  \\ \cline{3-4}
& & Flexural Modulus & 3600 & \\ \cline{3-4}
& & Flexural Strength & 72MPa & \\ \cline{3-4}
& & Melting Point & 172--180$^{\circ}$C & \\ \cline{3-4}
& & Dielectric Constant & $13 \pm 1.5$ &  \\ 
\cline{2-4}

& \multirow{7}{*}{Nylon (PA2200) \tnote{9}} 
  & Tensile Modulus & 1700MPa &  \\ \cline{3-4}
& & Tensile Strength & 48MPa &  \\ \cline{3-4}
& & Elongation to Break & 24\% &  \\ \cline{3-4}
& & Flexural Modulus & 1500 &  \\ \cline{3-4}
& & Flexural Strength & 58MPa &  \\ \cline{3-4}
& & Melting Point & 172--180$^{\circ}$C &  \\ \cline{3-4}
& & Dielectric Constant & NA &  \\ 
%%%\cline{2-4}
\hline
\end{tabular}

\begin{tablenotes}
\raggedright\footnotesize
\item[1] All data is against XZ axis.
\item[2] All data obtained from \cite{materials:pcabs_stratasys}
\item[3] Due to amorphous nature, material does not display a melting point.
\item[4] Also known as Relative Permittivity.
\item[5] All data obtained from \cite{materials:abs_stratasys}
\item[6] All data obtained from \cite{materials:nylon_stratasys}
\item[7] All data obtained from \cite{materials:3dsystems_materials}
\item[8] All data obtained from \cite{materials:shapeways_alumide}
\item[9] All data obtained from \cite{materials:shapeways_pa2200}
\end{tablenotes}
\end{threeparttable}
\end{table}

\end{document}

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