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1 | | -\documentclass{article} |
2 | | -\usepackage[table]{xcolor} |
| 1 | + |
| 2 | +\documentclass[border=20pt]{standalone} |
| 3 | +\usepackage{blindtext}% |
| 4 | +\usepackage{subcaption} |
| 5 | +\usepackage{url} |
3 | 6 | \usepackage{graphicx} |
| 7 | +\usepackage{caption} |
| 8 | +\usepackage{multirow} |
4 | 9 | \usepackage{booktabs} |
5 | | -\usepackage{multirow} |
6 | | -\usepackage[accsupp]{axessibility} |
7 | | -\usepackage{CJKutf8} |
8 | | -\usepackage{orcidlink} |
| 10 | +\usepackage{color} |
| 11 | +\usepackage{colortbl} |
| 12 | +\usepackage{xcolor,soul,framed} |
| 13 | +\usepackage{xeCJK} |
| 14 | +%\usepackage{fontspec} |
| 15 | +%\usepackage[margin=1in]{geometry} |
| 16 | +\usepackage{printlen} |
| 17 | +\usepackage{amsmath,amssymb,mathtools,bm,mathrsfs,textcomp} |
| 18 | +\setlength{\parindent}{0pt} |
9 | 19 |
|
10 | 20 | \begin{document} |
11 | | -\begin{CJK}{UTF8}{gbsn} |
12 | | - |
13 | | -% Put your latex code here. |
14 | 21 |
|
15 | 22 | \begin{tabular}{|c|c|c|c|} |
16 | | -\hline |
17 | | -Quantity $\backslash$ Unit System & International System SI (kg-m-s) & Traditional aeronautical (lb-ft-s) & Traditional structural (lb-inch-s) \\ |
18 | | -\hline |
19 | | -Mass (translational inertia), $m$ & kilogram mass (kg) & slug = lb-s$^2$/f & lb-s$^2$/inch \\ |
20 | | -\hline |
21 | | -Length, translational motion & meter (m) & foot (ft) & inch (in.) \\ |
22 | | -\hline |
23 | | -Time, $t$ & second (s) & second (s) & second (s) \\ |
24 | | -\hline |
25 | | -Force, translational action & newton (N) = kg-m/s$^2$ & pound force (lb) & pound force (lb) \\ |
26 | | -\hline |
27 | | -Translational stiffness constant, $k$ & N/m & lb/ft & lb/inch \\ |
28 | | -\hline |
29 | | -Translational damping constant, $c$ & N/(m/s) = N-s/m & lb/(ft/s) = lb-s/ft & lb/(inch/s) = lb-s/inch \\ |
30 | | -\hline |
31 | | -Angle, rotational motion & radial (rad), which is dimensionless & radial (rad), which is dimensionless & radial (rad), which is dimensionless \\ |
32 | | -\hline |
33 | | -Rotational inertia, $J$ & kg-m$^2$ & slug-ft$^2$ = lb-s$^2$ - ft & lb-s$^2$ - inch \\ |
34 | | -\hline |
35 | | -Moment or torque, rotational action & N-m & lb-ft & lb-inch \\ |
36 | | -\hline |
37 | | -Rotational stiffness constant, $k_\theta$ & (N-m)/rad = N-m & (lb-ft)/rad = lb-ft & (lb-inch)/rad = lb-inch \\ |
38 | | -\hline |
39 | | -Rotational damping constant, $c_\theta$ & (N-m)/(rad/s) = N-m-s & (lb-ft)/(rad/s) = lb-ft-s & (lb-inch)/(rad/s) = lb-inch-s \\ |
40 | | -\hline |
| 23 | + \hline |
| 24 | + Quantity $\backslash$ Unit System & International System SI (kg-m-s) & Traditional aeronautical (lb-ft-s) & Traditional structural (lb-inch-s) \\ |
| 25 | + \hline |
| 26 | + Mass (translational inertia), $m$ & kilogram mass (kg) & slug = lb-s$^2$/f & lb-s$^2$/inch \\ |
| 27 | + \hline |
| 28 | + Length, translational motion & meter (m) & foot (ft) & inch (in.) \\ |
| 29 | + \hline |
| 30 | + Time, $t$ & second (s) & second (s) & second (s) \\ |
| 31 | + \hline |
| 32 | + Force, translational action & newton (N) = kg-m/s$^2$ & pound force (lb) & pound force (lb) \\ |
| 33 | + \hline |
| 34 | + Translational stiffness constant, $k$ & N/m & lb/ft & lb/inch \\ |
| 35 | + \hline |
| 36 | + Translational damping constant, $c$ & N/(m/s) = N-s/m & lb/(ft/s) = lb-s/ft & lb/(inch/s) = lb-s/inch \\ |
| 37 | + \hline |
| 38 | + Angle, rotational motion & radial (rad), which is dimensionless & radial (rad), which is dimensionless & radial (rad), which is dimensionless \\ |
| 39 | + \hline |
| 40 | + Rotational inertia, $J$ & kg-m$^2$ & slug-ft$^2$ = lb-s$^2$ - ft & lb-s$^2$ - inch \\ |
| 41 | + \hline |
| 42 | + Moment or torque, rotational action & N-m & lb-ft & lb-inch \\ |
| 43 | + \hline |
| 44 | + Rotational stiffness constant, $k_\theta$ & (N-m)/rad = N-m & (lb-ft)/rad = lb-ft & (lb-inch)/rad = lb-inch \\ |
| 45 | + \hline |
| 46 | + Rotational damping constant, $c_\theta$ & (N-m)/(rad/s) = N-m-s & (lb-ft)/(rad/s) = lb-ft-s & (lb-inch)/(rad/s) = lb-inch-s \\ |
| 47 | + \hline |
41 | 48 | \end{tabular} |
42 | 49 |
|
43 | | -\end{CJK} |
44 | | -\end{document} |
45 | | - |
| 50 | +\end{document} |
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