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% Most of the following are not required for the majority
% of cheat sheets but are needed for some symbol support.
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% Document Info
\author{Tito (tito.vinicius)}
\pdfinfo{
  /Title (fatigue-crack.pdf)
  /Creator (Cheatography)
  /Author (Tito (tito.vinicius))
  /Subject (Fatigue Crack Cheat Sheet)
}

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\noindent
\begin{multicols}{3}
\begin{tabulary}{5.8cm}{C}
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    \vspace{-7pt}
    {\parbox{\dimexpr\textwidth-2\fboxsep\relax}{\noindent
        \hspace*{-6pt}\includegraphics[width=5.8cm]{/web/www.cheatography.com/public/images/cheatography_logo.pdf}}
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\columnbreak
\begin{tabulary}{11cm}{L}
    \vspace{-2pt}\large{\bf{\textcolor{DarkBackground}{\textrm{Fatigue Crack Cheat Sheet}}}} \\
    \normalsize{by \textcolor{DarkBackground}{Tito (tito.vinicius)} via \textcolor{DarkBackground}{\uline{cheatography.com/147214/cs/32094/}}}
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\noindent
\begin{multicols}{3}
\begin{tabulary}{5.8cm}{LL}
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  \mymulticolumn{2}{p{5.377cm}}{\bf\textcolor{white}{Cheatographer}}  \\
  \vspace{-2pt}Tito (tito.vinicius) \\
  \uline{cheatography.com/tito-vinicius} \\
  \end{tabulary}
\vfill
\columnbreak
\begin{tabulary}{5.8cm}{L}
  \SetRowColor{FootBackground}
  \mymulticolumn{1}{p{5.377cm}}{\bf\textcolor{white}{Cheat Sheet}}  \\
   \vspace{-2pt}Not Yet Published.\\
   Updated 12th May, 2022.\\
   Page {\thepage} of \pageref{LastPage}.
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\vfill
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  \mymulticolumn{1}{p{5.377cm}}{\bf\textcolor{white}{Sponsor}}  \\
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  \vspace{-5pt}
  %\includegraphics[width=48px,height=48px]{dave.jpeg}
  Measure your website readability!\\
  www.readability-score.com
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\begin{document}
\raggedright
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% www.emerson.emory.edu/services/latex/latex_169.html
\footnotesize % Small font.


\begin{tabularx}{17.67cm}{X}
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\mymulticolumn{1}{x{17.67cm}}{\bf\textcolor{white}{Summary}}  \tn
\SetRowColor{white}
\mymulticolumn{1}{x{17.67cm}}{\{\{ac\}\}The potential for fatigue cracks to occur in pipeline structures due to cycling  \newline % Row Count 2 (+ 2)
loads inherent of offshore oil production, makes necessary have an inspection tool to  \newline % Row Count 4 (+ 2)
carry out periodic non destructive inspection in the inner pipe surface. The most critical  \newline % Row Count 6 (+ 2)
point of pipeline structures is the circumferential weld and demands special attention  \newline % Row Count 8 (+ 2)
during inspection. The results achieved demonstrate the feasibility to apply eddy current  \newline % Row Count 10 (+ 2)
technology to detect fatigue cracks in welded joints of clad pipes.% Row Count 12 (+ 2)
} \tn 
\hhline{>{\arrayrulecolor{DarkBackground}}-}
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\par\addvspace{1.3em}

\begin{tabularx}{17.67cm}{x{4.7236 cm} x{4.3862 cm} x{7.7602 cm} }
\SetRowColor{DarkBackground}
\mymulticolumn{3}{x{17.67cm}}{\bf\textcolor{white}{Literature Review}}  \tn
% Row 0
\SetRowColor{LightBackground}
{\bf{Yusa  et. al. {[}28{]}}} & {\bf{Purpose}} & Application of the eddy current technique for detection of fatigue cracks \tn 
% Row Count 5 (+ 5)
% Row 1
\SetRowColor{white}
 & {\bf{Material}} & Nickel 600 (Incoloy Alloy) plate \tn 
% Row Count 7 (+ 2)
% Row 2
\SetRowColor{LightBackground}
 & {\bf{Artificial Defects}} & The cracks were fabricated on a three-point support fatigue machine. \tn 
% Row Count 11 (+ 4)
% Row 3
\SetRowColor{white}
 & {\bf{Image}} & \{\{link="https://1drv.ms/u/s!AsxrgPK91ExWhcguVs0muqeaTQCcwA"\}\}Crack image\{\{/link\}\} \tn 
% Row Count 16 (+ 5)
% Row 4
\SetRowColor{LightBackground}
{\bf{Huang et.al. {[}30{]}}} & {\bf{Purpose}} & In addition to detection, the sizing of cracks of fatigue \tn 
% Row Count 20 (+ 4)
% Row 5
\SetRowColor{white}
 & {\bf{Material}} & 316 Stainless Steel plate \tn 
% Row Count 22 (+ 2)
% Row 6
\SetRowColor{LightBackground}
 & {\bf{Artificial Defects}} & The cracks were fabricated on a four-point support fatigue machine. \tn 
% Row Count 26 (+ 4)
% Row 7
\SetRowColor{white}
 & {\bf{Image}} & \{\{link="https://1drv.ms/u/s!AsxrgPK91ExWhcgv0FSkAtVyAAS1Gw"\}\}Crack image\{\{/link\}\} \tn 
% Row Count 31 (+ 5)
\end{tabularx}
\par\addvspace{1.3em}

\begin{tabularx}{17.67cm}{x{4.7236 cm} x{4.3862 cm} x{7.7602 cm} }
\SetRowColor{DarkBackground}
\mymulticolumn{3}{x{17.67cm}}{\bf\textcolor{white}{Literature Review (cont)}}  \tn
% Row 8
\SetRowColor{LightBackground}
{\bf{Nakagawa et.al. {[}31{]}}} & {\bf{Purpose}} & In addition to the detection reliability of the eddy current technique, the effects of using EDM notches to represent fatigue cracks. \tn 
% Row Count 8 (+ 8)
% Row 9
\SetRowColor{white}
 & {\bf{Material}} & Titanium Alloy (Ti-6246) e Nickel (IN-100) \tn 
% Row Count 11 (+ 3)
% Row 10
\SetRowColor{LightBackground}
 & {\bf{Artificial Defects}} & Electrical Erosion notches \tn 
% Row Count 14 (+ 3)
% Row 11
\SetRowColor{white}
 & {\bf{Image}} & \{\{link="https://1drv.ms/u/s!AsxrgPK91ExWhcgtZUNk5SKrQhSEMg"\}\}Electrical Erosion crack\{\{/link\}\} \tn 
% Row Count 20 (+ 6)
% Row 12
\SetRowColor{LightBackground}
 & {\bf{Image}} & \{\{link="https://1drv.ms/u/s!AsxrgPK91ExWhcgwDDAiyoyVEvoyaw."\}\}Extrapolation of results\{\{/link\}\} \tn 
% Row Count 26 (+ 6)
% Row 13
\SetRowColor{white}
 & {\bf{Final results}} & From the results achieved with the fabricated notches, a linear function was fitted to the data, extrapolating them to opening values that the authors named "zero" opening. \tn 
% Row Count 36 (+ 10)
\end{tabularx}
\par\addvspace{1.3em}

\begin{tabularx}{17.67cm}{x{4.7236 cm} x{4.3862 cm} x{7.7602 cm} }
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\mymulticolumn{3}{x{17.67cm}}{\bf\textcolor{white}{Literature Review (cont)}}  \tn
% Row 14
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{\bf{Larson et.al. {[}32{]}}} & {\bf{Purpose}} & Similar Nakagawa et.al. {[}31{]} \tn 
% Row Count 2 (+ 2)
% Row 15
\SetRowColor{white}
 & {\bf{Material}} & Titanium Alloy and aluminium \tn 
% Row Count 4 (+ 2)
% Row 16
\SetRowColor{LightBackground}
 & {\bf{Artificial Defects}} & The notches studied in the work were superficial and shallow, with depth ranging between 25.4 µm and 0.4 mm, and openings ranging from 30 µm and 0.12 mm, and the interaction between the opening and the depth of the defects was mainly analyzed. \tn 
% Row Count 18 (+ 14)
% Row 17
\SetRowColor{white}
 & {\bf{Image}} & \{\{link="https://1drv.ms/u/s!AsxrgPK91ExWhcgxCZIOUu56VCfU0w"\}\}Extrapolation of results\{\{/link\}\} \tn 
% Row Count 24 (+ 6)
% Row 18
\SetRowColor{LightBackground}
 & {\bf{Final results}} & The results achieved by the author indicated that the amplitude attenuation factor, so that signals from EDM notches are representative for fatigue cracks, is between 10 and 30\%. \tn 
% Row Count 34 (+ 10)
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\mymulticolumn{2}{x{17.67cm}}{\bf\textcolor{white}{Difficulties to be considered in Crack detection}}  \tn
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\end{document}