docx

.gitignore

@@ -16,3 +16,4 @@ nafems4.pdf
 nafems4.docx
 nafems4.epub
 nafems4.nafems4.docx
+nafems4.odt

make.sh

@@ -124,6 +124,8 @@ for format in ${formats}; do
   elif [[ "${format}" == "html" ]]; then
     template_file="${template}.html"
     flags="${flags} --katex"
+  elif [[ "${format}" == "docx" ]]; then
+    flags="${flags} --reference-doc=CS-Book.docx"
   else
     template_file="${template}.${format}"
   fi

meta.yaml

@@ -12,7 +12,7 @@ colorlinks: true
 linkReferences: true
 nameInLink: true
 mathspec: true
-formats: html tex pdf epub
+formats: html tex pdf epub docx odt
 listings: true
 template: simple
 documentclass: article

nafems4.md

@@ -80,7 +80,7 @@ Mechanical systems can fail due to a wide variety of reasons. The effect known a
  1. stress life, or
  2. strain life
 
-The first one is suitable for cases where the loads are nowhere near the yield stress of the material. In those cases where plastic deformation is expected to occur, strain-life methods ought to be employed.
+The first one is suitable for cases where the loads are nowhere near the yield stress of the material. When plastic deformation is expected to occur, strain-life methods ought to be employed.
 
 For the case study, as the loads come principally from operational loads, the ASME\ stress-life approach should be used. The stress amplitude of a periodic cycle can be related to the number of cycles where failure by fatigue is expected to occur. For each material, this dependence can be computed using normalised tests and a family of “fatigue curves” like the one depicted in\ [@fig:SN] (also called $S$-$N$ curve) for different temperatures can be obtained.