<?xml version="1.0" encoding="UTF-8"?>
<collection xmlns="http://www.loc.gov/MARC21/slim">
 <record>
  <leader>     caa a22        4500</leader>
  <controlfield tag="001">388067810</controlfield>
  <controlfield tag="003">CHVBK</controlfield>
  <controlfield tag="005">20180307125138.0</controlfield>
  <controlfield tag="007">cr unu---uuuuu</controlfield>
  <controlfield tag="008">161130e199909  xx      s     000 0 eng  </controlfield>
  <datafield tag="024" ind1="7" ind2="0">
   <subfield code="a">10.1017/S1727719100000411</subfield>
   <subfield code="2">doi</subfield>
  </datafield>
  <datafield tag="024" ind1="7" ind2="0">
   <subfield code="a">S1727719100000411</subfield>
   <subfield code="2">pii</subfield>
  </datafield>
  <datafield tag="035" ind1=" " ind2=" ">
   <subfield code="a">(NATIONALLICENCE)cambridge-10.1017/S1727719100000411</subfield>
  </datafield>
  <datafield tag="245" ind1="0" ind2="0">
   <subfield code="a">Evaluation of Interlaminar Shear Stress by Strain Measurements on Laminate Surfaces</subfield>
   <subfield code="h">[Elektronische Daten]</subfield>
  </datafield>
  <datafield tag="520" ind1="3" ind2=" ">
   <subfield code="a">For most composite structures, because of the uncertainty in some design variables, it is not possible to predict precisely the stresses during design stage. Therefore, monitoring the structural responses in service becomes crucial for structure with concerns, e.g., the composite panels on an airplane, etc. In this study, the strains at neighboring points of the interested location on surfaces of the laminate, along with the classical laminate theory and the higher-order shear deformation theory, are used to predict the interlaminar shear stresses in the cross-ply laminate. Several numerical examples using the simulated surface strains are employed to evaluate the accuracy of the proposed technique. It is found that the approach using the higher-order shear deformation theory has improved accuracy for the analysis of thick symmetric laminate over the approach using the classical laminate theory.</subfield>
  </datafield>
  <datafield tag="540" ind1=" " ind2=" ">
   <subfield code="a">Copyright © The Society of Theoretical and Applied Mechanics, R.O.C. 1999</subfield>
  </datafield>
  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">Interlaminar shear stress</subfield>
   <subfield code="2">nationallicence</subfield>
  </datafield>
  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">Strain measurement</subfield>
   <subfield code="2">nationallicence</subfield>
  </datafield>
  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">Composite laminate</subfield>
   <subfield code="2">nationallicence</subfield>
  </datafield>
  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">Lamination theory</subfield>
   <subfield code="2">nationallicence</subfield>
  </datafield>
  <datafield tag="700" ind1="1" ind2=" ">
   <subfield code="a">Lee</subfield>
   <subfield code="D">C.Y.</subfield>
   <subfield code="u">Department of Mechanical Engineering, Da-Yeh University, Da-Tsuen, Chang-Hwa, Taiwan 515, R.O.C.</subfield>
  </datafield>
  <datafield tag="700" ind1="1" ind2=" ">
   <subfield code="a">Huang</subfield>
   <subfield code="D">C.C.</subfield>
   <subfield code="u">Department of Mechanical Engineering, Da-Yeh University, Da-Tsuen, Chang-Hwa, Taiwan 515, R.O.C.</subfield>
  </datafield>
  <datafield tag="773" ind1="0" ind2=" ">
   <subfield code="t">Journal of Mechanics</subfield>
   <subfield code="d">Cambridge University Press</subfield>
   <subfield code="g">15/3(1999-09), 127-135</subfield>
   <subfield code="x">1727-7191</subfield>
   <subfield code="q">15:3&lt;127</subfield>
   <subfield code="1">1999</subfield>
   <subfield code="2">15</subfield>
   <subfield code="o">JOM</subfield>
  </datafield>
  <datafield tag="856" ind1="4" ind2="0">
   <subfield code="u">https://doi.org/10.1017/S1727719100000411</subfield>
   <subfield code="q">text/html</subfield>
   <subfield code="z">Onlinezugriff via DOI</subfield>
  </datafield>
  <datafield tag="908" ind1=" " ind2=" ">
   <subfield code="D">1</subfield>
   <subfield code="a">research-article</subfield>
   <subfield code="2">jats</subfield>
  </datafield>
  <datafield tag="950" ind1=" " ind2=" ">
   <subfield code="B">NATIONALLICENCE</subfield>
   <subfield code="P">856</subfield>
   <subfield code="E">40</subfield>
   <subfield code="u">https://doi.org/10.1017/S1727719100000411</subfield>
   <subfield code="q">text/html</subfield>
   <subfield code="z">Onlinezugriff via DOI</subfield>
  </datafield>
  <datafield tag="950" ind1=" " ind2=" ">
   <subfield code="B">NATIONALLICENCE</subfield>
   <subfield code="P">700</subfield>
   <subfield code="E">1-</subfield>
   <subfield code="a">Lee</subfield>
   <subfield code="D">C.Y.</subfield>
   <subfield code="u">Department of Mechanical Engineering, Da-Yeh University, Da-Tsuen, Chang-Hwa, Taiwan 515, R.O.C</subfield>
  </datafield>
  <datafield tag="950" ind1=" " ind2=" ">
   <subfield code="B">NATIONALLICENCE</subfield>
   <subfield code="P">700</subfield>
   <subfield code="E">1-</subfield>
   <subfield code="a">Huang</subfield>
   <subfield code="D">C.C.</subfield>
   <subfield code="u">Department of Mechanical Engineering, Da-Yeh University, Da-Tsuen, Chang-Hwa, Taiwan 515, R.O.C</subfield>
  </datafield>
  <datafield tag="950" ind1=" " ind2=" ">
   <subfield code="B">NATIONALLICENCE</subfield>
   <subfield code="P">773</subfield>
   <subfield code="E">0-</subfield>
   <subfield code="t">Journal of Mechanics</subfield>
   <subfield code="d">Cambridge University Press</subfield>
   <subfield code="g">15/3(1999-09), 127-135</subfield>
   <subfield code="x">1727-7191</subfield>
   <subfield code="q">15:3&lt;127</subfield>
   <subfield code="1">1999</subfield>
   <subfield code="2">15</subfield>
   <subfield code="o">JOM</subfield>
  </datafield>
  <datafield tag="900" ind1=" " ind2="7">
   <subfield code="b">CC0</subfield>
   <subfield code="u">http://creativecommons.org/publicdomain/zero/1.0</subfield>
   <subfield code="2">nationallicence</subfield>
  </datafield>
  <datafield tag="898" ind1=" " ind2=" ">
   <subfield code="a">BK010053</subfield>
   <subfield code="b">XK010053</subfield>
   <subfield code="c">XK010000</subfield>
  </datafield>
  <datafield tag="949" ind1=" " ind2=" ">
   <subfield code="B">NATIONALLICENCE</subfield>
   <subfield code="F">NATIONALLICENCE</subfield>
   <subfield code="b">NL-cambridge</subfield>
  </datafield>
 </record>
</collection>
