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<article-meta><doi>203</doi>
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<article-title>Determination of Mode I Stress Intensity Factor for Orthotropic Laminates Using a Single Strain Gage</article-title>
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<author>Debaleena Chakraborty<sup>a</sup>, D. Chakraborty<sup>b</sup> and K. S. R. K. Murthy<sup>c</sup>  </author>

<aff>Department of Mechanical Engineering, Indian Institute of Technology Guwahati, <br />Guwahati-781039, India. </aff>

<email><a href="mailto:debaleena@iitg.ernet.in"><sup>a</sup>debaleena@iitg.ernet.in</a></email>

<email><a href="mailto:chakra@iitg.ernet.in"><sup>b</sup>chakra@iitg.ernet.in</a></email>

<email><a href="mailto:ksrkm@iitg.ernet.in "><sup>c</sup>ksrkm@iitg.ernet.in </a></email>

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<title>ABSTRACT</title>
<p>In this paper, a single strain gage technique has been used for determination of mode I stress intensity factor (SIF) for orthotropic laminates. Considering mode I crack in an orthotropic laminate as plane stress problem, angular position and orientation of a strain gage has been determined such that mode I SIF could be determined pasting a single strain gage. A finite element based procedure has been adopted to simulate the determination of mode I SIF, K<sub>I</sub> using a single strain gage. Numerical examples show that the single strain gage technique can be used to determine accurate value of  K<sub>I</sub> of orthotropic laminates.  </p>
<p><i>Keywords: </i>Composites, Orthotropic, Strain gage, Finite element analysis, Stress intensity factor. </p>
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