<?xml version="1.0" encoding="UTF-8"?><?xml-stylesheet type="text/xsl" href="static/style.xsl"?><OAI-PMH xmlns="http://www.openarchives.org/OAI/2.0/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/ http://www.openarchives.org/OAI/2.0/OAI-PMH.xsd"><responseDate>2026-05-27T21:56:43Z</responseDate><request verb="GetRecord" identifier="oai:riuma.uma.es:10630/26357" metadataPrefix="mods">https://riuma.uma.es/rest/oai/request</request><GetRecord><record><header><identifier>oai:riuma.uma.es:10630/26357</identifier><datestamp>2026-02-03T11:02:43Z</datestamp><setSpec>com_10630_2254</setSpec><setSpec>col_10630_37953</setSpec></header><metadata><mods:mods xmlns:doc="http://www.lyncode.com/xoai" xmlns:mods="http://www.loc.gov/mods/v3" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-1.xsd">
   <mods:name>
      <mods:namePart>Cruces, A.S.</mods:namePart>
   </mods:name>
   <mods:name>
      <mods:namePart>Branco, Ricardo</mods:namePart>
   </mods:name>
   <mods:name>
      <mods:namePart>Borrego, L.P.</mods:namePart>
   </mods:name>
   <mods:name>
      <mods:namePart>López-Crespo, Pablo</mods:namePart>
   </mods:name>
   <mods:extension>
      <mods:dateAvailable encoding="iso8601">2023-04-21T11:44:52Z</mods:dateAvailable>
   </mods:extension>
   <mods:extension>
      <mods:dateAccessioned encoding="iso8601">2023-04-21T11:44:52Z</mods:dateAccessioned>
   </mods:extension>
   <mods:originInfo>
      <mods:dateIssued encoding="iso8601">2023</mods:dateIssued>
   </mods:originInfo>
   <mods:identifier type="citation">Cruces, Branco, R., Borrego, L. P., &amp; Lopez-Crespo, P. (2023). Energy-based critical plane fatigue methods applied to additively manufactured 18Ni300 steel. International Journal of Fatigue, 170, 107548–. https://doi.org/10.1016/j.ijfatigue.2023.107548</mods:identifier>
   <mods:identifier type="uri">https://hdl.handle.net/10630/26357</mods:identifier>
   <mods:identifier type="doi">https://doi.org/10.1016/j.ijfatigue.2023.107548</mods:identifier>
   <mods:abstract>In this work, the uniaxial and biaxial fatigue behaviour of maraging steel (18Ni300) obtained by additive manufacturing was studied. The material was evaluated using several biaxial load paths and different load levels. The predictive capacity of the fatigue life and crack initiation angle of the critical plane methods of Liu (I and II), and Chu, Conle, and Bonnen (CCB) were evaluated. The results obtained showed that normal stresses had a strong effect on the fatigue life. In general, the best estimates of the useful life and initial crack angle prediction were obtained with the CCB method.</mods:abstract>
   <mods:language>
      <mods:languageTerm>eng</mods:languageTerm>
   </mods:language>
   <mods:accessCondition type="useAndReproduction">http://creativecommons.org/licenses/by-nc-nd/4.0/</mods:accessCondition>
   <mods:accessCondition type="useAndReproduction">open access</mods:accessCondition>
   <mods:accessCondition type="useAndReproduction">Attribution-NonCommercial-NoDerivatives 4.0 Internacional</mods:accessCondition>
   <mods:subject>
      <mods:topic>Metales -- Fatiga</mods:topic>
   </mods:subject>
   <mods:subject>
      <mods:topic>Fatiga (Fisiología)</mods:topic>
   </mods:subject>
   <mods:titleInfo>
      <mods:title>Energy-based critical plane fatigue methods applied to additively manufactured 18Ni300 steel</mods:title>
   </mods:titleInfo>
   <mods:genre>journal article</mods:genre>
</mods:mods>
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