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      Residual stress measurement techniques for Ti6Al4V parts fabricated using selective laser melting: state of the art review

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      Rapid Prototyping Journal
      Emerald

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          Abstract

          Purpose

          This paper aims to generate a review of available techniques to measure Residual Stress (RS) in Ti6Al4V components made by Ti6Al4V.

          Design/methodology/approach

          State of the art; literature review in the field of Residual Stress measurement of Ti6Al4V parts made by selective laser melting (SLM).

          Findings

          Different Residual Stress measurement techniques were detailed, regarding its concept, advantages and limitations. Regarding all researched references, hole drilling (semi destructive) and X-ray diffraction (nondestructive) were the most cited techniques for Residual Stress measurement of Ti6Al4V parts made by SLM.

          Originality/value

          An extensive analysis of RS measurement techniques for Ti6Al4V parts made by SLM.

          Related collections

          Most cited references81

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          Additive manufacturing of metallic components – Process, structure and properties

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            Heat treatment of Ti6Al4V produced by Selective Laser Melting: Microstructure and mechanical properties

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              • Record: found
              • Abstract: not found
              • Article: not found

              Densification behavior, microstructure evolution, and wear performance of selective laser melting processed commercially pure titanium

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                Author and article information

                Journal
                Rapid Prototyping Journal
                RPJ
                Emerald
                1355-2546
                1355-2546
                July 03 2020
                August 10 2023
                July 03 2020
                August 10 2023
                : 29
                : 8
                : 1549-1564
                Article
                10.1108/RPJ-04-2019-0097
                d8bd847e-b1e5-43f6-b046-94fce68917ea
                © 2023

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