Loading…
Experimental determination of the residual stresses in a spiral weld overlay tube
Neutron diffraction was used to determine the residual stresses in a spiral weld overlay tube. The specimen was a 2.5 in. OD carbon steel tube covered with a layer of alloy 625 weld overlay. Residual strains in the carbon steel and weld overlay layers were determined using the ferritic (211) and aus...
Saved in:
Published in: | Materials science & engineering. A, Structural materials : properties, microstructure and processing Structural materials : properties, microstructure and processing, 1997-07, Vol.232 (1), p.31-38 |
---|---|
Main Authors: | , , , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
cited_by | cdi_FETCH-LOGICAL-c367t-81281bc5d3d5e34a8aacb5db90ebabf4cd4c0e274cf972184ce5137531c3cc963 |
---|---|
cites | cdi_FETCH-LOGICAL-c367t-81281bc5d3d5e34a8aacb5db90ebabf4cd4c0e274cf972184ce5137531c3cc963 |
container_end_page | 38 |
container_issue | 1 |
container_start_page | 31 |
container_title | Materials science & engineering. A, Structural materials : properties, microstructure and processing |
container_volume | 232 |
creator | Wang, X.-L. Payzant, E.A. Taljat, B. Hubbard, C.R. Keiser, J.R. Jirinec, M.J. |
description | Neutron diffraction was used to determine the residual stresses in a spiral weld overlay tube. The specimen was a 2.5 in. OD carbon steel tube covered with a layer of alloy 625 weld overlay. Residual strains in the carbon steel and weld overlay layers were determined using the ferritic (211) and austenitic (311) reflections, respectively. The residual stresses in each material were derived from the measured strains using Hooke's law and appropriate elastic constants. Tensile stress regions were found not only in the weld metal but also in the heat-affected zone in the carbon steel. The maximum tensile stress was located in the weld overlay layer and amounted to 360 MPa, about 75% of the 0.2% yield strength of the weld metal. The experimental data were compared with a finite element analysis based on an uncoupled thermal-mechanical formulation. Overall, the modeling results are in satisfactory agreement with the experimental data, although the hoop strain (stress) seems to have been overestimated by the finite element model. Additional neutron diffraction measurements reveal that these welding residual stresses vanished after annealing at 900°C for 20 min. |
doi_str_mv | 10.1016/S0921-5093(97)00089-0 |
format | article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_27435550</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0921509397000890</els_id><sourcerecordid>27435550</sourcerecordid><originalsourceid>FETCH-LOGICAL-c367t-81281bc5d3d5e34a8aacb5db90ebabf4cd4c0e274cf972184ce5137531c3cc963</originalsourceid><addsrcrecordid>eNqFkElLBDEQhYMoOC4_QchBRA-tSacz6ZxEBjcYEFHPIV2pxkhP95hkXP69mYW5eqqi6nv1qEfICWeXnPHx1QvTJS8k0-JcqwvGWK0LtkNGvFaiqLQY75LRFtknBzF-ZIhXTI7I8-3PHIOfYZ9sRx0mDDPf2-SHng4tTe9IA0bvFnkbU24jRup7ammc-5CH39g5Onxh6OwvTYsGj8hea7uIx5t6SN7ubl8nD8X06f5xcjMtQIxVKmpe1rwB6YSTKCpbWwuNdI1m2NimrcBVwLBUFbRalbyuACUXSgoOAkCPxSE5W9-dh-FzgTGZmY-AXWd7HBbRZKmQUrIMyjUIYYgxYGvm-WEbfg1nZhmgWQVolukYrcwqQLPUnW4MbATbtcH24ONWXCqpKlVn7HqNYX72y2MwETz2gM4HhGTc4P8x-gPXVoX4</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>27435550</pqid></control><display><type>article</type><title>Experimental determination of the residual stresses in a spiral weld overlay tube</title><source>ScienceDirect Freedom Collection</source><creator>Wang, X.-L. ; Payzant, E.A. ; Taljat, B. ; Hubbard, C.R. ; Keiser, J.R. ; Jirinec, M.J.</creator><creatorcontrib>Wang, X.-L. ; Payzant, E.A. ; Taljat, B. ; Hubbard, C.R. ; Keiser, J.R. ; Jirinec, M.J.</creatorcontrib><description>Neutron diffraction was used to determine the residual stresses in a spiral weld overlay tube. The specimen was a 2.5 in. OD carbon steel tube covered with a layer of alloy 625 weld overlay. Residual strains in the carbon steel and weld overlay layers were determined using the ferritic (211) and austenitic (311) reflections, respectively. The residual stresses in each material were derived from the measured strains using Hooke's law and appropriate elastic constants. Tensile stress regions were found not only in the weld metal but also in the heat-affected zone in the carbon steel. The maximum tensile stress was located in the weld overlay layer and amounted to 360 MPa, about 75% of the 0.2% yield strength of the weld metal. The experimental data were compared with a finite element analysis based on an uncoupled thermal-mechanical formulation. Overall, the modeling results are in satisfactory agreement with the experimental data, although the hoop strain (stress) seems to have been overestimated by the finite element model. Additional neutron diffraction measurements reveal that these welding residual stresses vanished after annealing at 900°C for 20 min.</description><identifier>ISSN: 0921-5093</identifier><identifier>EISSN: 1873-4936</identifier><identifier>DOI: 10.1016/S0921-5093(97)00089-0</identifier><language>eng</language><publisher>Amsterdam: Elsevier B.V</publisher><subject>Analysing. Testing. Standards ; Applied sciences ; Exact sciences and technology ; Metals. Metallurgy ; Neutron diffraction ; Residual stresses ; Stress analysis ; Weld overlay</subject><ispartof>Materials science & engineering. A, Structural materials : properties, microstructure and processing, 1997-07, Vol.232 (1), p.31-38</ispartof><rights>1997 Elsevier Science S.A. All rights reserved.</rights><rights>1997 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c367t-81281bc5d3d5e34a8aacb5db90ebabf4cd4c0e274cf972184ce5137531c3cc963</citedby><cites>FETCH-LOGICAL-c367t-81281bc5d3d5e34a8aacb5db90ebabf4cd4c0e274cf972184ce5137531c3cc963</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>315,786,790,27957,27958</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=2757478$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Wang, X.-L.</creatorcontrib><creatorcontrib>Payzant, E.A.</creatorcontrib><creatorcontrib>Taljat, B.</creatorcontrib><creatorcontrib>Hubbard, C.R.</creatorcontrib><creatorcontrib>Keiser, J.R.</creatorcontrib><creatorcontrib>Jirinec, M.J.</creatorcontrib><title>Experimental determination of the residual stresses in a spiral weld overlay tube</title><title>Materials science & engineering. A, Structural materials : properties, microstructure and processing</title><description>Neutron diffraction was used to determine the residual stresses in a spiral weld overlay tube. The specimen was a 2.5 in. OD carbon steel tube covered with a layer of alloy 625 weld overlay. Residual strains in the carbon steel and weld overlay layers were determined using the ferritic (211) and austenitic (311) reflections, respectively. The residual stresses in each material were derived from the measured strains using Hooke's law and appropriate elastic constants. Tensile stress regions were found not only in the weld metal but also in the heat-affected zone in the carbon steel. The maximum tensile stress was located in the weld overlay layer and amounted to 360 MPa, about 75% of the 0.2% yield strength of the weld metal. The experimental data were compared with a finite element analysis based on an uncoupled thermal-mechanical formulation. Overall, the modeling results are in satisfactory agreement with the experimental data, although the hoop strain (stress) seems to have been overestimated by the finite element model. Additional neutron diffraction measurements reveal that these welding residual stresses vanished after annealing at 900°C for 20 min.</description><subject>Analysing. Testing. Standards</subject><subject>Applied sciences</subject><subject>Exact sciences and technology</subject><subject>Metals. Metallurgy</subject><subject>Neutron diffraction</subject><subject>Residual stresses</subject><subject>Stress analysis</subject><subject>Weld overlay</subject><issn>0921-5093</issn><issn>1873-4936</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1997</creationdate><recordtype>article</recordtype><recordid>eNqFkElLBDEQhYMoOC4_QchBRA-tSacz6ZxEBjcYEFHPIV2pxkhP95hkXP69mYW5eqqi6nv1qEfICWeXnPHx1QvTJS8k0-JcqwvGWK0LtkNGvFaiqLQY75LRFtknBzF-ZIhXTI7I8-3PHIOfYZ9sRx0mDDPf2-SHng4tTe9IA0bvFnkbU24jRup7ammc-5CH39g5Onxh6OwvTYsGj8hea7uIx5t6SN7ubl8nD8X06f5xcjMtQIxVKmpe1rwB6YSTKCpbWwuNdI1m2NimrcBVwLBUFbRalbyuACUXSgoOAkCPxSE5W9-dh-FzgTGZmY-AXWd7HBbRZKmQUrIMyjUIYYgxYGvm-WEbfg1nZhmgWQVolukYrcwqQLPUnW4MbATbtcH24ONWXCqpKlVn7HqNYX72y2MwETz2gM4HhGTc4P8x-gPXVoX4</recordid><startdate>19970731</startdate><enddate>19970731</enddate><creator>Wang, X.-L.</creator><creator>Payzant, E.A.</creator><creator>Taljat, B.</creator><creator>Hubbard, C.R.</creator><creator>Keiser, J.R.</creator><creator>Jirinec, M.J.</creator><general>Elsevier B.V</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8BQ</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>19970731</creationdate><title>Experimental determination of the residual stresses in a spiral weld overlay tube</title><author>Wang, X.-L. ; Payzant, E.A. ; Taljat, B. ; Hubbard, C.R. ; Keiser, J.R. ; Jirinec, M.J.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c367t-81281bc5d3d5e34a8aacb5db90ebabf4cd4c0e274cf972184ce5137531c3cc963</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1997</creationdate><topic>Analysing. Testing. Standards</topic><topic>Applied sciences</topic><topic>Exact sciences and technology</topic><topic>Metals. Metallurgy</topic><topic>Neutron diffraction</topic><topic>Residual stresses</topic><topic>Stress analysis</topic><topic>Weld overlay</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Wang, X.-L.</creatorcontrib><creatorcontrib>Payzant, E.A.</creatorcontrib><creatorcontrib>Taljat, B.</creatorcontrib><creatorcontrib>Hubbard, C.R.</creatorcontrib><creatorcontrib>Keiser, J.R.</creatorcontrib><creatorcontrib>Jirinec, M.J.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Materials science & engineering. A, Structural materials : properties, microstructure and processing</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Wang, X.-L.</au><au>Payzant, E.A.</au><au>Taljat, B.</au><au>Hubbard, C.R.</au><au>Keiser, J.R.</au><au>Jirinec, M.J.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Experimental determination of the residual stresses in a spiral weld overlay tube</atitle><jtitle>Materials science & engineering. A, Structural materials : properties, microstructure and processing</jtitle><date>1997-07-31</date><risdate>1997</risdate><volume>232</volume><issue>1</issue><spage>31</spage><epage>38</epage><pages>31-38</pages><issn>0921-5093</issn><eissn>1873-4936</eissn><notes>ObjectType-Article-2</notes><notes>SourceType-Scholarly Journals-1</notes><notes>ObjectType-Feature-1</notes><notes>content type line 23</notes><abstract>Neutron diffraction was used to determine the residual stresses in a spiral weld overlay tube. The specimen was a 2.5 in. OD carbon steel tube covered with a layer of alloy 625 weld overlay. Residual strains in the carbon steel and weld overlay layers were determined using the ferritic (211) and austenitic (311) reflections, respectively. The residual stresses in each material were derived from the measured strains using Hooke's law and appropriate elastic constants. Tensile stress regions were found not only in the weld metal but also in the heat-affected zone in the carbon steel. The maximum tensile stress was located in the weld overlay layer and amounted to 360 MPa, about 75% of the 0.2% yield strength of the weld metal. The experimental data were compared with a finite element analysis based on an uncoupled thermal-mechanical formulation. Overall, the modeling results are in satisfactory agreement with the experimental data, although the hoop strain (stress) seems to have been overestimated by the finite element model. Additional neutron diffraction measurements reveal that these welding residual stresses vanished after annealing at 900°C for 20 min.</abstract><cop>Amsterdam</cop><pub>Elsevier B.V</pub><doi>10.1016/S0921-5093(97)00089-0</doi><tpages>8</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0921-5093 |
ispartof | Materials science & engineering. A, Structural materials : properties, microstructure and processing, 1997-07, Vol.232 (1), p.31-38 |
issn | 0921-5093 1873-4936 |
language | eng |
recordid | cdi_proquest_miscellaneous_27435550 |
source | ScienceDirect Freedom Collection |
subjects | Analysing. Testing. Standards Applied sciences Exact sciences and technology Metals. Metallurgy Neutron diffraction Residual stresses Stress analysis Weld overlay |
title | Experimental determination of the residual stresses in a spiral weld overlay tube |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-09-23T06%3A33%3A16IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Experimental%20determination%20of%20the%20residual%20stresses%20in%20a%20spiral%20weld%20overlay%20tube&rft.jtitle=Materials%20science%20&%20engineering.%20A,%20Structural%20materials%20:%20properties,%20microstructure%20and%20processing&rft.au=Wang,%20X.-L.&rft.date=1997-07-31&rft.volume=232&rft.issue=1&rft.spage=31&rft.epage=38&rft.pages=31-38&rft.issn=0921-5093&rft.eissn=1873-4936&rft_id=info:doi/10.1016/S0921-5093(97)00089-0&rft_dat=%3Cproquest_cross%3E27435550%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c367t-81281bc5d3d5e34a8aacb5db90ebabf4cd4c0e274cf972184ce5137531c3cc963%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=27435550&rft_id=info:pmid/&rfr_iscdi=true |