Loading…
Fatigue damage accumulation in aluminium and titanium alloys subjected to block program loading under conditions of stress concentration and fretting
The regularities of high-cycle fatigue of aluminium (D16AT, AMg6) and titanium (VT-14) alloys are studied under regular and block program (two-step) loading conditions in the presence of a stress concentration and fretting. It is shown that, according to the linear damage rule (LDR), the magnitudes...
Saved in:
Published in: | International journal of fatigue 1999-03, Vol.21 (3), p.271-279 |
---|---|
Main Authors: | , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | 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-6d212921456ac454cf528c8f4ee8c571f4b19f0d868d682e11371ecd376e87613 |
---|---|
cites | |
container_end_page | 279 |
container_issue | 3 |
container_start_page | 271 |
container_title | International journal of fatigue |
container_volume | 21 |
creator | Troshchenko, V.T Dragan, V.I Semenyuk, S.M |
description | The regularities of high-cycle fatigue of aluminium (D16AT, AMg6) and titanium (VT-14) alloys are studied under regular and block program (two-step) loading conditions in the presence of a stress concentration and fretting. It is shown that, according to the linear damage rule (LDR), the magnitudes of the cumulative damage at fracture under block program loading with stress concentration and fretting are equal to or exceed those for smooth specimens. The degree of this excess is determined by the degree of the influence of the process initiated on the high block step upon the process of the fatigue damage accumulation on the low block step. No difference has been found in the damage accumulated to the nucleation of a crack and to complete failure. |
doi_str_mv | 10.1016/S0142-1123(98)00080-2 |
format | article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_26969259</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0142112398000802</els_id><sourcerecordid>26969259</sourcerecordid><originalsourceid>FETCH-LOGICAL-c367t-6d212921456ac454cf528c8f4ee8c571f4b19f0d868d682e11371ecd376e87613</originalsourceid><addsrcrecordid>eNqFUc1uFSEYnRhNvFYfwYSFMbqYCszAwMqYxqpJky7UNeHCxw2VgcqPSR_E95XpNLp0Rfg4Px_nDMNLgs8JJvzdV0xmOhJCpzdSvMUYCzzSR8OBiEWO08zo4-HwF_J0eFbKTQdJvLDD8PtSV39qgKxe9QmQNqatLfRhishHpENbffRtRTpaVH3V-yWEdFdQaccbMBX6S0LHkMwPdJvTKesVhaStjyfUooWMTIrWb5oFJYdKzVDKNjQQa97NNn2XodbOej48cToUePFwng3fLz9-u_g8Xl1_-nLx4Wo0E1_qyC0lVFIyM67NzGbjGBVGuBlAGLYQNx-JdNgKLiwXFAiZFgLGTgsHsXAynQ2vd92-9c8GparVFwMh6AipFUW55JIy2YFsB5qcSsng1G32q853imC1laDuS1BbwkoKdV-Cop336sFAF6ODyzoaX_6Rl4nNVHTY-x0G_bO_PGRVjIeejvW556ts8v8x-gO5cZ6W</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>26969259</pqid></control><display><type>article</type><title>Fatigue damage accumulation in aluminium and titanium alloys subjected to block program loading under conditions of stress concentration and fretting</title><source>ScienceDirect Freedom Collection</source><creator>Troshchenko, V.T ; Dragan, V.I ; Semenyuk, S.M</creator><creatorcontrib>Troshchenko, V.T ; Dragan, V.I ; Semenyuk, S.M</creatorcontrib><description>The regularities of high-cycle fatigue of aluminium (D16AT, AMg6) and titanium (VT-14) alloys are studied under regular and block program (two-step) loading conditions in the presence of a stress concentration and fretting. It is shown that, according to the linear damage rule (LDR), the magnitudes of the cumulative damage at fracture under block program loading with stress concentration and fretting are equal to or exceed those for smooth specimens. The degree of this excess is determined by the degree of the influence of the process initiated on the high block step upon the process of the fatigue damage accumulation on the low block step. No difference has been found in the damage accumulated to the nucleation of a crack and to complete failure.</description><identifier>ISSN: 0142-1123</identifier><identifier>EISSN: 1879-3452</identifier><identifier>DOI: 10.1016/S0142-1123(98)00080-2</identifier><identifier>CODEN: IJFADB</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Aluminium and titanium alloys ; Applied sciences ; Block program loading ; Exact sciences and technology ; Fatigue ; Fatigue damage accumulation ; Fretting fatigue ; Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology ; Metals. Metallurgy ; Stress concentration</subject><ispartof>International journal of fatigue, 1999-03, Vol.21 (3), p.271-279</ispartof><rights>1999 Elsevier Science Ltd</rights><rights>1999 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c367t-6d212921456ac454cf528c8f4ee8c571f4b19f0d868d682e11371ecd376e87613</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=1735428$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Troshchenko, V.T</creatorcontrib><creatorcontrib>Dragan, V.I</creatorcontrib><creatorcontrib>Semenyuk, S.M</creatorcontrib><title>Fatigue damage accumulation in aluminium and titanium alloys subjected to block program loading under conditions of stress concentration and fretting</title><title>International journal of fatigue</title><description>The regularities of high-cycle fatigue of aluminium (D16AT, AMg6) and titanium (VT-14) alloys are studied under regular and block program (two-step) loading conditions in the presence of a stress concentration and fretting. It is shown that, according to the linear damage rule (LDR), the magnitudes of the cumulative damage at fracture under block program loading with stress concentration and fretting are equal to or exceed those for smooth specimens. The degree of this excess is determined by the degree of the influence of the process initiated on the high block step upon the process of the fatigue damage accumulation on the low block step. No difference has been found in the damage accumulated to the nucleation of a crack and to complete failure.</description><subject>Aluminium and titanium alloys</subject><subject>Applied sciences</subject><subject>Block program loading</subject><subject>Exact sciences and technology</subject><subject>Fatigue</subject><subject>Fatigue damage accumulation</subject><subject>Fretting fatigue</subject><subject>Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology</subject><subject>Metals. Metallurgy</subject><subject>Stress concentration</subject><issn>0142-1123</issn><issn>1879-3452</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1999</creationdate><recordtype>article</recordtype><recordid>eNqFUc1uFSEYnRhNvFYfwYSFMbqYCszAwMqYxqpJky7UNeHCxw2VgcqPSR_E95XpNLp0Rfg4Px_nDMNLgs8JJvzdV0xmOhJCpzdSvMUYCzzSR8OBiEWO08zo4-HwF_J0eFbKTQdJvLDD8PtSV39qgKxe9QmQNqatLfRhishHpENbffRtRTpaVH3V-yWEdFdQaccbMBX6S0LHkMwPdJvTKesVhaStjyfUooWMTIrWb5oFJYdKzVDKNjQQa97NNn2XodbOej48cToUePFwng3fLz9-u_g8Xl1_-nLx4Wo0E1_qyC0lVFIyM67NzGbjGBVGuBlAGLYQNx-JdNgKLiwXFAiZFgLGTgsHsXAynQ2vd92-9c8GparVFwMh6AipFUW55JIy2YFsB5qcSsng1G32q853imC1laDuS1BbwkoKdV-Cop336sFAF6ODyzoaX_6Rl4nNVHTY-x0G_bO_PGRVjIeejvW556ts8v8x-gO5cZ6W</recordid><startdate>19990301</startdate><enddate>19990301</enddate><creator>Troshchenko, V.T</creator><creator>Dragan, V.I</creator><creator>Semenyuk, S.M</creator><general>Elsevier Ltd</general><general>Elsevier Science</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7QF</scope><scope>8BQ</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>19990301</creationdate><title>Fatigue damage accumulation in aluminium and titanium alloys subjected to block program loading under conditions of stress concentration and fretting</title><author>Troshchenko, V.T ; Dragan, V.I ; Semenyuk, S.M</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c367t-6d212921456ac454cf528c8f4ee8c571f4b19f0d868d682e11371ecd376e87613</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1999</creationdate><topic>Aluminium and titanium alloys</topic><topic>Applied sciences</topic><topic>Block program loading</topic><topic>Exact sciences and technology</topic><topic>Fatigue</topic><topic>Fatigue damage accumulation</topic><topic>Fretting fatigue</topic><topic>Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology</topic><topic>Metals. Metallurgy</topic><topic>Stress concentration</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Troshchenko, V.T</creatorcontrib><creatorcontrib>Dragan, V.I</creatorcontrib><creatorcontrib>Semenyuk, S.M</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>International journal of fatigue</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Troshchenko, V.T</au><au>Dragan, V.I</au><au>Semenyuk, S.M</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Fatigue damage accumulation in aluminium and titanium alloys subjected to block program loading under conditions of stress concentration and fretting</atitle><jtitle>International journal of fatigue</jtitle><date>1999-03-01</date><risdate>1999</risdate><volume>21</volume><issue>3</issue><spage>271</spage><epage>279</epage><pages>271-279</pages><issn>0142-1123</issn><eissn>1879-3452</eissn><coden>IJFADB</coden><abstract>The regularities of high-cycle fatigue of aluminium (D16AT, AMg6) and titanium (VT-14) alloys are studied under regular and block program (two-step) loading conditions in the presence of a stress concentration and fretting. It is shown that, according to the linear damage rule (LDR), the magnitudes of the cumulative damage at fracture under block program loading with stress concentration and fretting are equal to or exceed those for smooth specimens. The degree of this excess is determined by the degree of the influence of the process initiated on the high block step upon the process of the fatigue damage accumulation on the low block step. No difference has been found in the damage accumulated to the nucleation of a crack and to complete failure.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/S0142-1123(98)00080-2</doi><tpages>9</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0142-1123 |
ispartof | International journal of fatigue, 1999-03, Vol.21 (3), p.271-279 |
issn | 0142-1123 1879-3452 |
language | eng |
recordid | cdi_proquest_miscellaneous_26969259 |
source | ScienceDirect Freedom Collection |
subjects | Aluminium and titanium alloys Applied sciences Block program loading Exact sciences and technology Fatigue Fatigue damage accumulation Fretting fatigue Mechanical properties and methods of testing. Rheology. Fracture mechanics. Tribology Metals. Metallurgy Stress concentration |
title | Fatigue damage accumulation in aluminium and titanium alloys subjected to block program loading under conditions of stress concentration and fretting |
url | http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-27T14%3A46%3A28IST&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=Fatigue%20damage%20accumulation%20in%20aluminium%20and%20titanium%20alloys%20subjected%20to%20block%20program%20loading%20under%20conditions%20of%20stress%20concentration%20and%20fretting&rft.jtitle=International%20journal%20of%20fatigue&rft.au=Troshchenko,%20V.T&rft.date=1999-03-01&rft.volume=21&rft.issue=3&rft.spage=271&rft.epage=279&rft.pages=271-279&rft.issn=0142-1123&rft.eissn=1879-3452&rft.coden=IJFADB&rft_id=info:doi/10.1016/S0142-1123(98)00080-2&rft_dat=%3Cproquest_cross%3E26969259%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c367t-6d212921456ac454cf528c8f4ee8c571f4b19f0d868d682e11371ecd376e87613%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=26969259&rft_id=info:pmid/&rfr_iscdi=true |