Loading…

Stress-controlled LCF experiments and ratcheting behaviour simulation of a nickel-based single crystal superalloy with [001] orientation

Uniaxial ratcheting behaviour and low cycle fatigue (LCF) failure mechanism of nickel-based single crystal superalloy DD6 with [001] orientation are investigated through the stress-controlled LCF tests with stress ratio of −1. Then the deformation behaviour during the whole-lifetime from the beginni...

Full description

Saved in:
Bibliographic Details
Published in:Chinese journal of aeronautics 2021-08, Vol.34 (8), p.112-121
Main Authors: ZHANG, Bin, WANG, Rongqiao, HU, Dianyin, JIANG, Kanghe, MAO, Jianxing, JING, Fulei, HAO, Xinyi
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-c372t-ec28e367291aac0a46da32a845d490b4e2ecd41cef9ca4db7e6f6acade2427cc3
cites cdi_FETCH-LOGICAL-c372t-ec28e367291aac0a46da32a845d490b4e2ecd41cef9ca4db7e6f6acade2427cc3
container_end_page 121
container_issue 8
container_start_page 112
container_title Chinese journal of aeronautics
container_volume 34
creator ZHANG, Bin
WANG, Rongqiao
HU, Dianyin
JIANG, Kanghe
MAO, Jianxing
JING, Fulei
HAO, Xinyi
description Uniaxial ratcheting behaviour and low cycle fatigue (LCF) failure mechanism of nickel-based single crystal superalloy DD6 with [001] orientation are investigated through the stress-controlled LCF tests with stress ratio of −1. Then the deformation behaviour during the whole-lifetime from the beginning of the experiment to the fracture of the specimen, as well as the fractographic/metallographic morphology, are compared with the strain-controlled LCF experimental results. Through the scanning electron microscope (SEM) observations, it is shown that the failure characteristics under stress-controlled LCF loading are similar with those under strain-controlled loading. Nevertheless, unlike strain-controlled LCF loading, even under fully reversed cycle loading for stress-controlled LCF, DD6 shows significant ratcheting behaviour due to the tension-compression asymmetry. In addition, the LCF lifetimes under stress control are significantly shorter than the LCF lifetimes under strain control, and the culprit might be the detrimental effect of ratcheting strain on LCF lifetime. Based on these phenomena, an improved crystal plasticity constitutive model on the basis of slip-based Walker constitutive model is developed through modifying the kinematic hardening rule in order to overcome the inaccurate prediction of decelerating stage and stable stage of ratcheting behaviour. Furthermore, combining the continuum damage mechanics, a damage-coupled crystal plasticity constitutive model is proposed to reflect the damage behaviour of DD6 and the accelerating stage of ratcheting behaviour. The simulation results for the stress-controlled LCF deformation behaviour including the whole-lifetime ratcheting behaviour show good agreement with the experimental data.
doi_str_mv 10.1016/j.cja.2020.05.030
format article
fullrecord <record><control><sourceid>wanfang_jour_cross</sourceid><recordid>TN_cdi_wanfang_journals_hkxb_e202108010</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><wanfj_id>hkxb_e202108010</wanfj_id><els_id>S1000936120302661</els_id><sourcerecordid>hkxb_e202108010</sourcerecordid><originalsourceid>FETCH-LOGICAL-c372t-ec28e367291aac0a46da32a845d490b4e2ecd41cef9ca4db7e6f6acade2427cc3</originalsourceid><addsrcrecordid>eNp9kMFO3DAQhnMoUin0AXrzraekYyebbNRTtSql0kocoKeqsibjCetgbGR7gX2DPjam2zOnufz_N_q_qvokoZEg-y9LQws2ChQ0sGqghXfVqQSAemx7-b76kNIC0I6DhNPq73WOnFJNwecYnGMjtpsLwc8PHO09-5wEeiMiZtpxtv5WTLzDRxv2USR7v3eYbfAizAKFt3THrp4wFUoqWceC4iFldCLtCxCdCwfxZPNO_AaQf0SItrz4hzivTmZ0iT_-v2fVr4vvN5vLenv14-fm27amdlC5ZlJrbvtBjRKRALveYKtw3a1MN8LUsWIynSSeR8LOTAP3c4-EhlWnBqL2rPp85D6hn9Hf6qVM8eWj3t09T5qLNglrkFCS8pikGFKKPOuHogTjQUvQr6L1ooto_Spaw0oX0aXz9djhMuHRctSJykRiYyNT1ibYN9ovDGSL9g</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype></control><display><type>article</type><title>Stress-controlled LCF experiments and ratcheting behaviour simulation of a nickel-based single crystal superalloy with [001] orientation</title><source>ScienceDirect Journals</source><creator>ZHANG, Bin ; WANG, Rongqiao ; HU, Dianyin ; JIANG, Kanghe ; MAO, Jianxing ; JING, Fulei ; HAO, Xinyi</creator><creatorcontrib>ZHANG, Bin ; WANG, Rongqiao ; HU, Dianyin ; JIANG, Kanghe ; MAO, Jianxing ; JING, Fulei ; HAO, Xinyi</creatorcontrib><description>Uniaxial ratcheting behaviour and low cycle fatigue (LCF) failure mechanism of nickel-based single crystal superalloy DD6 with [001] orientation are investigated through the stress-controlled LCF tests with stress ratio of −1. Then the deformation behaviour during the whole-lifetime from the beginning of the experiment to the fracture of the specimen, as well as the fractographic/metallographic morphology, are compared with the strain-controlled LCF experimental results. Through the scanning electron microscope (SEM) observations, it is shown that the failure characteristics under stress-controlled LCF loading are similar with those under strain-controlled loading. Nevertheless, unlike strain-controlled LCF loading, even under fully reversed cycle loading for stress-controlled LCF, DD6 shows significant ratcheting behaviour due to the tension-compression asymmetry. In addition, the LCF lifetimes under stress control are significantly shorter than the LCF lifetimes under strain control, and the culprit might be the detrimental effect of ratcheting strain on LCF lifetime. Based on these phenomena, an improved crystal plasticity constitutive model on the basis of slip-based Walker constitutive model is developed through modifying the kinematic hardening rule in order to overcome the inaccurate prediction of decelerating stage and stable stage of ratcheting behaviour. Furthermore, combining the continuum damage mechanics, a damage-coupled crystal plasticity constitutive model is proposed to reflect the damage behaviour of DD6 and the accelerating stage of ratcheting behaviour. The simulation results for the stress-controlled LCF deformation behaviour including the whole-lifetime ratcheting behaviour show good agreement with the experimental data.</description><identifier>ISSN: 1000-9361</identifier><identifier>DOI: 10.1016/j.cja.2020.05.030</identifier><language>eng</language><publisher>Elsevier Ltd</publisher><subject>Crystal plasticity constitutive model ; Low cycle fatigue ; Nickel-based single crystal superalloy ; Ratcheting behaviour ; Stress-controlled experiment</subject><ispartof>Chinese journal of aeronautics, 2021-08, Vol.34 (8), p.112-121</ispartof><rights>2020 Chinese Society of Aeronautics and Astronautics</rights><rights>Copyright © Wanfang Data Co. Ltd. All Rights Reserved.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c372t-ec28e367291aac0a46da32a845d490b4e2ecd41cef9ca4db7e6f6acade2427cc3</citedby><cites>FETCH-LOGICAL-c372t-ec28e367291aac0a46da32a845d490b4e2ecd41cef9ca4db7e6f6acade2427cc3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://www.wanfangdata.com.cn/images/PeriodicalImages/hkxb-e/hkxb-e.jpg</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S1000936120302661$$EHTML$$P50$$Gelsevier$$Hfree_for_read</linktohtml><link.rule.ids>314,780,784,3549,27924,27925,45780</link.rule.ids></links><search><creatorcontrib>ZHANG, Bin</creatorcontrib><creatorcontrib>WANG, Rongqiao</creatorcontrib><creatorcontrib>HU, Dianyin</creatorcontrib><creatorcontrib>JIANG, Kanghe</creatorcontrib><creatorcontrib>MAO, Jianxing</creatorcontrib><creatorcontrib>JING, Fulei</creatorcontrib><creatorcontrib>HAO, Xinyi</creatorcontrib><title>Stress-controlled LCF experiments and ratcheting behaviour simulation of a nickel-based single crystal superalloy with [001] orientation</title><title>Chinese journal of aeronautics</title><description>Uniaxial ratcheting behaviour and low cycle fatigue (LCF) failure mechanism of nickel-based single crystal superalloy DD6 with [001] orientation are investigated through the stress-controlled LCF tests with stress ratio of −1. Then the deformation behaviour during the whole-lifetime from the beginning of the experiment to the fracture of the specimen, as well as the fractographic/metallographic morphology, are compared with the strain-controlled LCF experimental results. Through the scanning electron microscope (SEM) observations, it is shown that the failure characteristics under stress-controlled LCF loading are similar with those under strain-controlled loading. Nevertheless, unlike strain-controlled LCF loading, even under fully reversed cycle loading for stress-controlled LCF, DD6 shows significant ratcheting behaviour due to the tension-compression asymmetry. In addition, the LCF lifetimes under stress control are significantly shorter than the LCF lifetimes under strain control, and the culprit might be the detrimental effect of ratcheting strain on LCF lifetime. Based on these phenomena, an improved crystal plasticity constitutive model on the basis of slip-based Walker constitutive model is developed through modifying the kinematic hardening rule in order to overcome the inaccurate prediction of decelerating stage and stable stage of ratcheting behaviour. Furthermore, combining the continuum damage mechanics, a damage-coupled crystal plasticity constitutive model is proposed to reflect the damage behaviour of DD6 and the accelerating stage of ratcheting behaviour. The simulation results for the stress-controlled LCF deformation behaviour including the whole-lifetime ratcheting behaviour show good agreement with the experimental data.</description><subject>Crystal plasticity constitutive model</subject><subject>Low cycle fatigue</subject><subject>Nickel-based single crystal superalloy</subject><subject>Ratcheting behaviour</subject><subject>Stress-controlled experiment</subject><issn>1000-9361</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNp9kMFO3DAQhnMoUin0AXrzraekYyebbNRTtSql0kocoKeqsibjCetgbGR7gX2DPjam2zOnufz_N_q_qvokoZEg-y9LQws2ChQ0sGqghXfVqQSAemx7-b76kNIC0I6DhNPq73WOnFJNwecYnGMjtpsLwc8PHO09-5wEeiMiZtpxtv5WTLzDRxv2USR7v3eYbfAizAKFt3THrp4wFUoqWceC4iFldCLtCxCdCwfxZPNO_AaQf0SItrz4hzivTmZ0iT_-v2fVr4vvN5vLenv14-fm27amdlC5ZlJrbvtBjRKRALveYKtw3a1MN8LUsWIynSSeR8LOTAP3c4-EhlWnBqL2rPp85D6hn9Hf6qVM8eWj3t09T5qLNglrkFCS8pikGFKKPOuHogTjQUvQr6L1ooto_Spaw0oX0aXz9djhMuHRctSJykRiYyNT1ibYN9ovDGSL9g</recordid><startdate>20210801</startdate><enddate>20210801</enddate><creator>ZHANG, Bin</creator><creator>WANG, Rongqiao</creator><creator>HU, Dianyin</creator><creator>JIANG, Kanghe</creator><creator>MAO, Jianxing</creator><creator>JING, Fulei</creator><creator>HAO, Xinyi</creator><general>Elsevier Ltd</general><general>Research Institute of Aero-Engine,Beihang University,Beijing 100083,China%Hunan Aviation Powerplant Research Institute,Aero Engine (Group) Corporation of China,Zhuzhou 412002,China%Aero Engine Academy of China,Aero Engine (Group) Corporation of China,Beijing 101304,China</general><general>School of Energy,Power Engineering,Beihang University,Beijing 100083,China%School of Energy,Power Engineering,Beihang University,Beijing 100083,China</general><general>Beijing Key Laboratory of Aero-Engine Structure and Strength,Beijing 100083,China%School of Energy,Power Engineering,Beihang University,Beijing 100083,China</general><general>Beijing Key Laboratory of Aero-Engine Structure and Strength,Beijing 100083,China</general><scope>6I.</scope><scope>AAFTH</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>2B.</scope><scope>4A8</scope><scope>92I</scope><scope>93N</scope><scope>PSX</scope><scope>TCJ</scope></search><sort><creationdate>20210801</creationdate><title>Stress-controlled LCF experiments and ratcheting behaviour simulation of a nickel-based single crystal superalloy with [001] orientation</title><author>ZHANG, Bin ; WANG, Rongqiao ; HU, Dianyin ; JIANG, Kanghe ; MAO, Jianxing ; JING, Fulei ; HAO, Xinyi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c372t-ec28e367291aac0a46da32a845d490b4e2ecd41cef9ca4db7e6f6acade2427cc3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Crystal plasticity constitutive model</topic><topic>Low cycle fatigue</topic><topic>Nickel-based single crystal superalloy</topic><topic>Ratcheting behaviour</topic><topic>Stress-controlled experiment</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>ZHANG, Bin</creatorcontrib><creatorcontrib>WANG, Rongqiao</creatorcontrib><creatorcontrib>HU, Dianyin</creatorcontrib><creatorcontrib>JIANG, Kanghe</creatorcontrib><creatorcontrib>MAO, Jianxing</creatorcontrib><creatorcontrib>JING, Fulei</creatorcontrib><creatorcontrib>HAO, Xinyi</creatorcontrib><collection>ScienceDirect Open Access Titles</collection><collection>Elsevier:ScienceDirect:Open Access</collection><collection>CrossRef</collection><collection>Wanfang Data Journals - Hong Kong</collection><collection>WANFANG Data Centre</collection><collection>Wanfang Data Journals</collection><collection>万方数据期刊 - 香港版</collection><collection>China Online Journals (COJ)</collection><collection>China Online Journals (COJ)</collection><jtitle>Chinese journal of aeronautics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>ZHANG, Bin</au><au>WANG, Rongqiao</au><au>HU, Dianyin</au><au>JIANG, Kanghe</au><au>MAO, Jianxing</au><au>JING, Fulei</au><au>HAO, Xinyi</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Stress-controlled LCF experiments and ratcheting behaviour simulation of a nickel-based single crystal superalloy with [001] orientation</atitle><jtitle>Chinese journal of aeronautics</jtitle><date>2021-08-01</date><risdate>2021</risdate><volume>34</volume><issue>8</issue><spage>112</spage><epage>121</epage><pages>112-121</pages><issn>1000-9361</issn><abstract>Uniaxial ratcheting behaviour and low cycle fatigue (LCF) failure mechanism of nickel-based single crystal superalloy DD6 with [001] orientation are investigated through the stress-controlled LCF tests with stress ratio of −1. Then the deformation behaviour during the whole-lifetime from the beginning of the experiment to the fracture of the specimen, as well as the fractographic/metallographic morphology, are compared with the strain-controlled LCF experimental results. Through the scanning electron microscope (SEM) observations, it is shown that the failure characteristics under stress-controlled LCF loading are similar with those under strain-controlled loading. Nevertheless, unlike strain-controlled LCF loading, even under fully reversed cycle loading for stress-controlled LCF, DD6 shows significant ratcheting behaviour due to the tension-compression asymmetry. In addition, the LCF lifetimes under stress control are significantly shorter than the LCF lifetimes under strain control, and the culprit might be the detrimental effect of ratcheting strain on LCF lifetime. Based on these phenomena, an improved crystal plasticity constitutive model on the basis of slip-based Walker constitutive model is developed through modifying the kinematic hardening rule in order to overcome the inaccurate prediction of decelerating stage and stable stage of ratcheting behaviour. Furthermore, combining the continuum damage mechanics, a damage-coupled crystal plasticity constitutive model is proposed to reflect the damage behaviour of DD6 and the accelerating stage of ratcheting behaviour. The simulation results for the stress-controlled LCF deformation behaviour including the whole-lifetime ratcheting behaviour show good agreement with the experimental data.</abstract><pub>Elsevier Ltd</pub><doi>10.1016/j.cja.2020.05.030</doi><tpages>10</tpages><oa>free_for_read</oa></addata></record>
fulltext fulltext
identifier ISSN: 1000-9361
ispartof Chinese journal of aeronautics, 2021-08, Vol.34 (8), p.112-121
issn 1000-9361
language eng
recordid cdi_wanfang_journals_hkxb_e202108010
source ScienceDirect Journals
subjects Crystal plasticity constitutive model
Low cycle fatigue
Nickel-based single crystal superalloy
Ratcheting behaviour
Stress-controlled experiment
title Stress-controlled LCF experiments and ratcheting behaviour simulation of a nickel-based single crystal superalloy with [001] orientation
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-05T01%3A56%3A17IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-wanfang_jour_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Stress-controlled%20LCF%20experiments%20and%20ratcheting%20behaviour%20simulation%20of%20a%20nickel-based%20single%20crystal%20superalloy%20with%20%5B001%5D%20orientation&rft.jtitle=Chinese%20journal%20of%20aeronautics&rft.au=ZHANG,%20Bin&rft.date=2021-08-01&rft.volume=34&rft.issue=8&rft.spage=112&rft.epage=121&rft.pages=112-121&rft.issn=1000-9361&rft_id=info:doi/10.1016/j.cja.2020.05.030&rft_dat=%3Cwanfang_jour_cross%3Ehkxb_e202108010%3C/wanfang_jour_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c372t-ec28e367291aac0a46da32a845d490b4e2ecd41cef9ca4db7e6f6acade2427cc3%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_id=info:pmid/&rft_wanfj_id=hkxb_e202108010&rfr_iscdi=true