An equivalent model of a nonlinear bolted flange joint

Jamia, Nidhal; Jalali, H.; Taghipour, Javad; Friswell, Michael; Khodaparast, Hamed Haddad

doi:10.1016/j.ymssp.2020.107507

Journal article 741 views 389 downloads

An equivalent model of a nonlinear bolted flange joint

Nidhal Jamia

, H. Jalali, Javad Taghipour, Michael Friswell, Hamed Haddad Khodaparast

Mechanical Systems and Signal Processing, Volume: 153, Start page: 107507

Swansea University Authors: Nidhal Jamia , Javad Taghipour, Michael Friswell, Hamed Haddad Khodaparast

PDF | Version of Record

© 2020 Author(s). All article content, except where otherwise noted, is licensed under a Creative Commons Attribution 4.0 (CC BY) License
Download (4.2MB)

Check full text

DOI (Published version): 10.1016/j.ymssp.2020.107507

Abstract

The dynamic response of individual components in an assembled structure shows high accuracy compared to experimental measurements of the system response. However, when it comes to assemblies, the conventional linear approaches fail to deliver good accuracy, due to the uncertain linear and nonlinear...

Full description

Published in:	Mechanical Systems and Signal Processing
ISSN:	0888-3270
Published:	Elsevier BV 2021
Online Access:	Check full text
URI:	https://cronfa.swan.ac.uk/Record/cronfa55840
Tags:	Add Tag No Tags, Be the first to tag this record!

first_indexed	2020-12-07T11:11:18Z
last_indexed	2023-01-11T14:34:40Z
id	cronfa55840
recordtype	SURis
fullrecord	<?xml version="1.0"?><rfc1807><datestamp>2022-10-31T18:15:20.1421794</datestamp><bib-version>v2</bib-version><id>55840</id><entry>2020-12-07</entry><title>An equivalent model of a nonlinear bolted flange joint</title><swanseaauthors><author><sid>846b2cd3a7717b296654010df30cb22a</sid><ORCID>0000-0003-0643-7812</ORCID><firstname>Nidhal</firstname><surname>Jamia</surname><name>Nidhal Jamia</name><active>true</active><ethesisStudent>false</ethesisStudent></author><author><sid>dc7cba835218dde37fe7f447962d4058</sid><firstname>Javad</firstname><surname>Taghipour</surname><name>Javad Taghipour</name><active>true</active><ethesisStudent>false</ethesisStudent></author><author><sid>5894777b8f9c6e64bde3568d68078d40</sid><firstname>Michael</firstname><surname>Friswell</surname><name>Michael Friswell</name><active>true</active><ethesisStudent>false</ethesisStudent></author><author><sid>f207b17edda9c4c3ea074cbb7555efc1</sid><ORCID>0000-0002-3721-4980</ORCID><firstname>Hamed</firstname><surname>Haddad Khodaparast</surname><name>Hamed Haddad Khodaparast</name><active>true</active><ethesisStudent>false</ethesisStudent></author></swanseaauthors><date>2020-12-07</date><deptcode>AERO</deptcode><abstract>The dynamic response of individual components in an assembled structure shows high accuracy compared to experimental measurements of the system response. However, when it comes to assemblies, the conventional linear approaches fail to deliver good accuracy, due to the uncertain linear and nonlinear mechanisms in the contact interface of the joints. Therefore, the inherent dynamics of the contact interfaces needs to be considered in modeling assembled structures. In this paper the prediction of the nonlinear dynamic response in a bolted flange joint was obtained in two ways. First, a 3D detailed finite element model capable of representing the micro-slip mechanism was made using a quasi-static time stepping analysis. The linear characteristics and nonlinear mechanisms developing in the contact interface of a bolted joint are investigated by using the 3D detailed model. Moreover, the natural frequencies of the assembled structure (representing the linear response) and the micro-slip behavior in terms of hysteresis loops (representing the nonlinear response) are obtained using the detailed model. Second, an equivalent model composed of beam elements and an appropriate joint model is then constructed for the assembled structure. An identification approach is proposed, and the parameters of the joint model are identified using both linear and nonlinear characteristics, i.e. natural frequencies and hysteresis loops. Comparing the hysteresis loops obtained from the detailed and equivalent models verifies the accuracy of the joint model used to represent the contact interface and the identification approach proposed for parameter quantification.</abstract><type>Journal Article</type><journal>Mechanical Systems and Signal Processing</journal><volume>153</volume><journalNumber/><paginationStart>107507</paginationStart><paginationEnd/><publisher>Elsevier BV</publisher><placeOfPublication/><isbnPrint/><isbnElectronic/><issnPrint>0888-3270</issnPrint><issnElectronic/><keywords>Bolted flange, Nonlinear analysis, Detailed model, Equivalent model</keywords><publishedDay>15</publishedDay><publishedMonth>5</publishedMonth><publishedYear>2021</publishedYear><publishedDate>2021-05-15</publishedDate><doi>10.1016/j.ymssp.2020.107507</doi><url/><notes/><college>COLLEGE NANME</college><department>Aerospace Engineering</department><CollegeCode>COLLEGE CODE</CollegeCode><DepartmentCode>AERO</DepartmentCode><institution>Swansea University</institution><apcterm/><funders>UKRI, EP/R006768/1</funders><projectreference/><lastEdited>2022-10-31T18:15:20.1421794</lastEdited><Created>2020-12-07T11:09:45.0212973</Created><path><level id="1">Faculty of Science and Engineering</level><level id="2">School of Engineering and Applied Sciences - Uncategorised</level></path><authors><author><firstname>Nidhal</firstname><surname>Jamia</surname><orcid>0000-0003-0643-7812</orcid><order>1</order></author><author><firstname>H.</firstname><surname>Jalali</surname><order>2</order></author><author><firstname>Javad</firstname><surname>Taghipour</surname><order>3</order></author><author><firstname>Michael</firstname><surname>Friswell</surname><order>4</order></author><author><firstname>Hamed</firstname><surname>Haddad Khodaparast</surname><orcid>0000-0002-3721-4980</orcid><order>5</order></author></authors><documents><document><filename>55840__18901__77a49f1e2e3e44a8beddf71b37ba5627.pdf</filename><originalFilename>55840.pdf</originalFilename><uploaded>2020-12-17T09:48:15.7104468</uploaded><type>Output</type><contentLength>4408721</contentLength><contentType>application/pdf</contentType><version>Version of Record</version><cronfaStatus>true</cronfaStatus><documentNotes>© 2020 Author(s). All article content, except where otherwise noted, is licensed under a Creative Commons Attribution 4.0 (CC BY) License</documentNotes><copyrightCorrect>true</copyrightCorrect><language>eng</language><licence>http://creativecommons.org/licenses/by/4.0/</licence></document></documents><OutputDurs/></rfc1807>
spelling	2022-10-31T18:15:20.1421794 v2 55840 2020-12-07 An equivalent model of a nonlinear bolted flange joint 846b2cd3a7717b296654010df30cb22a 0000-0003-0643-7812 Nidhal Jamia Nidhal Jamia true false dc7cba835218dde37fe7f447962d4058 Javad Taghipour Javad Taghipour true false 5894777b8f9c6e64bde3568d68078d40 Michael Friswell Michael Friswell true false f207b17edda9c4c3ea074cbb7555efc1 0000-0002-3721-4980 Hamed Haddad Khodaparast Hamed Haddad Khodaparast true false 2020-12-07 AERO The dynamic response of individual components in an assembled structure shows high accuracy compared to experimental measurements of the system response. However, when it comes to assemblies, the conventional linear approaches fail to deliver good accuracy, due to the uncertain linear and nonlinear mechanisms in the contact interface of the joints. Therefore, the inherent dynamics of the contact interfaces needs to be considered in modeling assembled structures. In this paper the prediction of the nonlinear dynamic response in a bolted flange joint was obtained in two ways. First, a 3D detailed finite element model capable of representing the micro-slip mechanism was made using a quasi-static time stepping analysis. The linear characteristics and nonlinear mechanisms developing in the contact interface of a bolted joint are investigated by using the 3D detailed model. Moreover, the natural frequencies of the assembled structure (representing the linear response) and the micro-slip behavior in terms of hysteresis loops (representing the nonlinear response) are obtained using the detailed model. Second, an equivalent model composed of beam elements and an appropriate joint model is then constructed for the assembled structure. An identification approach is proposed, and the parameters of the joint model are identified using both linear and nonlinear characteristics, i.e. natural frequencies and hysteresis loops. Comparing the hysteresis loops obtained from the detailed and equivalent models verifies the accuracy of the joint model used to represent the contact interface and the identification approach proposed for parameter quantification. Journal Article Mechanical Systems and Signal Processing 153 107507 Elsevier BV 0888-3270 Bolted flange, Nonlinear analysis, Detailed model, Equivalent model 15 5 2021 2021-05-15 10.1016/j.ymssp.2020.107507 COLLEGE NANME Aerospace Engineering COLLEGE CODE AERO Swansea University UKRI, EP/R006768/1 2022-10-31T18:15:20.1421794 2020-12-07T11:09:45.0212973 Faculty of Science and Engineering School of Engineering and Applied Sciences - Uncategorised Nidhal Jamia 0000-0003-0643-7812 1 H. Jalali 2 Javad Taghipour 3 Michael Friswell 4 Hamed Haddad Khodaparast 0000-0002-3721-4980 5 55840__18901__77a49f1e2e3e44a8beddf71b37ba5627.pdf 55840.pdf 2020-12-17T09:48:15.7104468 Output 4408721 application/pdf Version of Record true © 2020 Author(s). All article content, except where otherwise noted, is licensed under a Creative Commons Attribution 4.0 (CC BY) License true eng http://creativecommons.org/licenses/by/4.0/
title	An equivalent model of a nonlinear bolted flange joint
spellingShingle	An equivalent model of a nonlinear bolted flange joint Nidhal Jamia Javad Taghipour Michael Friswell Hamed Haddad Khodaparast
title_short	An equivalent model of a nonlinear bolted flange joint
title_full	An equivalent model of a nonlinear bolted flange joint
title_fullStr	An equivalent model of a nonlinear bolted flange joint
title_full_unstemmed	An equivalent model of a nonlinear bolted flange joint
title_sort	An equivalent model of a nonlinear bolted flange joint
author_id_str_mv	846b2cd3a7717b296654010df30cb22a dc7cba835218dde37fe7f447962d4058 5894777b8f9c6e64bde3568d68078d40 f207b17edda9c4c3ea074cbb7555efc1
author_id_fullname_str_mv	846b2cd3a7717b296654010df30cb22a_*_Nidhal Jamia dc7cba835218dde37fe7f447962d4058__Javad Taghipour 5894777b8f9c6e64bde3568d68078d40__Michael Friswell f207b17edda9c4c3ea074cbb7555efc1_*_Hamed Haddad Khodaparast
author	Nidhal Jamia Javad Taghipour Michael Friswell Hamed Haddad Khodaparast
author2	Nidhal Jamia H. Jalali Javad Taghipour Michael Friswell Hamed Haddad Khodaparast
format	Journal article
container_title	Mechanical Systems and Signal Processing
container_volume	153
container_start_page	107507
publishDate	2021
institution	Swansea University
issn	0888-3270
doi_str_mv	10.1016/j.ymssp.2020.107507
publisher	Elsevier BV
college_str	Faculty of Science and Engineering
hierarchytype
hierarchy_top_id	facultyofscienceandengineering
hierarchy_top_title	Faculty of Science and Engineering
hierarchy_parent_id	facultyofscienceandengineering
hierarchy_parent_title	Faculty of Science and Engineering
department_str	School of Engineering and Applied Sciences - Uncategorised{{{_:::_}}}Faculty of Science and Engineering{{{_:::_}}}School of Engineering and Applied Sciences - Uncategorised
document_store_str	1
active_str	0
description	The dynamic response of individual components in an assembled structure shows high accuracy compared to experimental measurements of the system response. However, when it comes to assemblies, the conventional linear approaches fail to deliver good accuracy, due to the uncertain linear and nonlinear mechanisms in the contact interface of the joints. Therefore, the inherent dynamics of the contact interfaces needs to be considered in modeling assembled structures. In this paper the prediction of the nonlinear dynamic response in a bolted flange joint was obtained in two ways. First, a 3D detailed finite element model capable of representing the micro-slip mechanism was made using a quasi-static time stepping analysis. The linear characteristics and nonlinear mechanisms developing in the contact interface of a bolted joint are investigated by using the 3D detailed model. Moreover, the natural frequencies of the assembled structure (representing the linear response) and the micro-slip behavior in terms of hysteresis loops (representing the nonlinear response) are obtained using the detailed model. Second, an equivalent model composed of beam elements and an appropriate joint model is then constructed for the assembled structure. An identification approach is proposed, and the parameters of the joint model are identified using both linear and nonlinear characteristics, i.e. natural frequencies and hysteresis loops. Comparing the hysteresis loops obtained from the detailed and equivalent models verifies the accuracy of the joint model used to represent the contact interface and the identification approach proposed for parameter quantification.
published_date	2021-05-15T04:10:20Z
_version_	1763753717426814976
score	10.997615

An equivalent model of a nonlinear bolted flange joint

Similar Items