Loading…

Automated procedure to derive convex failure envelope formulations for circular surface foundations under six degrees of freedom loading

Failure envelope formulations are typically employed to assess the ultimate capacity of foundations under combined loading and for incorporation in macro-element models. However, the complex interaction between each load component, especially for six degree of freedom (6DoF) loading, means that dete...

Full description

Saved in:
Bibliographic Details
Published in:Computers and geotechnics 2021-09, Vol.137, p.104174, Article 104174
Main Authors: Suryasentana, Stephen K., Burd, Harvey J., Byrne, Byron W., Shonberg, Avi
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-c314t-109f3f8cb6ee8e4fef08448fb33a551e8863d9efce4f46a743ea43d75d11d6c23
cites cdi_FETCH-LOGICAL-c314t-109f3f8cb6ee8e4fef08448fb33a551e8863d9efce4f46a743ea43d75d11d6c23
container_end_page
container_issue
container_start_page 104174
container_title Computers and geotechnics
container_volume 137
creator Suryasentana, Stephen K.
Burd, Harvey J.
Byrne, Byron W.
Shonberg, Avi
description Failure envelope formulations are typically employed to assess the ultimate capacity of foundations under combined loading and for incorporation in macro-element models. However, the complex interaction between each load component, especially for six degree of freedom (6DoF) loading, means that determining satisfactory formulations is often a complex process. Previous researchers have identified this difficulty as an obstacle to the adoption of the failure envelope approach in foundation engineering applications. To address this issue, the paper describes a systematic procedure for deriving globally convex failure envelope formulations; the procedure is applied to a circular surface foundation, bearing on undrained clay, in 6DoF load space. The formulations are shown to closely represent the failure load combinations determined from finite element analyses for a variety of loading conditions, including non-planar horizontal-moment loading. An example macro-element model based on the proposed formulation is described; the macro-element model provides a close representation of the foundation behaviour determined from a separate finite element analysis. A key aspect of the paper is that it demonstrates an automated process to determine well-behaved failure envelope formulations. The automated nature of the process has considerable advantages over the manual procedures that have previously been employed to determine failure envelope formulations.
doi_str_mv 10.1016/j.compgeo.2021.104174
format article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2564174247</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0266352X21001786</els_id><sourcerecordid>2564174247</sourcerecordid><originalsourceid>FETCH-LOGICAL-c314t-109f3f8cb6ee8e4fef08448fb33a551e8863d9efce4f46a743ea43d75d11d6c23</originalsourceid><addsrcrecordid>eNqFkM9KxDAQxoMouK4-ghDw3LVp0jQ9ybL4Dxa8KHgL2WSypLTNmrSLvoGPbUr37ikz833zhfkhdEvyFckJv29W2neHPfhVkRckzRip2BlaEFHRrOKUnqNFXnCe0bL4vERXMTZ52qtFvUC_63HwnRrA4EPwGswYAA8eGwjuCFj7_gjf2CrXTgKkrvUHwNaHbmzV4HwfpwZrF3QaBBzHYJWeHGNvToZUQVLcd4rdB4CIvcU2FcZ3uPXKuH5_jS6saiPcnN4l-nh6fN-8ZNu359fNeptpStiQkby21Aq94wACmAWbC8aE3VGqypKAEJyaGqxOGuOqYhQUo6YqDSGG64Iu0d2cm879GiEOsvFj6NOXsij5RK5gVXKVs0sHH2MAKw_BdSr8SJLLCbps5Am6nKDLGXrae5j3IJ1wdBBk1A76xNUF0IM03v2T8Af8zJGp</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2564174247</pqid></control><display><type>article</type><title>Automated procedure to derive convex failure envelope formulations for circular surface foundations under six degrees of freedom loading</title><source>ScienceDirect Freedom Collection</source><creator>Suryasentana, Stephen K. ; Burd, Harvey J. ; Byrne, Byron W. ; Shonberg, Avi</creator><creatorcontrib>Suryasentana, Stephen K. ; Burd, Harvey J. ; Byrne, Byron W. ; Shonberg, Avi</creatorcontrib><description>Failure envelope formulations are typically employed to assess the ultimate capacity of foundations under combined loading and for incorporation in macro-element models. However, the complex interaction between each load component, especially for six degree of freedom (6DoF) loading, means that determining satisfactory formulations is often a complex process. Previous researchers have identified this difficulty as an obstacle to the adoption of the failure envelope approach in foundation engineering applications. To address this issue, the paper describes a systematic procedure for deriving globally convex failure envelope formulations; the procedure is applied to a circular surface foundation, bearing on undrained clay, in 6DoF load space. The formulations are shown to closely represent the failure load combinations determined from finite element analyses for a variety of loading conditions, including non-planar horizontal-moment loading. An example macro-element model based on the proposed formulation is described; the macro-element model provides a close representation of the foundation behaviour determined from a separate finite element analysis. A key aspect of the paper is that it demonstrates an automated process to determine well-behaved failure envelope formulations. The automated nature of the process has considerable advantages over the manual procedures that have previously been employed to determine failure envelope formulations.</description><identifier>ISSN: 0266-352X</identifier><identifier>EISSN: 1873-7633</identifier><identifier>DOI: 10.1016/j.compgeo.2021.104174</identifier><language>eng</language><publisher>New York: Elsevier Ltd</publisher><subject>Automation ; Bearing capacity ; Combined loading ; Degrees of freedom ; Failure ; Failure analysis ; Failure load ; Finite element method ; Foundations ; Mathematical models ; Numerical modelling ; Offshore engineering ; Procedures ; Soil-structure interaction</subject><ispartof>Computers and geotechnics, 2021-09, Vol.137, p.104174, Article 104174</ispartof><rights>2021 Elsevier Ltd</rights><rights>Copyright Elsevier BV Sep 2021</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c314t-109f3f8cb6ee8e4fef08448fb33a551e8863d9efce4f46a743ea43d75d11d6c23</citedby><cites>FETCH-LOGICAL-c314t-109f3f8cb6ee8e4fef08448fb33a551e8863d9efce4f46a743ea43d75d11d6c23</cites><orcidid>0000-0001-5460-5089</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,778,782,27911,27912</link.rule.ids></links><search><creatorcontrib>Suryasentana, Stephen K.</creatorcontrib><creatorcontrib>Burd, Harvey J.</creatorcontrib><creatorcontrib>Byrne, Byron W.</creatorcontrib><creatorcontrib>Shonberg, Avi</creatorcontrib><title>Automated procedure to derive convex failure envelope formulations for circular surface foundations under six degrees of freedom loading</title><title>Computers and geotechnics</title><description>Failure envelope formulations are typically employed to assess the ultimate capacity of foundations under combined loading and for incorporation in macro-element models. However, the complex interaction between each load component, especially for six degree of freedom (6DoF) loading, means that determining satisfactory formulations is often a complex process. Previous researchers have identified this difficulty as an obstacle to the adoption of the failure envelope approach in foundation engineering applications. To address this issue, the paper describes a systematic procedure for deriving globally convex failure envelope formulations; the procedure is applied to a circular surface foundation, bearing on undrained clay, in 6DoF load space. The formulations are shown to closely represent the failure load combinations determined from finite element analyses for a variety of loading conditions, including non-planar horizontal-moment loading. An example macro-element model based on the proposed formulation is described; the macro-element model provides a close representation of the foundation behaviour determined from a separate finite element analysis. A key aspect of the paper is that it demonstrates an automated process to determine well-behaved failure envelope formulations. The automated nature of the process has considerable advantages over the manual procedures that have previously been employed to determine failure envelope formulations.</description><subject>Automation</subject><subject>Bearing capacity</subject><subject>Combined loading</subject><subject>Degrees of freedom</subject><subject>Failure</subject><subject>Failure analysis</subject><subject>Failure load</subject><subject>Finite element method</subject><subject>Foundations</subject><subject>Mathematical models</subject><subject>Numerical modelling</subject><subject>Offshore engineering</subject><subject>Procedures</subject><subject>Soil-structure interaction</subject><issn>0266-352X</issn><issn>1873-7633</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNqFkM9KxDAQxoMouK4-ghDw3LVp0jQ9ybL4Dxa8KHgL2WSypLTNmrSLvoGPbUr37ikz833zhfkhdEvyFckJv29W2neHPfhVkRckzRip2BlaEFHRrOKUnqNFXnCe0bL4vERXMTZ52qtFvUC_63HwnRrA4EPwGswYAA8eGwjuCFj7_gjf2CrXTgKkrvUHwNaHbmzV4HwfpwZrF3QaBBzHYJWeHGNvToZUQVLcd4rdB4CIvcU2FcZ3uPXKuH5_jS6saiPcnN4l-nh6fN-8ZNu359fNeptpStiQkby21Aq94wACmAWbC8aE3VGqypKAEJyaGqxOGuOqYhQUo6YqDSGG64Iu0d2cm879GiEOsvFj6NOXsij5RK5gVXKVs0sHH2MAKw_BdSr8SJLLCbps5Am6nKDLGXrae5j3IJ1wdBBk1A76xNUF0IM03v2T8Af8zJGp</recordid><startdate>202109</startdate><enddate>202109</enddate><creator>Suryasentana, Stephen K.</creator><creator>Burd, Harvey J.</creator><creator>Byrne, Byron W.</creator><creator>Shonberg, Avi</creator><general>Elsevier Ltd</general><general>Elsevier BV</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7UA</scope><scope>8FD</scope><scope>C1K</scope><scope>F1W</scope><scope>FR3</scope><scope>H96</scope><scope>JQ2</scope><scope>KR7</scope><scope>L.G</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><orcidid>https://orcid.org/0000-0001-5460-5089</orcidid></search><sort><creationdate>202109</creationdate><title>Automated procedure to derive convex failure envelope formulations for circular surface foundations under six degrees of freedom loading</title><author>Suryasentana, Stephen K. ; Burd, Harvey J. ; Byrne, Byron W. ; Shonberg, Avi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c314t-109f3f8cb6ee8e4fef08448fb33a551e8863d9efce4f46a743ea43d75d11d6c23</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Automation</topic><topic>Bearing capacity</topic><topic>Combined loading</topic><topic>Degrees of freedom</topic><topic>Failure</topic><topic>Failure analysis</topic><topic>Failure load</topic><topic>Finite element method</topic><topic>Foundations</topic><topic>Mathematical models</topic><topic>Numerical modelling</topic><topic>Offshore engineering</topic><topic>Procedures</topic><topic>Soil-structure interaction</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Suryasentana, Stephen K.</creatorcontrib><creatorcontrib>Burd, Harvey J.</creatorcontrib><creatorcontrib>Byrne, Byron W.</creatorcontrib><creatorcontrib>Shonberg, Avi</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Water Resources Abstracts</collection><collection>Technology Research Database</collection><collection>Environmental Sciences and Pollution Management</collection><collection>ASFA: Aquatic Sciences and Fisheries Abstracts</collection><collection>Engineering Research Database</collection><collection>Aquatic Science &amp; Fisheries Abstracts (ASFA) 2: Ocean Technology, Policy &amp; Non-Living Resources</collection><collection>ProQuest Computer Science Collection</collection><collection>Civil Engineering Abstracts</collection><collection>Aquatic Science &amp; Fisheries Abstracts (ASFA) Professional</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts – Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>Computers and geotechnics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Suryasentana, Stephen K.</au><au>Burd, Harvey J.</au><au>Byrne, Byron W.</au><au>Shonberg, Avi</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Automated procedure to derive convex failure envelope formulations for circular surface foundations under six degrees of freedom loading</atitle><jtitle>Computers and geotechnics</jtitle><date>2021-09</date><risdate>2021</risdate><volume>137</volume><spage>104174</spage><pages>104174-</pages><artnum>104174</artnum><issn>0266-352X</issn><eissn>1873-7633</eissn><abstract>Failure envelope formulations are typically employed to assess the ultimate capacity of foundations under combined loading and for incorporation in macro-element models. However, the complex interaction between each load component, especially for six degree of freedom (6DoF) loading, means that determining satisfactory formulations is often a complex process. Previous researchers have identified this difficulty as an obstacle to the adoption of the failure envelope approach in foundation engineering applications. To address this issue, the paper describes a systematic procedure for deriving globally convex failure envelope formulations; the procedure is applied to a circular surface foundation, bearing on undrained clay, in 6DoF load space. The formulations are shown to closely represent the failure load combinations determined from finite element analyses for a variety of loading conditions, including non-planar horizontal-moment loading. An example macro-element model based on the proposed formulation is described; the macro-element model provides a close representation of the foundation behaviour determined from a separate finite element analysis. A key aspect of the paper is that it demonstrates an automated process to determine well-behaved failure envelope formulations. The automated nature of the process has considerable advantages over the manual procedures that have previously been employed to determine failure envelope formulations.</abstract><cop>New York</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.compgeo.2021.104174</doi><orcidid>https://orcid.org/0000-0001-5460-5089</orcidid><oa>free_for_read</oa></addata></record>
fulltext fulltext
identifier ISSN: 0266-352X
ispartof Computers and geotechnics, 2021-09, Vol.137, p.104174, Article 104174
issn 0266-352X
1873-7633
language eng
recordid cdi_proquest_journals_2564174247
source ScienceDirect Freedom Collection
subjects Automation
Bearing capacity
Combined loading
Degrees of freedom
Failure
Failure analysis
Failure load
Finite element method
Foundations
Mathematical models
Numerical modelling
Offshore engineering
Procedures
Soil-structure interaction
title Automated procedure to derive convex failure envelope formulations for circular surface foundations under six degrees of freedom loading
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-15T21%3A28%3A52IST&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=Automated%20procedure%20to%20derive%20convex%20failure%20envelope%20formulations%20for%20circular%20surface%20foundations%20under%20six%20degrees%20of%20freedom%20loading&rft.jtitle=Computers%20and%20geotechnics&rft.au=Suryasentana,%20Stephen%20K.&rft.date=2021-09&rft.volume=137&rft.spage=104174&rft.pages=104174-&rft.artnum=104174&rft.issn=0266-352X&rft.eissn=1873-7633&rft_id=info:doi/10.1016/j.compgeo.2021.104174&rft_dat=%3Cproquest_cross%3E2564174247%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c314t-109f3f8cb6ee8e4fef08448fb33a551e8863d9efce4f46a743ea43d75d11d6c23%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=2564174247&rft_id=info:pmid/&rfr_iscdi=true