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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...
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Published in: | Computers and geotechnics 2021-09, Vol.137, p.104174, Article 104174 |
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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 |
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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. 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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 & Fisheries Abstracts (ASFA) 2: Ocean Technology, Policy & Non-Living Resources</collection><collection>ProQuest Computer Science Collection</collection><collection>Civil Engineering Abstracts</collection><collection>Aquatic Science & 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. 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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 |
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