Please use this identifier to cite or link to this item: https://doi.org/10.15480/882.1708
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dc.contributor.authorKriegesmann, Benedikt-
dc.contributor.authorJansen, Eelco Luc-
dc.contributor.authorRolfes, Raimund-
dc.date.accessioned2018-07-11T09:39:07Z-
dc.date.available2018-07-11T09:39:07Z-
dc.date.issued2016-11-
dc.identifier.citationThin-Walled Structures (108) : 369-380 (2016)de_DE
dc.identifier.issn1879-3223de_DE
dc.identifier.urihttp://tubdok.tub.tuhh.de/handle/11420/1711-
dc.description.abstractThe Single Perturbation Load Approach (SPLA) is a promising deterministic procedure on the basis of mechanical considerations to determine reasonable design loads for cylindrical shells in axial compression. In this paper, two main issues are identified that should be understood better in order to appreciate the potential and the limits of application of the SPLA. Firstly, the question whether a single perturbation load in general represents a “worst case” imperfection is addressed. Secondly, the influence of the stiffness properties of the shell on the quality of the SPLA predictions is studied. Finally, an indicator is suggested which identifies, based on the cylinder stiffness properties, whether the SPLA is conservative for a considered shell or not.en
dc.language.isoen_USde_DE
dc.publisherElsevierde_DE
dc.relationinfo:eu-repo/grantAgreement/EC/FP7/282522-
dc.relation.ispartofThin-walled structuresde_DE
dc.rightsinfo:eu-repo/semantics/openAccessde_DE
dc.rightsinfo:eu-repo/semantics/embargoedAccess-
dc.subjectbucklingde_DE
dc.subjectshell structuresde_DE
dc.subjectsingle perturbation load approachde_DE
dc.subject.ddc620: Ingenieurwissenschaftende_DE
dc.titleDesign of cylindrical shells using the single perturbation load approach : potentials and application limitsde_DE
dc.typeArticlede_DE
dc.identifier.urnurn:nbn:de:gbv:830-88221753-
dc.identifier.doi10.15480/882.1708-
dc.type.diniarticle-
dc.subject.ddccode620-
dcterms.DCMITypeText-
tuhh.identifier.urnurn:nbn:de:gbv:830-88221753de_DE
tuhh.oai.showtrue-
dc.identifier.hdl11420/1711-
tuhh.abstract.englishThe Single Perturbation Load Approach (SPLA) is a promising deterministic procedure on the basis of mechanical considerations to determine reasonable design loads for cylindrical shells in axial compression. In this paper, two main issues are identified that should be understood better in order to appreciate the potential and the limits of application of the SPLA. Firstly, the question whether a single perturbation load in general represents a “worst case” imperfection is addressed. Secondly, the influence of the stiffness properties of the shell on the quality of the SPLA predictions is studied. Finally, an indicator is suggested which identifies, based on the cylinder stiffness properties, whether the SPLA is conservative for a considered shell or not.de_DE
tuhh.publisher.doi10.1016/j.tws.2016.09.005-
tuhh.publication.instituteStrukturoptimierung im Leichtbau M-EXK1de_DE
tuhh.identifier.doi10.15480/882.1708-
tuhh.type.opus(wissenschaftlicher) Artikelde
tuhh.institute.germanNeue Entwurfs- u. Berechnungsmethoden für hybride Flugzeugstrukturen M-EXK1de
tuhh.institute.englishStrukturoptimierung im Leichtbau M-EXK1de_DE
tuhh.gvk.hasppnfalse-
tuhh.hasurnfalse-
openaire.rightsinfo:eu-repo/semantics/embargoedAccessde_DE
openaire.funder.nameECde_DE
openaire.funder.programmeFP7de_DE
openaire.funder.projectid282522de_DE
dc.type.driverarticle-
dc.rights.ccby-nc-ndde_DE
dc.rights.ccversion4.0de_DE
dc.type.casraiJournal Articleen
tuhh.embargo.date01.12.2018-
tuhh.container.volume108de_DE
tuhh.container.startpage369de_DE
tuhh.container.endpage380de_DE
dc.rights.nationallicensefalsede_DE
item.fulltextWith Fulltext-
item.creatorOrcidKriegesmann, Benedikt-
item.creatorOrcidJansen, Eelco Luc-
item.creatorOrcidRolfes, Raimund-
item.creatorGNDKriegesmann, Benedikt-
item.creatorGNDJansen, Eelco Luc-
item.creatorGNDRolfes, Raimund-
item.grantfulltextopen-
crisitem.author.deptStrukturoptimierung im Leichtbau M-EXK1-
crisitem.author.orcid0000-0001-5330-9886-
crisitem.author.orcid0000-0001-7714-3382-
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