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dc.contributor.authorXue, Hui
dc.contributor.authorKhawaja, Hassan Abbas
dc.contributor.authorMoatamedi, Mojtaba
dc.date.accessioned2014-12-18T08:17:44Z
dc.date.available2014-12-18T08:17:44Z
dc.date.issued2014
dc.description.abstractThis paper presents the Multiphysics technique applied in the design optimization of a loading hanger for an aerial crane. In this study, design optimization is applied on the geometric modelling of a part being used in an aerial crane operation. A set of dimensional and loading requirements are provided. Various geometric models are built using SolidWorks® Computer Aided Design (CAD) Package. In addition, Finite Element Method (FEM) is applied to study these geometric models using ANSYS® Multiphysics package. Appropriate material is chosen based on the strength to weight ratio. Efforts are made to optimize the geometry to reduce the weight of the part. Based on the achieved results, conclusions are drawn.en
dc.identifier.citationAIP Conference Proceedings, 1637, 1211 (2014)en
dc.identifier.cristinIDFRIDAID 1184846
dc.identifier.doi10.1063/1.490469
dc.identifier.issn0094-243X
dc.identifier.urihttps://hdl.handle.net/10037/6953
dc.identifier.urnURN:NBN:no-uit_munin_6552
dc.language.isoengen
dc.publisherAmerican Institute of Physics (AIP)en
dc.rights.accessRightsopenAccess
dc.subjectVDP::Teknologi: 500::Maskinfag: 570::Maskinkonstruksjon og materialteknologi: 571en
dc.subjectVDP::Technology: 500::Mechanical engineering: 570::Machine construction and engineering technology: 571en
dc.titleMultiphysics design optimization for aerospace applications: Case study on helicopter loading hangeren
dc.typeJournal articleen
dc.typeTidsskriftartikkelen
dc.typePeer revieweden


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