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dc.contributor.authorGÜLBAHÇE, ERDİ
dc.contributor.authorSEZGEN, HAŞMET ÇAĞRI
dc.contributor.authorÇAKAN, ABDULLAH
dc.date.accessioned2021-01-12T08:48:34Z
dc.date.available2021-01-12T08:48:34Z
dc.date.issued2019-09-30
dc.identifier.issn2466-4677
dc.identifier.urihttp://hdl.handle.net/20.500.12498/4876
dc.description.abstractIn this study, topology optimization of a jet engine bracket which was proposed from GE Aviation challenge for improving the brackets is presented using finite element analysis (FEA). The minimum mass, maximum equivalent stress and first natural frequency are selected for the objective functions to topology optimization. Then, topology optimization procedure is implemented according to the identified boundary conditions and objective functions. Finally, the manufacturing model is obtained and compared with the original model according to the maximum equivalent stress, mass reduction and first natural frequency. Also, modal analysis and static analysis results of the proposed models are presenteden_US
dc.language.isoenen_US
dc.publisherApplied Engineering Letters : Journal of Engineering and Applied Sciencesen_US
dc.rightsAttribution 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by/3.0/us/*
dc.subjectmechanical engineeringen_US
dc.titleTopology Design and Modal Analysis of a Bracket via FEAen_US
dc.typeArticleen_US


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Attribution 3.0 United States
Except where otherwise noted, this item's license is described as Attribution 3.0 United States