dc.contributor.author | GÜLBAHÇE, Erdi | |
dc.contributor.author | SEZGEN, Haşmet Çağrı | |
dc.contributor.author | ÇAKAN, Abdullah | |
dc.date.accessioned | 2021-01-12T08:48:34Z | |
dc.date.available | 2021-01-12T08:48:34Z | |
dc.date.issued | 2019-09-30 | |
dc.identifier.issn | 2466-4677 | |
dc.identifier.uri | http://hdl.handle.net/20.500.12498/4876 | |
dc.description.abstract | In 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 presented | en_US |
dc.language.iso | en | en_US |
dc.publisher | Applied Engineering Letters : Journal of Engineering and Applied Sciences | en_US |
dc.rights | Attribution 3.0 United States | * |
dc.rights.uri | http://creativecommons.org/licenses/by/3.0/us/ | * |
dc.subject | Mechanical Engineering | en_US |
dc.title | Topology Design and Modal Analysis of a Bracket via FEA | en_US |
dc.type | Makale | en_US |