Publication: Design of curved composite panels for optimal dynamic response using lamination parameters
dc.contributor.department | Department of Mechanical Engineering | |
dc.contributor.department | Graduate School of Sciences and Engineering | |
dc.contributor.kuauthor | Başdoğan, İpek | |
dc.contributor.kuauthor | Serhat, Gökhan | |
dc.contributor.schoolcollegeinstitute | College of Engineering | |
dc.contributor.schoolcollegeinstitute | GRADUATE SCHOOL OF SCIENCES AND ENGINEERING | |
dc.date.accessioned | 2024-11-09T23:59:13Z | |
dc.date.issued | 2018 | |
dc.description.abstract | In this paper, dynamic response of composite panels is investigated using lamination parameters as design variables. Finite element analyses are performed to observe the individual and combined effects of different panel aspect ratios, curvatures and boundary conditions on the dynamic responses. Fundamental frequency contours for curved panels are obtained in lamination parameters domain and optimal points yielding maximum values are found. Subsequently, forced dynamic analyses are carried out to calculate equivalent radiated power (ERP) for the panels under harmonic pressure excitation. ERP contours at the maximum fundamental frequency are presented. Optimal lamination parameters providing minimum ERP are determined for different excitation frequencies and their effective frequency bands are shown. The relationship between the designs optimized for maximum fundamental frequency and minimum ERP responses is investigated to study the effectiveness of the frequency maximization technique. The results demonstrate the potential of using lamination parameters technique in the design of curved composite panels for optimal dynamic response and provide valuable insight on the effect of various design parameters. | |
dc.description.indexedby | WOS | |
dc.description.indexedby | Scopus | |
dc.description.openaccess | NO | |
dc.description.sponsoredbyTubitakEu | EU | |
dc.description.sponsorship | European Union [316394] The authors would like to gratefully acknowledge the funding from European Union Seventh Framework Programme "FP7-PEOPLE-2012-ITN" under grant agreement 316394, through the Marie Curie Initial Training Network "Aerospace Multidisciplinarity Enabling DEsign Optimization (AMEDEO)". | |
dc.description.volume | 147 | |
dc.identifier.doi | 10.1016/j.compositesb.2018.04.033 | |
dc.identifier.eissn | 1879-1069 | |
dc.identifier.issn | 1359-8368 | |
dc.identifier.scopus | 2-s2.0-85045691095 | |
dc.identifier.uri | https://doi.org/10.1016/j.compositesb.2018.04.033 | |
dc.identifier.uri | https://hdl.handle.net/20.500.14288/15591 | |
dc.identifier.wos | 437064900015 | |
dc.keywords | Optimization | |
dc.keywords | Curved composite panels | |
dc.keywords | Vibration | |
dc.keywords | Fundamental frequency | |
dc.keywords | Equivalent radiated power | |
dc.keywords | Lamination parameters | |
dc.keywords | Maximum fundamental-frequency | |
dc.keywords | Forced vibration analysis | |
dc.keywords | Plates | |
dc.keywords | Optimization | |
dc.keywords | Maximization | |
dc.keywords | Behavior | |
dc.keywords | Shells | |
dc.language.iso | eng | |
dc.publisher | Elsevier Sci Ltd | |
dc.relation.ispartof | Composites Part B-Engineering | |
dc.subject | Engineering | |
dc.subject | Materials sciences | |
dc.subject | Composite materials | |
dc.title | Design of curved composite panels for optimal dynamic response using lamination parameters | |
dc.type | Journal Article | |
dspace.entity.type | Publication | |
local.contributor.kuauthor | Serhat, Gökhan | |
local.contributor.kuauthor | Başdoğan, İpek | |
local.publication.orgunit1 | GRADUATE SCHOOL OF SCIENCES AND ENGINEERING | |
local.publication.orgunit1 | College of Engineering | |
local.publication.orgunit2 | Department of Mechanical Engineering | |
local.publication.orgunit2 | Graduate School of Sciences and Engineering | |
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