Effects of nonuniform boundary conditions on the buckling load optimization of laminated composite plates
MakaleYalnız künye
Özet
This paper deals with buckling load optimization of symmetrically laminated composite thin plates under the uniaxial and biaxial compressive loads with discontinuities along the boundaries. The objective of the design problem is to maximize the buckling load of the laminated plates and the fibre orientation is taken as design variable. The classical laminate plate theory is used for the mathematical formulations of the laminates. The modified feasible direction method is used as optimization routine. Therefore a program based on FORTRAN is used. Finally, the effect of nonuniform boundary conditions, aspect ratios and load ratios on the optimum results is illustrated.
Anahtar Kelimeler
RDL Kalıcı Bağlantı (PID)
https://rdlopen.rawdatalibrary.net/r/gumushane/14713Resmi atıflarda kullanılan kalıcı adresTam Kayıt
| Alan | Değer | Dil |
|---|---|---|
| dc.contributor.author | Topal, Umut | |
| dc.contributor.author | Uzman, Ümit | |
| dc.date.accessioned | 2026-10-22T10:23:02.629453620Z | |
| dc.date.available | 2026-10-22T10:23:02.629453620Z | |
| dc.date.issued | 2009 | |
| dc.description.abstract | This paper deals with buckling load optimization of symmetrically laminated composite thin plates under the uniaxial and biaxial compressive loads with discontinuities along the boundaries. The objective of the design problem is to maximize the buckling load of the laminated plates and the fibre orientation is taken as design variable. The classical laminate plate theory is used for the mathematical formulations of the laminates. The modified feasible direction method is used as optimization routine. Therefore a program based on FORTRAN is used. Finally, the effect of nonuniform boundary conditions, aspect ratios and load ratios on the optimum results is illustrated. | |
| dc.identifier.doi | 10.1016/j.matdes.2008.05.012 | |
| dc.identifier.endpage | 717 | |
| dc.identifier.issn | 0264-1275 | |
| dc.identifier.issue | 3 | |
| dc.identifier.scopus | 2-s2.0-57149086889 | |
| dc.identifier.startpage | 710 | |
| dc.identifier.uri | https://rdlopen.rawdatalibrary.net/r/gumushane/14713 | |
| dc.identifier.volume | 30 | |
| dc.language.iso | en | |
| dc.relation.ispartof | Materials and Design | |
| dc.rights | info:eu-repo/semantics/closedAccess | |
| dc.subject | B. Laminates | |
| dc.subject | E. Mechanical | |
| dc.subject | I. Buckling | |
| dc.subject.other | Aspect ratio | |
| dc.subject.other | Boundary conditions | |
| dc.subject.other | Boundary value problems | |
| dc.subject.other | Electric load management | |
| dc.subject.other | Laminated composites | |
| dc.subject.other | Laminates | |
| dc.subject.other | Laminating | |
| dc.subject.other | Optimization | |
| dc.subject.other | B. Laminates | |
| dc.subject.other | Buckling loads | |
| dc.subject.other | Compressive loads | |
| dc.subject.other | Design problems | |
| dc.subject.other | Design variables | |
| dc.subject.other | E. Mechanical | |
| dc.subject.other | Fibre orientations | |
| dc.subject.other | Fortrans | |
| dc.subject.other | I. Buckling | |
| dc.subject.other | Laminate plate theories | |
| dc.subject.other | Laminated composite plates | |
| dc.subject.other | Laminated plates | |
| dc.subject.other | Load ratios | |
| dc.subject.other | Mathematical formulations | |
| dc.subject.other | Modified feasible direction methods | |
| dc.subject.other | Nonuniform boundary conditions | |
| dc.subject.other | Optimization routines | |
| dc.subject.other | Thin plates | |
| dc.subject.other | Buckling | |
| dc.title | Effects of nonuniform boundary conditions on the buckling load optimization of laminated composite plates | |
| dc.type | Article | |
| dspace.entity.type | Publication | |
| rdl.citation.scopus | 12 | |
| rdl.oa.status | closed | |
| rdl.source.index | SCOPUS |
