Buckling analysis of laminated composite plates with a central hole in different geometric shapes
Yükleniyor...
Dosyalar
Tarih
2017
Yazarlar
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
Fırat Üniversitesi
Erişim Hakkı
info:eu-repo/semantics/openAccess
Attribution-NonCommercial-ShareAlike 3.0 United States
Attribution-NonCommercial-ShareAlike 3.0 United States
Özet
In this study, the buckling behaviors of E-glass/epoxy composite plates with a central hole in different
geometric shapes for different boundary conditions will be analyzed. For the analyzes, ratio between
thickness and length of the specimen (L/t = 20, 30, 40, 50) and two different laminae orientation angles
such as [0o
/90o
] 4 and [(0o
/90o
)2] S parameters will be considered. The buckling behavior of laminated
composite plates subjected to axial compressive load using a finite element method package program
such as ANSYS will be analyzed. The analyzes will be carried out for three different boundary conditions:
clamped-clamped support, clamped-fixed support and fixed-fixed support. Thus, the L/t ratio and laminae
orientation angle effects on the buckling behavior of composite plates for different boundary conditions
will be investigated. The obtained analyze results show that different L/t ratios and laminae orientation
angles have significant effects on the buckling load of composite plates. In additon, the hole shape also
affects the buckling load
Açıklama
Anahtar Kelimeler
Buckling Load, Laminated Composite Plate, Boundary Condition, Buckling Analyses
Kaynak
WoS Q Değeri
Scopus Q Değeri
Cilt
6
Sayı
Künye
Deniz, M.E. (2017). Buckling analysis of laminated composite plates with a central hole in different geometric shapes. 8th International Advanced Technologies Symposium, 19-22 October 2017, Elazığ, Turkey
