Effect of hole geometry and matrix material on buckling behavior of composite plates
Yükleniyor...
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 behavior of E-glass/epoxy, E-glass/polyester and E-glass/vinylester based
composite plates with fiber orientation of [0o
/90o
] 4 will be determined experimentally. Test specimens
prepared according to the ASTM standards. All buckling tests were performed using a Shimadzu brand
tensile machine with load capacity of ± 250 kN. Some of the specimens consist hole and some do not. The
specimens with hole have different geometrical shapes and also same hole area. The specimens were
subjected to axial compressive load until buckling failure occurred. From the obtained test results, it was
shown that the hole geometry and matrix materials have significant effects on the buckling load of the
laminated composite plates.
Açıklama
Anahtar Kelimeler
Buckling Load, Laminated Composite Plate, Matrix Material, Hole Geometry
Kaynak
WoS Q Değeri
Scopus Q Değeri
Cilt
6
Sayı
Künye
Deniz, M.E. (2017). Effect of hole geometry and matrix material on buckling behavior of composite plates. 8th International Advanced Technologies Symposium, 19-22 October 2017, Elazığ, Turkey
