Curvilinear free-edge form effect on stability of perforated laminated composite plates
Yazarlar (3)
Prof. Dr. Zihni Zerin Ondokuz Mayıs Üniversitesi, Türkiye
Dr. Öğr. Üyesi Muhammed Fatih BAŞOĞLU Ondokuz Mayıs Üniversitesi, Türkiye
Dr. Öğr. Üyesi Ferruh Turan Ondokuz Mayıs Üniversitesi, Türkiye
Makale Türü Özgün Makale (SSCI, AHCI, SCI, SCI-Exp dergilerinde yayınlanan tam makale)
Dergi Adı Structural Engineering and Mechanics (Q2)
Dergi ISSN 1225-4568 Wos Dergi Scopus Dergi
Dergi Tarandığı Indeksler SCI-Expanded
Makale Dili İngilizce Basım Tarihi 01-2017
Cilt / Sayı / Sayfa 61 / 2 / 255–266 DOI 10.12989/sem.2017.61.2.255
Makale Linki http://dx.doi.org/10.12989/sem.2017.61.2.255
UAK Araştırma Alanları
Katı Cisimler Mekaniği
Özet
In this study, self-supporting roofing elements especially convenient for large-span structures such as stadium, airport terminal, mall, coliseum, etc. were examined with respect to critical buckling load. These elements were assumed as laminated composite plates and, variation of free-edge forms, cutout types and lamination configurations were used as design parameters. Based on the architectural feature and structural requirements, the effects of curvilinear free-edge form on critical buckling load were focused on in this research. Within this scope, 14 types of lamination configuration were specified according to various orientation angle, number and thickness of plies with a constant value of total plate thickness. Besides that, 6 different types of cutout and 3 different free-edge forms were determined. By combining all these parameters 294 different critical buckling load analyses were performed by using ANSYS …
Anahtar Kelimeler
Curvilinear free-edge | Finite element method | Laminated composite plate | Plate with cutout | Self-supporting | Stability
BM Sürdürülebilir Kalkınma Amaçları
Atıf Sayıları
Web of Science 1
Scopus 1
Google Scholar 2
Curvilinear free-edge form effect on stability of perforated laminated composite plates

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