Atıf İçin Kopyala
SÜSLER S., Kurtaran H., Türkmen H. S., Kazanci Z., Lopresto V.
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, cilt.27, sa.6, ss.441-454, 2020 (SCI-Expanded)
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Yayın Türü:
Makale / Tam Makale
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Cilt numarası:
27
Sayı:
6
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Basım Tarihi:
2020
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Doi Numarası:
10.1080/15376494.2018.1478049
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Dergi Adı:
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES
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Derginin Tarandığı İndeksler:
Science Citation Index Expanded (SCI-EXPANDED), Scopus, Academic Search Premier, Aerospace Database, Communication Abstracts, Compendex, INSPEC, Metadex, DIALNET, Civil Engineering Abstracts
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Sayfa Sayıları:
ss.441-454
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Anahtar Kelimeler:
Basalt, experimental mechanics, laminated composite plate, first-order shear deformation, computational modeling, blast load, dynamic response, generalized differential quadrature, large deflection, shock tube, NONLINEAR DYNAMIC-BEHAVIOR, DIFFERENTIAL QUADRATURE, LAMINATED PLATES, STATIC ANALYSIS, ELEMENT-METHOD, VIBRATION, SHELLS, PANELS
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İstanbul Teknik Üniversitesi Adresli:
Evet
Özet
Nonlinear air blast response of basalt composite plates is analysed by using a generalized differential quadrature (GDQ) method, which requires less solution time and decreases the complexity compared to finite element method. A test environment that contains a shock tube is designed and set to experiment on the transient response of blast loaded laminated plates. Experimental and numerical results show a good agreement in terms of displacement, strain, and acceleration versus time. The responses of glass/epoxy, Kevlar/epoxy, and carbon/epoxy composite plates are also investigated by using GDQ method and the results are compared with the basalt/epoxy composite plate and discussed.