Vibration analysis of thick arbitrarily laminated plates of various shapes and edge conditions

T. Pervez*, F. K.S. Al-Jahwari, A. C. Seibi

*المؤلف المقابل لهذا العمل

نتاج البحث: Conference contribution

ملخص

Free vibration analysis of arbitrarily laminated plates of quad, penta and hexagonal shapes, which have combinations of clamped, simply supported and free edge conditions is performed. The finite element formulation is based on first and higher order shear deformation theories to study the free vibration response of thick laminated composite plates. A finite element code is developed incorporating shear deformation theories using an 8-noded serendipity element. The effect of plate shape, arbitrary lamination and different edge conditions on natural frequencies and mode shapes are investigated. A systematic study is carried out to determine the influence of material orthotropy and aspect ratio on free vibration response. For various cases, the comparisons of results from present study showed good agreement with those published in the literature.

اللغة الأصليةEnglish
عنوان منشور المضيفComposite Science and Technology
ناشرTrans Tech Publications Ltd
الصفحات1177-1183
عدد الصفحات7
رقم المعيار الدولي للكتب (المطبوع)9783037850596
المعرِّفات الرقمية للأشياء
حالة النشرPublished - 2011

سلسلة المنشورات

الاسمKey Engineering Materials
مستوى الصوت471-472
رقم المعيار الدولي للدوريات (المطبوع)1013-9826
رقم المعيار الدولي للدوريات (الإلكتروني)1662-9795

ASJC Scopus subject areas

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