کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
253808 | 503027 | 2008 | 18 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Progressive failure and post-buckling response of tapered composite plates under uni-axial compression
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی عمران و سازه
پیش نمایش صفحه اول مقاله
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چکیده انگلیسی
The objective of the present work is to predict the first-ply failure load, the ultimate failure load, the buckling load, the associated maximum transverse displacements, and locations and modes of failure of tapered laminated plates under the action of uni-axial compression. A non-linear finite element formulation is developed based on the first-order shear deformation theory and the geometric non-linearity in the von Karman sense. The tensor polynomial form of the maximum stress criterion is used in conjunction with a progressive failure simulation methodology. A parametric study on tapered composite plates is conducted, considering the influences of different laminate configurations, taper configurations and fiber orientation angles.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Composite Structures - Volume 82, Issue 2, January 2008, Pages 159–176
Journal: Composite Structures - Volume 82, Issue 2, January 2008, Pages 159–176
نویسندگان
Rajamohan Ganesan, Dai Ying Liu,