Tensile Damage Analysis Method for Composite Laminates Using a Quasi-3-Dimensional Model
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概要
- 論文の詳細を見る
Measurement of the strength for laminated composites is very difficult because their failure processes involve various failure modes, which are, for example, interlaminar delamination, destruction of the matrix and interfacial fracture between the fiber and matrix. However, their strength is one of the most important characteristics in structural design using laminated composites. Hence we attempted to develop a fractural progress analysis of laminated composites using a quasi-3-dimensional analysis method under a tensile load. The quasi-3-dimensional model is constructed of shell elements and beam elements which represent the fiber and matrix, respectively. The fractural progress analyses of the laminated composites are carried out to evaluate this proposed model, and are compared with experimental results. Therefore we confirm that this proposed model can simulate a transverse crack and interlaminar delamination independently.
- 一般社団法人日本機械学会の論文
- 1995-01-15
著者
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YOKOYAMA Atsushi
Faculty of Dentistry, Tokyo Med. & Dent. Univ.
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MAEKAWA Zenichiro
Faculty of Engineering,Osaka City University
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Maekawa Z
Division Of Advanced Fibro-science Kyoto Institute Of Technology
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Maekawa Yoshinori
Faculty Of Engineering Osaka Sangyo University
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NISHIWAKI Tsuyoshi
Asics Corporation
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Hamada Hiroyuki
Faculty of Textile Science, Kyoto Institute of Technology
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Mori Sadaki
ASICS Corp.
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Nishiwaki Tsuyoshi
Asics Corp.
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Hamada H
Faculty Of Textile Science Kyoto Institute Of Technology
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Maekawa Zenichiro
Faculty Of Engineering Osaka City University
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Yokoyama A
Faculty Of Education Mie University
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Yokoyama Atsushi
Faculty Of Dentistry Tokyo Med. & Dent. Univ.
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Hamada Hiroyuki
Faculty Of Textile Science Kyoto Institute Of Technology
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