213 Prediction of the Whole Stress-strain Curve and Final Composite Strength of GFRP Cross-ply Laminates
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概要
- 論文の詳細を見る
The strength prediction of the composite laminates is necessary for the engineering application. In predicting the strength of the arbitrary lay-up laminates, the interaction between the fiber failure and the ply cracks is critical. Therefore, the advanced micro-mechanical models considering the ply cracks and the fiber failures should be established. The present study investigates experimentally the microscopic damage evolution of glass fiber reinforced polymer (GFRP) cross-ply laminates and predicts the stress-strain relation up to failure using the statistical simulation. Especially, a new numerical model based on the finite element method and the Monte Carlo simulation is proposed and the fiber breakage is coupled with the matrix cracks in the 90-degree plies in this model. Concerning the matrix cracks, the present model utilizes the experimental results obtained from the replica observations. The simulated results have a good agreement with the experimental results and it is found that the present model can predict the micro mechanical damage process of GFRP.
- 一般社団法人日本機械学会の論文
著者
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Noda Junji
Department Of Integrated Design Engineering Keio University
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Takeda Nobuo
Graduate School Of Frontier Sciences The University Of Tokyo
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Okabe Tomonaga
National Institute Of Advanced Industrial Science And Technology
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Shimizu Masao
o Komaba Open Laboratory (KOL), The University of Tokyo
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Shimizu Masao
O Komaba Open Laboratory (kol) The University Of Tokyo
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Takeda Nobuo
Graduate School Of Frontier Sciences C
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NODA Junji
Department of Aerospace Engineering, Tohoku University
関連論文
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- Experimental characterization of microscopic damage progress in quasi-isotropic CFRP laminates : effect of interlaminar-toughened layers
- Analysis of stress and displacement fields in interlaminar-toughened composite laminates with transverse cracks
- Microscopic fatigue failure process in interleaved and toughness-improved CFRP cross-ply laminates
- Experimental characterization of microscopic damage progress in AS4/PEEK cross-ply laminates under thermal cycling
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- 213 Prediction of the Whole Stress-strain Curve and Final Composite Strength of GFRP Cross-ply Laminates
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