Composites are materials of choice for lightweight structures due to their excellent strength/weight/and stiffness/weight/properties. For several years, the application of composite materials with continuous fiber was limited to those with thermosetting matrix. Recently, interest in composites with thermoplastic matrix is growing thanks to their considerable advantages also in terms of recyclability. The thermoplastic composites appear to be the right alternative to the materials currently used, replacing not only the non-structural parts, but also the structural components located in areas potentially subject to impacts. This paper presents the results of an experimental campaign made on a fully thermoplastic composite, where both the reinforcement and the matrix are made in polypropylene. The target is to analyze its behavior under different impact loading conditions using a drop weight testing machine. The influence of the impact mass and of the velocity on the energy absorption capability of the material have been analyzed and discussed. During the tests, the material showed a ductile behavior and developed extended plasticity without a crack tip. The main observed damage mechanisms were the yarn sliding. (C) 2017 Elsevier Ltd. All rights reserved.
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Hong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R ChinaHong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R China
Kazemi, M. E.
Shanmugam, Logesh
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Hong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R ChinaHong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R China
Shanmugam, Logesh
Li, Zhonghong
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Shenzhen Univ, Coll Civil & Transportat Engn, Shenzhen 518060, Peoples R ChinaHong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R China
Li, Zhonghong
Ma, Rui
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Shenzhen Univ, Coll Civil & Transportat Engn, Shenzhen 518060, Peoples R ChinaHong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R China
Ma, Rui
Yang, Lei
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Shenzhen Univ, Coll Civil & Transportat Engn, Shenzhen 518060, Peoples R ChinaHong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R China
Yang, Lei
Yang, Jinglei
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Hong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R ChinaHong Kong Univ Sci & Technol, Dept Mech & Aerosp Engn, Kowloon, Clear Water Bay, Hong Kong, Peoples R China
机构:
School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai,200240, ChinaSchool of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai,200240, China
Lu, Taoye
Shen, Hui-Shen
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School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai,200240, ChinaSchool of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai,200240, China
Shen, Hui-Shen
Wang, Hai
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School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai,200240, ChinaSchool of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai,200240, China
Wang, Hai
Chen, Xiuhua
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School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai,200240, ChinaSchool of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai,200240, China