Kink band orientation of 3D printed continuous carbon fiber composites under compressive loading

Author:

Bin Zakaria Ahmad Zuhair1,Takahashi Takuya1,Todoroki Akira2,Ueda Masahito3

Affiliation:

1. Graduate Student, Tokyo Institute of Technology, Ookayama, 1528550, 2-12-1 Tokyo, Meguro, Japan

2. Department of Mechanical Engineering, Tokyo Institute of Technology, Ookayama, 1528550, 2-12-1 Tokyo, Meguro, Japan

3. Department of Mechanical Engineering, Nihon University 101-8308, 1-8-14 Chiyoda, Tokyo, Kanda-Surugadai, Japan

Funder

Tokyo Institute of Technology

Publisher

Informa UK Limited

Subject

Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference27 articles.

1. Dow NF, Rosen BW. Evaluations of filament-reinforced composites for aerospace structural applications. NASA Technical Report, NASA-CR-207. 1965. https://ntrs.nasa.gov/citations/19650012756

2. Fracture of Composites

3. A study on compressive strength of unidirectional graphite-epoxy composites.

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