TY - JOUR
T1 - Study on in-plane compression properties and numerical modeling of three dimensional five-directional braided composites
AU - Zuo, Hong-mei
AU - Zhu, Hao
AU - Li, Dian-sen
AU - Jiang, Lei
N1 - Funding Information:
The authors acknowledge the financial supports from Excellent Young Scientist Foundation of NSFC, China (No. 11522216 ); National Natural Science Foundation of China (No. 11872087 ); Beijing Municipal Natural Science Foundation, China (No. 2182033 ); The 111 Project (No. B14009 ); Project of the Science and Technology Commission of Military Commission, China (No. 17-163-12-ZT-004-002-01 ); Foundation of Shock and Vibration of Engineering Materials and Structures Key Laboratory of Sichuan Province, China (No. 18kfgk01 ). All authors approved the version of the manuscript to be published.
Publisher Copyright:
© 2021 Elsevier Ltd
PY - 2021/11
Y1 - 2021/11
N2 - Delamination phenomenon often occurs on traditional laminated composites while 3D five-directional braided composites (3D5dBC) could avoid this defect in practical application. In this work, the mechanical properties and failure mechanisms of 3D5dBC with different braiding angles are investigated at room temperature under transversal and longitudinal compression via experiments and finite element analysis (FEA) simultaneously. Meanwhile, the compression properties at elevated temperature are also researched. It is found that mechanical properties of composites under longitudinal compression are superior to those under transversal compression. Composite with small braiding angle possesses higher strength and modulus comparing to those of large braiding composite. Moreover, at room temperature, 3D5dBC exhibits 45º shear crack failure mode under transversal compression originated from matrix cracking, fiber failure along Z-direction obtained from FEA, and interfacial debonding; Under longitudinal compression, the structure shows shear expansion failure feature due to thorough fracture of axial yarns along L-direction, braiding yarns fracture along L-, T- and Z-direction, and matrix cracks obtained from FEA. With temperature increasing, interfacial debonding of fiber/matrix gets obvious. The microscopic failure modes and process at room temperature are well explained by FEA method.
AB - Delamination phenomenon often occurs on traditional laminated composites while 3D five-directional braided composites (3D5dBC) could avoid this defect in practical application. In this work, the mechanical properties and failure mechanisms of 3D5dBC with different braiding angles are investigated at room temperature under transversal and longitudinal compression via experiments and finite element analysis (FEA) simultaneously. Meanwhile, the compression properties at elevated temperature are also researched. It is found that mechanical properties of composites under longitudinal compression are superior to those under transversal compression. Composite with small braiding angle possesses higher strength and modulus comparing to those of large braiding composite. Moreover, at room temperature, 3D5dBC exhibits 45º shear crack failure mode under transversal compression originated from matrix cracking, fiber failure along Z-direction obtained from FEA, and interfacial debonding; Under longitudinal compression, the structure shows shear expansion failure feature due to thorough fracture of axial yarns along L-direction, braiding yarns fracture along L-, T- and Z-direction, and matrix cracks obtained from FEA. With temperature increasing, interfacial debonding of fiber/matrix gets obvious. The microscopic failure modes and process at room temperature are well explained by FEA method.
KW - 3D braided composite
KW - Damage mechanics
KW - Finite element analysis
KW - Mechanical properties
UR - http://www.scopus.com/inward/record.url?scp=85112755248&partnerID=8YFLogxK
U2 - 10.1016/j.tws.2021.108232
DO - 10.1016/j.tws.2021.108232
M3 - Article
AN - SCOPUS:85112755248
VL - 168
JO - Thin-Walled Structures
JF - Thin-Walled Structures
SN - 0263-8231
M1 - 108232
ER -