TY - JOUR
T1 - Mechanical behavior of C/SiC T-section under pulling load
AU - He, Zongbei
AU - Chen, Bo
AU - Zhang, Yi
AU - Liu, Yongsheng
AU - Zhang, Litong
N1 - Publisher Copyright:
© 2019
PY - 2019/12
Y1 - 2019/12
N2 - For the C/SiC T-section structures, fabrication defects such as pores and local delaminations can be easily formed in the intersection zone which significantly affect the load bearing capacity. In this work, the mechanical behavior of C/SiC T-section under pulling load was investigated, and especially the delamination behavior was studied by introducing the cohesive zone model into the finite element modeling. It was found that for C/SiC T-section under pulling load, the maximum critical delamination load was about 1075 N in the present work, and the interface delamination was the main failure mode. It was verified that the effective interfacial strength influenced the critical delamination load, and the strain energy release affected the delamination behavior of the T-section specimen. The failure mechanisms of C/SiC T-section under pulling load depend on the interface bonding states. When the interface is well bonded, the failure mechanisms mainly include matrix stripping, matrix fracture and fiber breakage. Otherwise, only the matrix stripping can be found at the interface of the C/SiC T-section specimen.
AB - For the C/SiC T-section structures, fabrication defects such as pores and local delaminations can be easily formed in the intersection zone which significantly affect the load bearing capacity. In this work, the mechanical behavior of C/SiC T-section under pulling load was investigated, and especially the delamination behavior was studied by introducing the cohesive zone model into the finite element modeling. It was found that for C/SiC T-section under pulling load, the maximum critical delamination load was about 1075 N in the present work, and the interface delamination was the main failure mode. It was verified that the effective interfacial strength influenced the critical delamination load, and the strain energy release affected the delamination behavior of the T-section specimen. The failure mechanisms of C/SiC T-section under pulling load depend on the interface bonding states. When the interface is well bonded, the failure mechanisms mainly include matrix stripping, matrix fracture and fiber breakage. Otherwise, only the matrix stripping can be found at the interface of the C/SiC T-section specimen.
KW - C/SiC composites
KW - Failure analysis
KW - Mechanical behavior
KW - Structure and properties
UR - http://www.scopus.com/inward/record.url?scp=85075403469&partnerID=8YFLogxK
U2 - 10.1016/j.jmst.2019.04.040
DO - 10.1016/j.jmst.2019.04.040
M3 - 文章
AN - SCOPUS:85075403469
SN - 1005-0302
VL - 35
SP - 2950
EP - 2956
JO - Journal of Materials Science and Technology
JF - Journal of Materials Science and Technology
IS - 12
ER -