Bin Yang

Bin Yang


Research Focus & Metrics

Academic Career Length

6Years (2021-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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9 May 2023 in Polymers
Verified
Journal Article
Open access
PDF file
HLHaiqing Liu
Haiqing Liu
KFKunkun Fu
Kunkun Fu
XCXiaoyu Cui
Xiaoyu Cui
HZHuixin Zhu
Huixin Zhu
Bin YangBin Yang
Bin Yang
Shear thickening fluid (STF) is a dense colloidal suspension of nanoparticles in a carrier fluid in which the viscosity increases dramatically with a rise in shear rate. Due to the excellent energy absorption and energy dissipation of STF, there is a desire to employ STFs in a variety of impact applications. In this study, a comprehensive review on STFs’ applications is presented. First, several common shear thickening mechanisms are discussed in this paper. The applications of different STF impregnated fabric composites and the STF’s contributions on improving the impact, ballistic and stab resistance performance have also been presented. Moreover, recent developments of STF’s applications, including dampers and shock absorbers, are included in this review. In addition, some novel applications (acoustic structure, STF-TENG and electrospun nonwoven mats) based on STF are summarized, to suggest the challenges of future research and propose some more deterministic research directions, e.g., potential trends for applications of STF.

1 December 2021 in Thin-Walled Structures
Verified
Journal Article
Closed access
Bin YangBin Yang
Bin Yang
HWHongjian Wang
Hongjian Wang
Yuan ChenYuan Chen
Yuan Chen
KFKunkun Fu
Kunkun Fu
YLYan Li
Yan Li

13 September 2023 in Polymers
Verified
Journal Article
Open access
PDF file
ZZZhuoying Zhou
Zhuoying Zhou
Zhongsen ZhangZhongsen Zhang
Zhongsen Zhang
KFKunkun Fu
Kunkun Fu
Bin YangBin Yang
Bin Yang
In aerospace applications, composite grids have been widely utilized to enhance the strength of large thin-shell components. Recently, a growing focus has been on the research of 3D printing continuous fiber-reinforced thermoplastic composites. The 3D printing method offers various advantages over traditional molding processes, including a simpler process, higher material utilization, and lower manufacturing costs. However, the use of 3D printing for manufacturing continuous fiber-reinforced composite structures presents challenges, such as a high occurrence of defects within the structure and insufficient mechanical properties. These limitations hinder its widespread application. To address these issues, this study proposes a method for treating 3D-printed composite grid structures using induction heating. Initially, the induction heating mechanism of 3D-printed composite grids was analyzed by studying the impedance at the junction, including direct contact resistance and dielectric hysteresis loss. Subsequently, the impact of induction heating treatment on internal defects was explored by observing micro morphologies. The results show that the combination of induction heating and vacuum pressure effectively reduces porosities within the 3D-printed carbon fiber composite grids. Additionally, 3D-printed composite grid-stiffened PLA structures were fabricated with induction heating, and the bending and impact tests were conducted to evaluate their mechanical properties. The results indicate that using a grid-unit size of 4 mm leads to significant increases in bending strength and modulus of the grid-stiffened structure, with improvements of 137.6% and 217.8%, respectively, compared to the neat PLA panel. This demonstrates the exceptional mechanical enhancement efficiency of the 3D-printed lightweight composite grids.

18 December 2024 in Composite Structures
Verified
Journal Article
Open access
JWJiang Wu
Jiang Wu
ALAonan Li
Aonan Li
YLYahui Lyu
Yahui Lyu
Bin YangBin Yang
Bin Yang
KFKunkun Fu
Kunkun Fu
DYDongmin Yang
Dongmin Yang

9 March 2021 in Journal of Composite Materials
Verified
Journal Article
Closed access
PDF file
Bin YangBin Yang
Bin Yang
KFKunkun Fu
Kunkun Fu
YLYan Li
Yan Li
In this paper, a finite element model (FEM) was developed to investigate failure mechanism and compression after impact (CAI) strength of woven carbon fibre reinforced polymer (CFRP) after low-velocity impact (LVI) subjected to biaxial compressive loading. A built-in VUMAT user-defined material subroutine was adopted to take into account the in-plane damage and intralaminar delamination under LVI loading and in-plane compression. The LVI response, failure pattern, and residual mechanical properties under uniaxial compression were compared to the available experimental data to verify the numerical model. The damage initiation, subsequent evolution, final failure modes, and residual strength of the composite laminates with LVI damages subjected to biaxial compressive loading are presented by numerical methods, and the effects of impact energy and impactor diameter on the residual strength of the laminates are discussed.

15 June 2023 in Composites Communications
Verified
Journal Article
Closed access
YWYun Wan
Yun Wan
CTChangfu Tang
Changfu Tang
ZJZhiyuan Jiang
Zhiyuan Jiang
FWFangxin Wang
Fangxin Wang
CHChaojie Hu
Chaojie Hu
Bin YangBin Yang
Bin Yang