Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Xuejuan Niu"'
Publikováno v:
Journal of Vibroengineering. 24:1568-1577
Fibre spreading before impregnation process has great importance for production of non-woven fabrics. Thousands of filaments can be transported and spread by airflow in a pneumatic chamber. To better understand the lateral-spreading mechanism of the
Publikováno v:
Journal of Vibroengineering. 24:714-725
This paper develops an optimum cell structure design method considering the in-plane tensile/compression and shear properties to improve the stiffness and strength of the honeycomb core. The equivalent elastic modulus in the X or Y direction and shea
Autor:
Xuejuan Niu, Yan Yao
Publikováno v:
Journal of Applied Polymer Science. 139
Progressive Damage Modelling of Composite Laminates Under Low Velocity Impact Based on MCT Criterion
Publikováno v:
Fibers and Polymers. 22:1623-1632
In order to study the damage mechanism of carbon fiber composite laminates, an experimental and numerical investigation has been carried out to study the dynamic perforation behaviors of composite plates subjected to low velocity impact. The numerica
Autor:
Xuejuan Niu, Tian Wang
Publikováno v:
Assembly Automation. 38:282-290
Purpose To realize the smooth interpolation of orientation on robot end-effector, this paper aims to propose a novel algorithm based on the unit quaternion spline curve. Design/methodology/approach This algorithm combines the spherical linear quatern
Publikováno v:
Composite Structures. 238:111986
Variable-stiffness laminates can redistribute the applied load and increase critical buckling loads compared to traditional straight fiber laminates. To take full advantage of fiber reinforced composite materials, a practical trajectory planning meth
Publikováno v:
IOP Conference Series: Materials Science and Engineering. 746:012038
In order to smoothly spread large-sized carbon-fiber bundle, hot-jet blower is added to a turbulent spreading platform to conduct pre-spreading process. To achieve the best spreading performance, CFD model of the blower are simulated based on the Rey
Publikováno v:
Advances in Material Science. 1:1
The three point bending fatigue properties of carbon fiber epoxy matrix composite laminates were compared for fatigue loading stress levels of 75, 80 and 85%, and fatigue loading frequencies of 10, 15 and 20Hz, respectively. The experimental results
Publikováno v:
IOP Conference Series: Materials Science & Engineering; Mar2020, Vol. 746 Issue 1, p1-1, 1p