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Kai Jin

Researcher at Nanjing University of Aeronautics and Astronautics

Publications -  35
Citations -  554

Kai Jin is an academic researcher from Nanjing University of Aeronautics and Astronautics. The author has contributed to research in topics: Ultimate tensile strength & Forming processes. The author has an hindex of 12, co-authored 35 publications receiving 345 citations. Previous affiliations of Kai Jin include Sogang University.

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Effect of Original Layer Thicknesses on the Interface Bonding and Mechanical Properties of Ti-Al Laminate Composites

TL;DR: In this article, vacuum hot pressing was employed to fabricate Ti Al laminate composites using Ti and Al foils of different thickness, and the resulting interface bond and mechanical properties were then studied to determine the optimum sheet configuration and thickness.
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Simulation and experimental research of the free bending process of a spatial tube

TL;DR: In this paper, the authors analyzed movement track of bending die based on the principle of free bending technology and analyzed distribution characteristics of equivalent stress and strain on tube and bending die during different stages of the free bending process.
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Forming characteristics of tube free-bending with small bending radii based on a new spherical connection

TL;DR: In this article, a new spherical connection of the bending die to the guide was designed through geometric derivation, which can lead to a greater deflection of the bend die, to realize the bending ratio of down to R/D0 = 2.5.
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Effect of fiber surface functionalization on shear behavior at carbon fiber/epoxy interface through molecular dynamics analysis

TL;DR: In this article, the dynamic adsorption and shear behavior at the interface between epoxy resin and carbon fibers were analyzed through molecular dynamics analysis and microscopic verification test, and it was found that more functional groups are accumulated at the surface and the interfacial shear strength increase with the extension of the acid treatment time.
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Mechanical analysis and progressive failure prediction for fibre metal laminates using a 3D constitutive model

TL;DR: In this paper, a 3D constitutive model was developed to analyse the mechanical behaviours under tensile and bending conditions, and ductile damage of metal layers, failure of fiber reinforced polymer (FRP) layers and interface delamination were predicted by 3D criteria.